Sanyo LA7615 Specifications

Page 1
Ordering number : ENN5841
91799RM (OT) No. 5841-1/39
Overview
The LA7615 is an NTSC color TV IC that supports computer control over an I2C bus. In addition to improved quality and increased functionality in color TV products, this IC supports the development of a TV set product line in software and the simplification of end product design. The provision of an I2C bus means that this product can also respond to desires for increased total manufacturing productivity, including improved automation of computer controlled production lines.
Functions
•I2C bus control, VIF, SIF, Y, C, and deflection circuits integrated on a single chip.
Features
• Pursuit of higher integration levels The LA7615 integrates VIF, SIF, luminance, chrominance, and deflection (horizontal and vertical synchronization) circuits, A/V switching, and power supply control on a single chip.
• Bus control for reduced external component counts and mechanical adjustment points All the LA7615 signal-processing circuits can be controlled and adjusted digitally over the I2C bus. All adjustments, both those required during manufacture and the user controls, can be controlled over the I2C bus, and both function selection and characteristics settings can be performed in software over the I2C bus. This increases flexibility in designing a product line of TV sets and also enhances productivity by allowing mixed production runs. While this device supports multifunction and good performance, it is also economical in that it achieves reduced power and reduced pin count.
Package Dimensions
unit: mm
3071-DIP64S
57.2
0.95 0.48 1.78 1.01
4.00.51min
5.0max
19.05
16.8
0.25
3.2
3364
321
SANYO: DIP64S
[LA7615]
LA7615
SANYO Electric Co.,Ltd. Semiconductor Company
TOKYO OFFICE Tokyo Bldg., 1-10, 1 Chome, Ueno, Taito-ku, TOKYO, 110-8534 JAPAN
Single-Chip NTSC Color TV IC
Monolithic Linear IC
Any and all SANYO products described or contained herein do not have specifications that can handle applications that require extremely high levels of reliability, such as life-support systems, aircraft’s control systems, or other applications whose failure can be reasonably expected to result in serious physical and/or material damage. Consult with your SANYO representative nearest you before using any SANYO products described or contained herein in such applications.
SANYO assumes no responsibility for equipment failures that result from using products at values that exceed, even momentarily, rated values (such as maximum ratings, operating condition ranges, or other parameters) listed in products specifications of any and all SANYO products described or contained herein.
Page 2
No. 5841-2/39
LA7615
Parameter Symbol Conditions Ratings Unit
V2 max 9.6 V
Maximum supply voltage
V17 max 9.6 V V32 max 9.6 V
V60 max 9.6 V Maximum supply current I24 max 30 mA Allowable power dissipation Pd max Ta 65°C 1.5 W Operating temperature Topr –10 to +65 °C Storage temperature Tstg –55 to +150 °C
Specifications
Maximum Ratings at Ta = 25°C
Parameter Symbol Conditions Ratings Unit
V2 7.6 V
Recommended supply voltage
V17 7.6 V V32 7.6 V V60 7.6 V
Recommended supply current I24 24 mA
V2 op 7.3 to 7.9 V
Operating supply voltage range
V17 op 7.3 to 7.9 V V32 op 7.3 to 7.9 V V60 op 7.3 to 7.9 V
Operating supply current range I24 op 20 to 30 mA
Operating Conditions at Ta = 25°C
Functional Description
<VIF/SIF Functions> In addition to a PLL synchronous detection system, the IF block also adopts a split system in which the VIF signal and the SIF signal are processed separately.
• Low-level VCO The LA7615 achieves a significant reduction in beat generation due to interference by lowering the VCO oscillator level from that used in earlier ICs.
• Adjustment-free VCO coil implemented using bus control By compensating for manufacturing variations in the VCO coil using bus control, the LA7615 eliminates coil adjustment from the manufacturing line.
• Built-in 4.5 MHz trap The LA7615 incorporates an on-chip trap that also provides a video equalizer function. Thus the number of external trap, inductor, and capacitor components is reduced.
• Built-in SIF FM detector: 4.5 MHz quadrature detection
• The video signal and FM demodulated signal levels can be controlled from the serial bus. The improved precision associated with controlling the output level over the serial bus makes it easier to design the interface with the following stage.
• Built-in buzz canceler Allows high performance to be maintained even during stereo reception.
• Built-in video switch (INT/EXT(AUX) switching circuit) Built-in AUX input switching circuit means that the dedicated switching ICs required can be reduced. Also, the ability to control this switch from the serial bus makes it easier to design the peripheral wiring pattern.
• Dedicated IF video signal output pin The provision of this pin makes it easier to design end products that support PIP and similar features.
<Luminance and Chrominance Circuits> These blocks have been designed to minimize the use of external components as much as possible. The filter circuits are now integrated on the same chip, and not only the adjustment circuits, but also the function selection and characteristics modifications functions can be controlled over the serial bus. As a result, basically all the signal processing from input to output can be performed with only the addition of the chrominance circuit VCO crystal and the APC filter circuit.
Page 3
Furthermore, this IC also supports high image quality systems and responds to needs from a diverse range of end products.
• Two independent inputs for the luminance and chrominance signals and switching between the Y1/C1 and Y2/C2 inputs
• Video muting on/off switch
• Built-in filters (The filter f0 adjustment function can be used to select the filter characteristics.) Chrominance system: Bandpass filter (symmetric and asymmetric types) Luminance system: Color trap and delay line
<Luminance System Circuit>
• Built-in high image quality variable-type luminance system filter (color trap and delay line) Luminance filter mode selection (f0 adjustment) Four modes are provided: 3.58 MHz trap, 4.2 MHz trap, 5.0 MHz wide, and 10.0 MHz high band.
• Peaking (sharpness) control Aperture type control implemented using the delay line The emphasis frequency is automatically selected according to the f0 mode using the delay line. One of the four frequencies 2.2, 2.6, 3.0, or 4.9 MHz is emphasized according to which of the f0 modes (3.58 MHz trap, 4.2 MHz trap, 5.0 MHz wide, or 10.0 MHz high band) is used.
• Adaptive coring For low-level signals, the above peaking is suppressed to reduce the image contamination due to that peaking. The coring level is automatically adjusted according to the amplitude of the input signal.
• Black stretch circuit: Can be turned on or off under control of the serial bus interface.
• SYO (Selected luminance (Y) output) One of the Y1/Y2 inputs is selected, and that input signal is output as the sync separator circuit signal directly. However, the DC level of that signal is clamped at 1/2 VCC. Also, this signal can be used for closed captions or as a velocity modulation.
• Support for analog/digital OSD Amplitude level limiting is applied to digital input signals internally to the IC.
• Contrast and brightness controls
• ABL (automatic beam limiter) Three-pin system (IB IN, BRT ABL FILT, and CONTRAST ABL FILT pins), mode switching under control of serial bus data.
• R, G, and B output drive and bias adjustments
• Sub-bias (brightness) control The DC level of each of the R, G, and B signals can be adjusted over a 4-step (2-bit) range.
<Chrominance Circuit>
• Built-in chrominance bandpass filter Chrominance system filter mode selection: bandpass filter peaking/symmetric type selection and chrominance bandpass filter bypass on/off setting
• Auto Flesh: Flesh tone correction (on/off)
• Overload (on/off) Limits the saturation of the color when the ratio of the burst and color signals is large, i.e. when the color is highly saturated.
• Color phase and saturation controls
• Demodulation angle: 104°
No. 5841-3/39
LA7615
<f0 Mode Selection>
*: Reference values
Mode f0 = Y signal Chroma signal
Trap f0 *Total delay BPF *Total 500 ns delay 0 3.58 MHz 500 ns Asymmetric (peaking type) 515 ns 1 4.2 MHz 510 ns
Symmetric 535 ns
2 5.0 MHz 520 ns 3 10.0 MHz 265 ns Bypass 265 ns
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<Deflection Circuits> Dedicated sync separator circuit input pin The horizontal deflection circuit adopts a dual AFC circuit, and the horizontal oscillator uses the 32fH (503 kHz) pulse signal as the horizontal decrement counter clock. The following are the main settings for the horizontal output system that can be controlled over the serial bus interface. These settings support even more efficient end product design.
• AFC gain (first loop gain control)
• APC gain (second loop gain control)
• Horizontal duty cycle
• Horizontal phase *: The vertical deflection circuit adopts a decrement counter system, and provides constantly adjustment-free and stable
vertical synchronization for any type of signal, from TV on air, to weak reception conditions, to VCR signals. Furthermore, this circuit uses an internal capacitor to implement a ramp generator, and allows the corrections described later in this document to be applied to correct image distortion and other problems due to manufacturing variations in the TV tube itself.
<Horizontal Circuit Functions>
• High-stability adjustment-free horizontal oscillator that uses a ceramic oscillator element
• Dual AFC circuit
• Multi-mode control of the AFC gain (first loop gain)
• Horizontal duty and phase controls
• Geometrical distortion correction: East-west DC (horizontal size)
East-west amplitude (horizontal pin-cushion distortion correction) Corner pin
East-west corner 1 East-west corner 2
Tilt adjustment
• Sync killer
<Vertical Circuit Functions>
• Forcible non-standard mode support (standard mode: 262.5 H)
• Vertical size/linearity and vertical DC (vertical position) adjustments, vertical S-curve correction
• V-comp adjustment (Corrects for changes in the vertical size due to variations in the luminance.)
• Vertical killer
<Power System> PWM circuits have come to be widely used in TV set power supplies in recent years. This IC integrates parts of the power supply circuit (the pulse generator and its control system) and allows the supply voltage (high B) to be adjusted over the serial bus.
No. 5841-4/39
LA7615
Page 5
No. 5841-5/39
LA7615
Bus Control
General Functions
ON/OFF SW 1 bit Video muting switch 1 bit
VIF/SIF
Video signal switching 1 bit RF AGC delay 6 bits IF AGC SW 1 bit PLL tuning 7 bits APC detector adjustment 6 bits AFT defeat switch 1 bit Noise inverter defeat switch 1 bit Video level 3 bits Sound 4.5 MHz trap 4 bits FM level 4 bits F0 fast (FM detection speed) 1 bit
Luminance/Chrominance Systems
Y/C input selection (one of two inputs) switch 1 bit Luminance (Y) F0 adjustment (filter control) 2 bits Chrominance signal bandpass filter mode switch 1 bit Chrominance signal bandpass filter bypass switch 1 bit Black stretch on/off switch 1 bit Peaking (sharpness) control 5 bits Coring on/off switch 1 bit Auro flesh on/off 1 bit Overload switch 1 bit Contrast control 6 bits Brightness control 6 bits Tint control 7 bits Saturation control 7 bits RGB bias adjustment 6 bits each RGB bias adjustment 7 bits each Sub-brightness control 2 bits each Brightness ABL operating point control 3 bits Brightness ABL mode defeat switch 1 bit each Emergency ABL defeat switch 1 bit
Deflection System
AFC gain (sync killer) 2 bits APC gain 2 bits Horizontal duty adjustment 2 bits Horizontal phase adjustment 4 bits Geometrical distortion correction EAST-WEST DC 5 bits EAST-WEST AMPLITUDE 4 bits East-west corner 1/2 3 bits each Tilt adjustment 4 bits Vertical linearity adjustment 4 bits Vertical S-curve correction 4 bits Vertical size adjustment 7 bits Vertical DC adjustment 6 bits Standard/nonstandard mode switch 1 bit VERTICAL KILL 1 bit V-COMP adjustment 3 bits DAC REF. (+B TRIM) 4 bits
Others: Status Register
POWER ON RESET 1 bit X-ray protection switch 1 bit Horizontal lock detection 1 bit AFT and RF AGC status discrimination 2 bits each
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No. 5841-6/39
LA7615
A10048
Wide
Vertical Linearity
Vertical S-Curve Correction
Tilt
East-West Amp
Corner Pin
The distortion correction operation is symmetric left to right.
Narrow
Narrow
Wide
Wide
Wide
Narrow
Narrow
Narrow
Wide
East-west corner 1
East-west corner 2
A10049
A10050
A10051
A10052
Page 7
No. 5841-7/39
LA7615
Bus : Control Register Bit Allocation Map
Control Register Bit Allocations
IC address Sub address MSB Data bits LSB
IC Add7 Add0 ¥ Add7 Add0 Bit 7 Bit 6 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0
1011 1010 0000 0000 1 On/Off Video AFC gain/sync kill
mute (b1) (b0)
0001 1 APC gain B+ trim
(b1) (b0) (b3) (b2) (b1) (b0)
0010 1 Hor duty cycle Horizontal phase
(b1) (b0) (b3) (b2) (b1) (b0)
0011 1 BNI RF AGC delay
defeat (b5) (b4) (b3) (b2) (b1) (b0)
0100 1 IF AGC AFT FM level
defeat defeat (b4) (b3) (b2) (b1) (b0)
0101 1 VCO free running
(b6) (b5) (b4) (b3) (b2) (b1) (b0)
0110 1 4.5 MHz trap
(b3) (b2) (b1) (b0) (b2) (b1) (b0)
0111 1 Video IF APC offset adjust.
switch (b5) (b4) (b3) (b2) (b1) (b0)
1000 1 Vertical Vertical DC
kill (b5) (b4) (b3) (b2) (b1) (b0)
1001 1 Countdown mode East-west DC
(b1) (b0) (b4) (b3) (b2) (b1) (b0)
1010 1 East-west amp
(b3) (b2) (b1) (b0)
1011 1 Vertical comp. East-west tilt
(b2) (b1) (b0) (b3) (b2) (b1) (b0)
1100 1 Vertical size
(b6) (b5) (b4) (b3) (b2) (b1) (b0)
1101 1 Vertical linearity
(b3) (b2) (b1) (b0)
1110 1 FM mode Vertical S-correction
switch (b3) (b2) (b1) (b0)
1111 1 East-west bottom corner East-west top corner
(b2) (b1) (b0) (b2) (b1) (b0)
Bits are transmitted in this order
Page 8
No. 5841-8/39
LA7615
Bus : Control Register Bit Allocation Map
Control Register Bit Allocations (cont)
IC address Sub address MSB Data bits LSB
IC Add7 0 Add7 Add0 Bit 7 Bit 6 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0
1011 1010 0001 0000 1 Red bias
(b6) (b5) (b4) (b3) (b2) (b1) (b0)
0001 1 Green bias
(b6) (b5) (b4) (b3) (b2) (b1) (b0)
0010 1 Blue bias
(b6) (b5) (b4) (b3) (b2) (b1) (b0)
0011 1 Red drive
(b5) (b4) (b3) (b2) (b1) (b0)
0100 1 Green drive
(b5) (b4) (b3) (b2) (b1) (b0)
0101 1 Blue drive
(b5) (b4) (b3) (b2) (b1) (b0)
0110 1 Blue sub bias Red sub bias Green sub bias Y/C
(b1) (b0) (b1) (b0) (b1) (b0) switch
0111 1 Brightness control
(b5) (b4) (b3) (b2) (b1) (b0)
1000 1 Pix control
(b5) (b4) (b3) (b2) (b1) (b0)
1001 1 Coring Peaking control
switch (b4) (b3) (b2) (b1) (b0)
1010 1 F0 select Chroma Auto Chrom Over
(b1) (b0) BPF flesh bypass load
1011 1 Tint control
(b6) (b5) (b4) (b3) (b2) (b1) (b0)
1100 1 Color control
(b6) (b5) (b4) (b3) (b2) (b1) (b0)
1101 1 ABL Mid Stp EMG Bright ABL threshold
defeat defeat defeat (b2) (b1) (b0)
1110 1 Test register 1 Test register 2
(b3) (b2) (b1) (b0) (b2) (b1) (b0)
1111 1 Test regster 3 Black Stretch Blanking Reserved
(b3) (b2) (b1) (b0) defeat defeat
IC address Sub address MSB Data bits LSB
IC Add7 Add0 Add7 Add0 Bit 7 Bit 6 Bit 5 Bit 4 Bit 3 Bit 2 Bit 1 Bit 0
1011 1010 0001 0000 Pon XRay Horiz On/off AFT status RF AGC status
lock
0001 1 1 1 1 1 1 1 1
Bits are transmitted in this order
Table 8 : Status Register Bit Allocation Map
Status Register Bit Allocations
Page 9
No. 5841-9/39
LA7615
Bus : Control Register Truth Table
Control Register Truth Table
Register 0 HEX 1 HEX 2 HEX 3 HEX On/off Off On na na Video mute Active Mute na na AFC gain/sync Kill Sync Kill Low gain (auto mode) Mid gain High gain BNI defeat Enable BNI Defeat na na IF AGC defeat Enable AGC Defeat na na AFT defeat Enable AFT Defeat na na Video switch IF video Aux video na na Vertical Kill Vertical active Vertical Killed na na Countdown mode Standard Non-standard 50 Hz 48 Hz FM mode switch Normal Fast na na Y/C switch Y1/C1 IN Y2/C2 IN na na Coring switch Defeat Enable na na F0 select 3.58 Trap 4.20 Trap 5.00 APF 10.0 APF Chrom BPF Symmetrical Peaker na na Autoflesh Off On na na Chroma bypass BPF Bypass na na Over load Off Active na na Bright ABL defeat Enable Defeat na na Bright mid stop defeat Enable Defeat na na Emergency ABL defeat Enable Defeat na na Black Str defeat Enable Defeat na na Blanking defeat Enable Defeat na na
Bus : Status Register Truth Table
Status Register Truth Table
Register 0 HEX 1 HEX 2 HEX 3 HEX POR Inactive Low standby detected na na XRP Inactive XRP fault detected na na Horizontal lock Locked Unlocked na na On/off Off On na na AFT IF frequency in high IF frequency in range na IF frequency is low RF AGC RF AGC voltage is Low. RF AGC voltage is in range. na RF AGC voltage is High.
Page 10
No. 5841-10/39
LA7615
Initial Condition
Function On/off 1 HEX Video mute 0 HEX AFC gain & sync Kill 1 HEX APC gain 3 HEX B+ trim 8 HEX Horizontal duty 1 HEX Horizontal phase 8 HEX BNI defeat 0 HEX RF AGC delay 20 HEX IF AGC defeat 0 HEX AFT defeat 0 HEX FM level 10 HEX IF VCO free running 40 HEX
4.5 trap 8 HEX Video level 4 HEX Video switch 0 HEX IF APC offset 20 HEX Vertical Kill 0 HEX Vertical DC 20 HEX Countdown mode 0 HEX East/west DC 10 HEX East/west amplitude 8 HEX Vertical comp. 0 HEX East/west tilt 8 HEX Vertical size 40 HEX Vertical linearity 8 HEX FM mode switch 0 HEX Vertical S-correction 8 HEX East/west bottom 0 HEX East/west top corner 0 HEX Red bias 00 HEX Green bias 00 HEX Blue bias 00 HEX Red drive 3F HEX Green drive 3F HEX Blue drive 3F HEX Blue sub bias 2 HEX Red sub bias1 2 HEX Green sub bias 2 HEX Y/C switch 0 HEX Brightness control 20 HEX Pix control 20 HEX Coring switch 0 HEX Peaking control 00 HEX F0 select 1 HEX Chroma BPF 0 HEX Autoflesh 0 HEX Chroma bypass 0 HEX Over load 0 HEX Tint control 40 HEX Color control 40 HEX Bright ABL defeat 0 HEX Bright mid stop 0 HEX Emergency ABL defeat 0 HEX Bright ABL threshold 0 HEX Test registers 1, 2, 3 0 HEX Black strech defeat 1 HEX Blanking defeat 0 HEX
Page 11
Power Up Sequence <Reference>
No. 5841-11/39
LA7615
6.3VDC
7.3VDC
3.0VDC
time 2ms
ON/OFF
= 0
ON/OFF
= 1
Mute
= 0
Initialize
TR1 to TR2
Initialize
TR3 to TR31
Standby
Vcc
ON/OFF
BIT
Registers
(TR1-TR2)
XRP BIT
(STATUS)
Pon BIT
(STATUS)
Registers
(TR3-TR31)
Video.Mute
BIT
Run.Vcc
stable
A10053
After Standby Vcc reaches 3.0VDC, the microcontroller has to wait 2ms in order to intitialize the HC Interface in LA7615.
Page 12
No. 5841-12/39
LA7615
Parameter Symbol Conditions
Ratings
Unit
min typ max
[Circuit Voltages and Currents]
Horizontal supply voltage HV
CC
7.2 7.6 8 V
IF power supplly current (V2) I2 (IFI
CC
) IF AGC : 5 V 28 43 58 mA
Vertical supply current (V17) I17 (DEFI
CC
)101316mA
Video/chrominance supply current (V32) I32 (YCI
CC
) 65 85 105 mA
FM supply current (V60) I60 (FMI
CC
) 5.5 8.5 11.5 mA
[VIF Block]
No signal AFT output voltage V14 With no input signal 2.8 3.8 4.8 Vdc No signal video output voltage V53 With no input signal 4.7 4.9 5.1 Vdc
APC pull-in range (U) f
PU
After APC, PLL, and D/A converter
1 MHz
adjustment
APC pull-in range (L) f
PL
After APC, PLL, and D/A converter
1 MHz
adjustment
Maximum RF AGC voltage V
4H
CW = 91 dBµ, DAC = 0 7.7 8.2 9.0 Vdc
Minimum RF AGC voltage V
4L
CW = 91 dBµ, DAC = 63 0 0.2 0.4 Vdc
RF AGC Delay Pt (@DAC = 0) RF
AGC0
DAC = 0 96 dBµ
RF AGC Delay Pt (@DAC = 63) RF
AGC63
DAC = 63 86 dBµ
Maximum AFT output voltage V
14H
CW = 93 dBµ, frequency change 6.2 6.5 7.6 Vdc
Minimum AFT output voltage V
14L
CW = 93 dBµ, frequency change 0.5 0.9 1.2 Vdc
AFT detection sensitivity Sf CW = 93 dBµ, frequency change 33 25 17 mV/kHz
4.5 MHz attenuation T
RAP
V100 kHz/V4.5 MHz –35 –32 dB
Video output amplitude V
O
53 93 dBµ, 87.5% Video MOD 1.8 2 2.2 Vp-p
Synchronizing signal tip level V53
TIP
93 dBµ, 87.5% Video MOD 2.4 2.6 2.8 Vdc
Input sensitivity V
IN
Output –3 dB 43 46 dBµ Vide/sync ratio (@100 dBµ) V/S 100 dBµ, 87.5% Video MOD 2.4 2.5 3 Differential gain DG 93 dBµ, 87.5% Video MOD 2 10 % Differential phase DP 93 dBµ, 87.5% Video MOD 2 10 deg Video signal-to-noise ratio S/N CW = 93 dBµ 55 58 dB 920 kHz beat level I920 V3.58 MHz/V920 kHz –57 –50 dB
[SIF Block]
[1st.SIF]
4.5 MHz conversion gain SG
G
21 26 31 dB
4.5 MHz output level SV
O
91 96 101 dB
First SIF maximum input SV
M
–1 0 +1 dB
[SIF Block]
FM detection output voltage S
OADJ
414 424 434 mVrms
FM limiting sensitivity S
LS
50 dBµ
FM detector output bandwidth S
F
50 100k Hz
FM detector output distortion S
THD
1%
AM rejection ratio S
AMR
40 dB
SIF. Signal-to-noise ratio S
SN
74 dB
[Chrominance Block]
ACC amplitude characteristics 1 ACC
M
1 Input: +6 dB/0 dB, 0 dB = 40 IRE 0.8 1.0 1.2 times
ACC amplitude characteristics 2 ACC
M
2 Input: –14 dB/0 dB 0.8 1.0 1.1 times
B-Y/Y amplitude ratio CLR
BY
75 100 120 %
Color control characteristics 1 CLR
MN
Color: max/normal 1.7 2.0 2.3 times Color control characteristics 2 CLR
MN
Color: max/min 33 40 50 dB Color control sensitivity CLR
SE
1 2 4 %/bit
Tint center TIN
CEN
TINT NOM –10 +5 deg Tint control max TIN
MAX
TINT max 30 45 60 deg Tint control min TIN
MIN
TINT min –60 –45 –30 deg Tint control sensitivity TIN
SE
0.7 2.0 deg/bit Demodulated output ratio: B-Y/R-Y BR 1.06 1.19 1.32 Demodulated output ratio: G-Y/R-Y GR 0.34 0.40 0.46
Electrical Characteristics at Ta = 25°C, VCC= V2 = V17 = V32 = V60 = 7.6 V, ICC= I24 = 24 mA
Continued on next page.
Page 13
No. 5841-13/39
LA7615
Continued from preceding page.
Parameter Symbol Conditions
Ratings
Unit
min typ max
Demodulation angle B-Y/R-Y AN
GBR
99 104 109 deg Demodulation angle G-Y/R-Y ANGGR –146 –136 –127 deg Killer operating point KILL 0 dB = 40IRE –32 –26 –22 dB Chrominance V
CO
free-running frequency CVCOF Deviation from 3.579545 MHz –250 +250 Hz
Chrominance pull-in range (+) PUL
IN+
350 Hz
Chrominance pull-in range (–) PUL
IN–
–350 Hz
Auto Flesh characteristics: 73° AF
073
8 20 30 deg
Auto Flesh characteristics: 118° AF
118
–7 0 +7 deg Auto Flesh characteristics: 163° AF
163
–30 –20 –8 deg Overload characteristics 1 OVL1 3.2 4.7 Overload characteristics 2 OVL2 4.2 6.8 Overload characteristics 3 OVL3 4.5 8.5
[Chrominance Bandpass Filter Block]
Peaking amplitude characteristics: 3.08 MHz C
PE308
Referenced to 3.48 MHz –5 –3 –1 dB
Peaking amplitude characteristics: 3.88/3.28 MHz
C
PE
Referenced to 3.28 MHz –0.5 +1.5 +3.5 dB
Peaking amplitude characteristics: 4.08/3.08 MHz
C
PE05
Referenced to 3.08 MHz –5.0 2.5 –1 dB
Bandpass amplitude characteristics: 3.08 MHz C
BP308
Referenced to 3.48 MHz –5 –3 –1 dB
Bandpass amplitude characteristics: 3.88/3.28 MHz
C
BP
Referenced to 3.28 MHz –2 0 +2 dB
Bandpass amplitude characteristics: 4.08/3.08 MHz
C
BP05
Referenced to 3.08 MHz –2.5 0 +2.5 dB
[Video Block]
Video overall gain (at maximum contrast) CONT63 10 12 14 dB Contrast adjustment characteristics (normal/max) CONT32 –7.5 –6.0 –4.5 dB Contrast adjustment characteristics (min/max) CONT0 –15 –12 –9 dB Video frequency characteristics: f0 = 3 Y
f03
–6.0 –3.5 0.0 dB
Chrominance trap level: f0 = 0 C
trap
–23 –15 dB
DC restoration C
lampG
95 100 105 %
Luminance delay: f0 = 1 Y
DLY
480 505 530 ns Maximum black stretch gain BKSTmax 12 16 20 IRE Black stretch threshold (40 IRE black) BKST
TH
–2 0 +2 IRE
Sharpness variation range (normal) Sharp16 4 6 8 dB
(max) Shaprp31 9.0 11.5 14.0 dB (min) Shapr0 –6.0 –3.5 –1.0 dB
Horizontal/vertical blanking output level RGB
BLK
1.4 1.7 2.0 V
[OSD Block]
OSD fast switch threshold FS
TH
1.7 1.9 2.2 V
RGB output level: red R
OSDH
120 165 200 IRE RGB output level: green G
OSDH
70 120 140 IRE
RGB output level: blue B
OSDH
85 120 155 IRE
Analog OSD output level R
RGB
1.12 1.4 1.68 Ratio
Gain matching Linearity LR
RGB
45 50 60 %
Continued on next page.
Page 14
No. 5841-14/39
LA7615
Continued from preceding page.
Parameter Symbol Conditions
Ratings
Unit
min typ max
Analog OSD green output level G
RGB
0.8 1.0 1.2 Ratio
Gain matching Linearity LG
RGB
45 50 60 %
Analog OSD blue output level B
RGB
0.8 1.0 1.2 Ratio
Gain matching Linearity LB
RGB
45 50 60 %
[RGB Output (cutoff and drive) Block]
Brightness control (normal) BRT32 2.0 2.35 2.7 V
High brightness (max) BRT63 15 20 25 IRE Low brightness (min) BRT60 –25 –20 –5 IRE
Cutoff control (min) Vbias0 1.6 2.0 2.4 V
(bias control) (max) Vbias128 2.8 3.2 3.6 V Cutoff contrad Resolution Vbiassns 3 4 6 mV/bit Sub-bias control resolution Vsbiassns 160 220 280 mV/bit
Drive adjustment: maximum output RGBout63 2.4 3.0 3.6 Vp-p
Output attenuation RGBout0 7 9 11 dB
[Deflection Block]
Sync separator circuit sensitivity S
sync
10 15 IRE
Horizontal free-running frequency deviation f
H
15.634 15.734 15.834 kHz
Horizontal pull-in range f
H PULL
±400 Hz Horizontal output pulse width @0 Hduty0 ON time, Hduty : 0 36.0 37.5 39.0 µs Horizontal output pulse width @1 Hduty1 ON time, Hduty : 1 34.3 35.8 37.5 µs Horizontal output pulse width @2 Hduty2 ON time, Hduty : 2 32.5 34.0 35.5 µs Horizontal output pulse width @3 Hduty3 ON time, Hduty : 3 30.5 32.0 33.5 µs Horizontal output pulse saturation voltage V
H
sat 0.4 V
Horizontal output pulse phase HPH
CEN
9.5 10.5 11.5 µs Horizontal position adjustment range HPHrange 4 bits ±2 µs Horizontal position adjustment maximum variation
HPHstep 350 ns
X-ray protection circuit operating voltage V
XRAY
2.7 3.0 3.3 V POR circuit operating voltage V
POR
5.5 6.3 6.7 V [Vertical Screen Size Adjustment] Vertical ramp output amplitude @64 Vsize64 V
SIZE
: 1000000 1.44 1.74 2.04 Vp-p
Vertical ramp output amplitude @0 Vsize0 V
SIZE
: 0000000 0.72 1.02 1.32 Vp-p
Vertical ramp output amplitude @127 Vsize127 V
SIZE
: 1111111 2.14 2.44 2.64 Vp-p [High Voltage Dependency Vertical Size Correction] Vertical size correction @3 Vsizecomp V
COMP
: 11 0.96 0.97 0.98 ratio [Vertical Screen Position Adjustment] Vertical ramp DC voltage @32 Vdc32 V
DC
: 1000000 3.686 3.876 4.484 Vdc
Vertical ramp DC voltage @0 Vdc0 V
DC
: 0000000 3.344 3.557 3.762 Vdc
Vertical ramp DC voltage @63 Vdc63 V
DC
: 1111111 4.104 4.294 4.484 Vdc
Vertical linearity @8 Vlin8 V
LIN
: 1000 0.93 0.985 1.04 ratio
Vertical linearity @0 Vlin0 V
LIN
: 0000 0.77 0.84 0.92 ratio
Vertical linearity @15 Vlin15 V
LIN
: 1111 1.13 1.18 1.25 ratio
Vertical S-curve correction @8 VScor8 V
S
: 1000 0.77 0.84 0.92 ratio
Vertical S-curve correction @0 VScor0 V
S
: 0000 0.92 1.00 1.08 ratio
Vertical S-curve correction @15 VScor15 V
S
: 1111 0.62 0.72 0.78 ratio
Continued on next page.
Page 15
No. 5841-15/39
LA7615
Continued from preceding page.
Parameter Symbol Conditions
Ratings
Unit
min typ max
[Horizontal Size Adjustment]
East/west DC voltage @16 EWdc16 EW
DC
: 10000 3.60 4.00 4.40 Vdc
East/west DC voltage @0 EWdc0 EW
DC
: 00000 2.70 3.05 3.40 Vdc
East/west DC voltage @31 EWdc31 EW
DC
: 11111 4.80 5.10 5.40 Vdc
[Pin cushion Distortion Correction]
East/west parabola amplitude @8 EWamp8 EW
AMP
: 1000 0.58 0.73 0.88 Vp-p
East/west parabola amplitude @0 EWamp0 EW
AMP
: 0000 0.15 0.30 0.45 Vp-p
East/west parabola amplitude @15 EWamp15 EW
AMP
: 1111 0.95 1.15 1.35 Vp-p
[Trapezoidal Distortion Correction]
East/west parabola tilt @8 EWtilt4 EW
TILT
: 1000 –0.14 0 +0.14 V
East/west parabola tilt @0 EWtilt0 EW
TILT
: 0000 –0.37 –0.23 –0.09 V
East/west parabola tilt @15 EWtilt7 EW
TILT
: 1111 0.09 0.23 0.37 V
[Corner Distortion Correction]
East/west parabola corner, top EWcorTOP COR
TOP
: 111-000 0.15 0.25 0.35 V
East/west parabola corner, bottom EWcorTOP COR
BOTTOM
: 111-000 0.15 0.25 0.35 V
[Sandcastle Output]
Burst gate pulse peak value V
BGP
5.0 5.7 6.5 V
Burst gate pulse phase Td
BGP
4.6 5.1 5.6 µs
Burst gate pulse width PW
BGP
2.35 2.85 3.35 µs
Blanking pulse peak value V
BLK
3.4 3.9 4.4 V
[D/A Converter Output]
Pin 30 D/A converter voltage @0 V
DAC
0 +B TRIM : 0000 2.75 3.00 3.25 V
Pin 30 D/A converter voltage @8 V
DAC
8 +B TRIM : 1000 3.15 3.40 3.65 V
Pin 30 D/A converter voltage @15 V
DAC
15 +B TRIM : 1111 3.55 3.80 4.05 V
Circuit Voltage and Current Test Conditions at Ta = 25°C, VCC= V2= V17= V32= V60= 7.6 V, ICC= I24= 24 mA
Parameter Symbol
Test point
Input signal Test procedure Bus condition
[Circuit Voltage and Current]
Horizontal supply voltage
IF current drain (pin 2)
Vertical current drain (pin 17) Video, chrominance, current drain
(pin 32)
FM power supply current (pin 60)
HV
CC
I2(IFICC)
I
17
(DEFICC)
I32(YCVCC)
I60(FMVCC)
No signal
No signal
Apply a 24-mA current to pin 24 and measure the voltage on pin 24 at that time.
Apply 7.6 V to pin 2 and measure the DC current (in mA) that flows into the IC. (With 5 V applied to the IF AGC)
Apply 7.6 V to pin 17 and measure the DC current (in mA) that flows into the IC.
Apply 7.6 V to pin 32 and measure the DC current (in mA) that flows into the IC.
Apply 7.6 V to pin 60 and measure the DC current (in mA) that flows into the IC.
Initial
Initial
Initial
Initial
Initial
24
2
17 32 60
Page 16
VIF Block - Input Signals and Test Conditions
1. All input signals are input to VIF IN in the test circuit diagram.
2. The input signal voltages are all taken to be the voltage at VIF IN in the test circuit diagram.
3. The signals and their levels are as follows.
No. 5841-16/39
LA7615
Input signal
Input signal Waveform Condition
SG1 45.75 MHz
SG2 42.17 MHz
SG3 41.25 MHz
SG4 Variable frequency
SG5 45.75 MHz
87.5% video modulation 10-step waveform (subcarrier: 3.58 MHz)
SG6 45.75 MHz
87.5% video modulation Sweep signal (APL: 50 IRE, sweep signal level: 40 IRE)
SG7 45.75 MHz
87.5% video modulation Flat field signal
4. Before testing, adjust the D/A converter in the order presented below.
Parameter
Test point
Input signal Adjustment
APC DAC
PLL DAC
Video level DAC
Trap
No signal, with pin 11 connected to ground
SG1, 93 dBµ
SG7, 93 dBµ
SG6, 93 dBµ
Set the pin 14 DC voltage to be as close to 3.8 V as possible.
Set the pin 14 DC voltage to be as close to 3.8 V as possible.
Set the pin 53 output level to be 2.0 ±0.2 Vpp. Lower the D/A converter from its maximum (15) and set the circuit so that the
4.5 MHz component is at least –32 dB below the 100 kHz component.
14 14 53 53
CW
A10054
CW
A10055
CW
A10056
CW
A10057
A10058
40 IRE
50 IRE
A10059
100 IRE
A10060
Page 17
No. 5841-17/39
LA7615
(Test Conditions)
Parameter Symbol
Test point
Input signal Test procedure Bus condition
[VIF Block]
No signal AFT output voltage
No signal video output voltage
APC pull-in range (U), (L)
Maximum RF AGC voltage
Minimum RF AGC voltage
Video output amplitude
RF AGC Delay Pt (@DAC = 0)
RF AGC Delay Pt (@DAC = 63)
Input sensitivity
Video/Sync ratio (@100 dBµ)
Differential gain
Differential phase
Video signal-to-noise ratio
Synchronizing signal tip level
4.5 MHz attenuation
920 kHz beat level
Maximum AFT output voltage
Minimum AFT output voltage
AFT detection sensitivity
V14
V53
f
PU
, f
PL
V4
H
V4
L
VO53
RF
AGC
0
RF
AGC
63
V
IN
V/S
DG
DP
S/N
V53 TIP
TRAP
I920
V14
H
V14
L
Sf
No signal
No signal
SG4 93 dBµ
SG1 91 dBµ
SG1 91 dBµ
SG7 93 dBµ
SG1
SG1
SG7
SG7 100 dBµ
SG5 93 dBµ
SG5 93 dBµ
SG1 93 dBµ
SG1 93 dBµ
SG6 93 dBµ
SG1 SG2 SG3
SG4 93 dBµ
44.75 MHz SG4
93 dBµ
46.75 MHz
SG4 93 dBµ
Connect the pin 11 to ground and measure the pin 14 DC voltage.
Connect the pin 11 to ground and measure the pin 53 DC voltage.
Monitor pin 53 with an oscilloscope, and modify SG4 to have a frequency higher than 45.75 MHz so that the PLL goes to the unlocked state. (Beating should appear at this point.) Gradually decrease the SG4 frequency until the PLL circuit locks, and measure the lock frequency. Also, and modify SG4 to have a frequency lower than 45.75 MHz so that the PLL goes to the unlocked state. Gradually increase the SG4 frequency until the PLL circuit locks, and measure the lock frequency.
Set the RF AGC D/A converter to 0 and measure the pin 4 DC voltage.
Set the RF AGC D/A converter to 63 and measure the pin 4 DC voltage.
Monitor the pin 53 with an oscilloscope, and measure the peak-to-peak value of the waveform.
Set the RF AGC D/A converter to 0 and determine the input level such that the pin 4 DC voltage becomes 3.8 ±0.5 V.
Set the RF AGC D/A converter to 63 and determine the input level such that the pin 4 DC voltage becomes 3.8 ±0.5 V.
Monitor the pin 53 with an oscilloscope, and measure the peak-to-peak value of the waveform. Gradually decrease the input level and determine the input level such that the output goes down to a level lower than the video amplitude (V
O
53) by –3 dB.
Monitor the pin 53 with an oscilloscope, and measure the peak-to-peak values of the sync waveform (Vs) and the luminance signal (Vy) to determine the ratio Vy/Vs.
Measure the pin 53 with a vectorscope.
Measure the pin 53 with a vectorscope. Pass the noise voltage signal generated at pin 53
through a 4 to 10 MHz bandpass filter and measure that signal(V
sn
) with an rms voltmeter. Determine the
value of the formula 20log(1.43/Vsn). Measure the pin 53 DC voltage.
Measure the values of the 100 kHz and 4.5 MHz components and determine their ratio.
Input the 93 dBµ SG1 signal, and measure the pin 11 DC voltage (V11). Mix the three signals SG1 = 87 dBµ, SG2 = 82 dBµ, and SG3 = 63 dBµ, and input that signal to VIF IN. Apply the voltage V11 to pin 11 using an external power supply. Measure the difflerence of the 3.58 MHz and 920 kHz components using a spectrum analyzer.
Measure the pin 14 DC voltage.
Measure the pin 14 DC voltage.
Gradually change the SG4 frequency and determined the frequency change f required to change the pin 14 DC voltage from 2.5 V to 5.0 V. Sf = 2500/f [mV/kHz]
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
The adjusted values from item 4.
14 53
53
4 4
53
4
4
53
53
53 53
53
53 53
53
14
14
14
Page 18
First SIF Block - Input Signals and Test Conditions
For each of the test items, set up the following conditions unless otherwise specified.
1. PIF.IN: 45.75 MHz, 93 dBµ, CW
2. Bus control conditions: Set the following 4 items to their adjusted values. (See the VIF block test description for details on the adjustment procedure.)
• APC DET.ADJ
• PLL tuning
• 4.5 MHz trap
• Video level
3. Apply the input signal to the pin 12, using a signal with a frequency of 41.25 MHz CW.
SIF Block - Input Signals and Test Conditions
For each of the test items, set up the following conditions unless otherwise specified.
1. Connect pin 13 (SIF AGC) to ground.
2. Bus control conditions: IF.AGC.SW = 1.
3. SW:IF1 = off
4. Apply the input signal to pin 61. The carrier frequency should be 4.5 MHz.
No. 5841-18/39
LA7615
Parameter Symbol
Test point
Input signal Test procedure Bus condition
4.5 MHz conversion gain
4.5 MHz output level
First SIF maximum input
SC
G
SV
O
SV
M
60 dBµ
88 dBµ
96 dBµ
Measure the pin 59 output 4.5 MHz component (mV rms). Let SV1 be this measured value and perform the following calculation. SC
G
= 20 × log(SV1 × 1000) – 60 [dB]
Measure the pin 59 output 4.5 MHz component (mV rms). Let SV2 be this measured value and perform the following calculation. SC
O
= 20 × log(SV2 × 1000) [dB]
Measure the pin 59 output 4.5 MHz component (mV rms). Let SV3 be this measured value and perform the following calculation. SC
M
= 20 × log(SV3/SV1) [dB]
59
Parameter Symbol
Test point
Input signal Test procedure Bus condition
FM detector output voltage
FM limiting sensitivity
FM detector output bandwidth
FM detector output distortion
AM rejection ratio
SIF signal-to-noise ratio
SO
ADJ
SLS
SF
S
THD
S
AMR
S
SN
90 dBµ, fm = 1 kHz, FM = ±25 kHz
fm = 1 kHz, FM = ±25 kHz
90 dBµ, FM ±25 kHz
90 dBµ, fm = 1 kHz, FM ±25 kHz
90 dBµ, fm = 1 kHz, AM = 30%
90 dBµ, CW
Adjust the D/A converter (FM.LEVEL) so that the pin 5 FM detector output 1 kHz component is as close to 424 mV rms as possible. Measure the output (mV rms) at that time. Let SV1 be the measured value at this time.
Determine the input level (dBµ) such that the pin 5 FM detector output 1 kHz component is down –3 dB from SV1.
Determine the modulation frequency bandwidth (Hz) for a –3 dB drop in the pin 5 FM detector output 1 kHz component with respect to SV1.
Determine the distortion in the pin 5 FM detector output 1 kHz component.
Measure (in mV rms) the pin 5 FM detector output 1 kHz component. Let SV2 be the measured value at this time and perform the following calculation. S
AMR
= 20 × log(SV1/SV2) [dB]
Set the SW:IF1 switch to the on state. Measure the noise level (mV rms) on pin 5. Let SV3 be the measured value at this time and perform the following calculation. S
SN
= 20 × log(SV1/SV3) [dB]
FM.LEVEL = adjusted value.
FM.LEVEL = adjusted value.
FM.LEVEL = adjusted value.
FM.LEVEL = adjusted value.
FM.LEVEL = adjusted value.
5
5
5
5
5
5
59
59
Page 19
Video Block - Input Signals and Test Conditions
[Input Signals] <CINinput signal> *: chrominance burst signal: 40 IRE <YINinput signal> 0 IRE signal (L-0): NTSC standard synchronizing signal
No. 5841-19/39
LA7615
H SYNC
4.7 µs
(H/V SYNC : 40 IRE : 286 mV)
Pedestal level
A10061
X IRE signal (L-X)
A10062
X IRE (X = 0 to 100)
0 IRE
CW signal (L-CW)
A10063
50 IRE
Black stretch 0 IRE signal (L-BK)
A10064
50 µs
5 µs
100 IRE
A10065
A
B
0.35 V
0.7 V
0.0 VDC
RGB input signal 2 (O-2)
A10066
20 µs 30 µs
1.0 VDC
0.0 VDC
20 IRE CW signal
20 µs each
(Point A)
<R/G/B IN input signal> RGB input signal 1 (O-1)
[ 100 IRE : 714 mV ]
Page 20
No. 5841-20/39
LA7615
(Test Conditions)
Parameter Symbol
Test point
Input signal Test procedure Bus bits/input signal
[Video Block] Overall video gain (at maximum
contrast)
Contrast adjustment characteristics (normal/max)
Contrast adjustment characteristics (normal/max)
Video frequency characteristics f0 = 1 (sharp 0)
f0 = 3 (sharp 15)
Chrominance trap level f0 = 0 (sharp 0)
DC restoration
Luminance delay f0 = 1
Maximum black stretch gain
Black stretch threshold black(40 IRE black)
Sharpness (peaking) variability characteristics (normal)
(maximum)
(minimum)
Horizontal/vertical blanking output level
CONT63
CONT32
CONT0
Yf03
Ctrap
ClampG
Y
DLY
BKSTmax
BKST
TH
Sharp16
Sharp31
Sharp0
RGB
BLK
L-50
L-50
L-50
L-CW
L-CW
L-0
L-100
L-50
L-BK
L-40
L-CW
L-CW
L-CW
L-100
Measure the output signal 50 IRE amplitude (CNT
HB
Vp-p) and calculate CONT63 = 20log(CNTHB/0.357).
Measure the output signal 50 IRE amplitude (CNT
CB
Vp-p) and calculate CONT32 = 20log(CNTCB/0.357).
Measure the output signal 50 IRE amplitude (CNT
LB
Vp-p) and calculate CONT0 = 20log(CNTLB/0.357). With the input signal CW = 100 kHz, measure the
amplitude of the CW signal in the output signal (PEAK
DC
Vp-p).
With the input signal CW = 10 MHz, measure the amplitude of the CW signal in the output signal (F03 Vp-p).
Calculate Yf3 = 20log(F03/PEAKDC). With the input signal CW = 3.58 MHz, measure the
amplitude of the CW signal in the output signal (F00 Vpp).
Calculate Ctrap = 20·log(F00/PEAKDC).
Measure the output signal 0 IRE DC level (BRTPL (V)).
Measure the output signal 0 IRE DC level (DRVPH (V)) and the 100 IRE amplitude (DRV
H
Vpp). Calculate ClampG = 100 × (1 + (DRVP
H
– BRTPL)/DRVH)).
Measure the time difference (amount of delay) between the rise of the input signal 50 IRE amplitude, and rise of the output signal 50 IRE amplitude.
Measure the 0 IRE DC level at point A in the output signal when the black stretch function is defeated (black stretch off). (BKST1 (V))
Measure the 0 IRE DC level at point A in the output signal when the black stretch function is on. (BKST2 (V))
Calculate BKSTmax = 2 × 50 × (BKST1 – BKST2)/CNT
HB
.
Measure the 40 IRE DC level in the output signal when the black stretch function is on. (BKST3 (V))
Measure the 40 IRE DC level in the output signal when the black stretch function is defeated (black stretch off). (BKST4 (V))
Calculate BKST
TH
= 50 × (BKST4 – BKST3)/CNTHB.
With the input signal CW = 2.2 MHz, measure the amplitude of the CW signal in the output signal (F00S16 Vp-p).
Calculate Sharp16 = 20log(F00S16/PEAK
DC
).
With the input signal CW = 2.2 MHz, measure the amplitude of the CW signal in the output signal (F00S31 Vp-p).
Calculate Sharp31 = 20log(F00S31/PEAK
DC
).
With the input signal CW = 2.2 MHz, measure the amplitude of the CW signal in the output signal (F00S0 Vp-p).
Calculate Sharp0 = 20log(F00S0/PEAKDC). Measure the DC level of the output signal during the
blanking period (RGB
BLK
(V)).
TR24: Contrast
111111
TR24: Contrast
000000
TR26: F0 Adjust 01
TR26: F0 Adjust 11 TR25: Sharpness
01111
TR26: F0 Adjust 00
TR23: Brightness
000000
TR24: Contrast
111111
TR23: Brightness
000000
TR24: Contrast
111111
TR31: BKST Defeat 1
TR31: BKST Defeat 0
TR31: BKST Defeat 0
TR31: BKST Defeat 1
TR26: F0 Adjust 00 TR25: Sharpness
10000
TR25: Sharpness
11111
TR25: Sharpness
00000
38
38
38
38
38
38
38
38
38
38
38
Continued on next page.
Page 21
No. 5841-21/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus bits/input signal
[OSD Block]
OSD fast switching threshold
RGB red output level
RGB green output level
RGB blue output level
Analog OSD red output level
Gain matching Linearity
Analog OSD green output level
Gain matching Linearity
Analog OSD blue output level
Gain matching Linearity [RGB Output Block] (Cutoff and Drive Blocks)
Brightness control
(normal)
(maximum)
(minimum)
FS
TH
R
OSDH
G
OSDH
B
OSDH
R
RGB
LR
RGB
G
RGB
LG
RGB
B
RGB
LB
RGB
BRT32
BRT63
BRT0
L-0 O-2
L-50 L-0
O-2
L-50 L-0
O-2
L-50 L-0
O-2
L-0 O-1
L-0 O-1
L-0 O-1
L-0
Gradually increase the pin 39 voltage starting at 1.5 V, and determine the pin 39 voltage at the point where the output signal switches to the OSD signal.
Measure the 50 IRE amplitude in the output signal. (CNT
CR
Vp-p).
Measure the OSD output amplitude (OSD
HR
Vp-p).
Calculate R
OSDH
= 50 × (OSDHR/CNTCR).
Measure the 50 IRE amplitude in the output signal. (CNTCGVp-p).
Measure the OSD output amplitude (OSD
HG
Vpp).
Calculate G
OSDH
= 50 × (OSDHG/CNTCG).
Measure the 50 IRE amplitude in the output signal. (CNTCB Vp-p).
Measure the OSD output amplitude (OSD
HB
Vp-p).
Calculate B
OSDH
= 50 × (OSDHB/CNTCB).
Measure the amplitudes at point A (the 0.35 V component of the input signal O-1) and point B (the
0.7 V component of the input signal O-1) in the output signal and record these as RGB
LR
and
RGB
HR
(Vp-p) respectively.
Calculate R
RGB
= RGBLR/CNTCR.
Calculate LR
RGB
= 100 × (RGBLR/RGBHR).
Measure the amplitudes at point A (the 0.35 V component of the input signal O-1) and point B (the
0.7 V component of the input signal O-1) in the output signal and record these as RGB
LG
and
RGB
HG
(Vp-p) respectively.
Calculate G
RGB
= RGBLG/CNTCG.
Calculate LG
RGB
= 100 × (RGBLG/RGBHG).
Measure the amplitudes at point A (the 0.35 V component of the input signal O-1) and point B (the
0.7 V component of the input signal O-1) in the output signal and record these as RGB
LB
and
RGB
HB
(Vp-p) respectively.
Calculate B
RGB
= RGBLB/CNTCB.
Calculate LB
RGB
= 100 × (RGBLB/RGBHB).
Measure the output signal 0 IRE DC levels of the R output (pin 36), G output (pin 37), and B output (pin
38) and record these as BRTPC
R
, BRTPCG, and
BRTPC
B
(V), respectively.
Calculate BRT63 = (BRTPCR+ BRTPCG+ BRTPCB)/3.
Measure the output signal 0 IRE DC level of the B output (pin 38) (BRTPHB).
Calculate BRT63 = 50 × (BRTPHB– BRTPCB) / CNTHB.
Measure the output signal 0 IRE DC level of the B output (pin 38) (BRTPLB).
Calculate BRT0 = 50 × (BRTPLB– BRTPCB) / CNTHB.
Pin 42:Apply signal O-2.
Pin 39: Apply 3.5 V. Pin 40: Apply signal O-2.
Pin 39: Apply 3.5 V. Pin 41: Apply signal O-2.
Pin 39: Apply 3.5 V. Pin 42: Apply signal O-2.
Pin 39: Apply 3.5 V. Pin 40: Apply signal O-1.
Pin 39: Apply 3.5 V. Pin 34: Apply signal O-1.
Pin 39: Apply 3.5 V. Pin 41: Apply signal O-1.
TR24: Contrast
111111
TR23: Brightness
111111
TR23: Brightness
000000
38
36
37
38
36
37
38
36 37 38
38
Continued on next page.
Page 22
No. 5841-22/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus bits/input signal [RGB Output Block] (Cutoff and Drive Blocks) Bias (cutoff) control
(minimum)
(maximum)
Bias (cutoff) control resolution
Sub-bias control resolution
Maximum drive adjustment output
Output attenuation
Vbias0
Vbias128
Vbiassns
Vsbiassns
RGBout63
RGBout0
L-50
L-50
L-100
Measure the output signal 0 IRE DC levels of the R output (pin 36), G output (pin 37), and B output (pin
38) and record these as Vbias0* (V), where * : R, G, and B, respectively.
Measure the output signal 0 IRE DC levels of the R output (pin 36), G output (pin 37), and B output (pin
38) and record these as Vbias128* (V), where * : R, G, and B, respectively.
Measure the output signal 0 IRE DC levels of the R output (pin 36), G output (pin 37), and B output (pin
38) and record these as BAS80* (V), where * : R, G, and B, respectively.
Measure the output signal 0 IRE DC levels of the R output (pin 36), G output (pin 37), and B output (pin
38) and record these as BAS48* (V), where * : R, G, and B, respectively.
Vbiassns * = (BAS80 * – BAS48 *)/32 Measure the output signal 0 IRE DC levels of the R
output (pin 36), G output (pin 37), and B output (pin
38) and record these as SBTPM* (V), where * : R, G, and B, respectively.
Vsbiassns * = (BRTPC * – SBTPM *) Measure the output signal 100 IRE DC amplitudes of
the R output (pin 36), G output (pin 37), and B output (pin 38) and record these as DRV
H
* (Vpp), where * :
R, G, and B, respectively.
Measure the output signal 100 IRE DC amplitudes of the R output (pin 36), G output (pin 37), and B output (pin 38) and record these as DRV
L
* (Vpp), where * :
R, G, and B, respectively.
RGBout0 * = 20 log(DRV
H
*/DRVL*)
TR24: CONTRAST
111111 TR22: SUB-BIAS R, G, B 000000
TR16: R BIAS
111111 TR: G BIAS
111111 TR18: B BIAS
111111 TR24: CONTRAST
111111 TR22: SUB-BIAS R, G, B 111111
TR16: R BIAS
1010000 TR17: G BIAS
1010000 TR18: B BIAS
1010000 TR24: CONTRAST
111111 TR16: R BIAS
0110000 TR17: G BIAS
0110000 TR18: B BIAS
0110000 TR24: CONTRAST
11111
TR22: SUB-BIAS R, G, B 101010
TR24: CONTRAST
111111 TR23: Brightness
000000 TR24: CONTRAST
111111 TR23: Brightness
000000 TR19: R DRIVE
000000 TR20: G DRIVE
000000 TR21: B DRIVE
000000
36 37 38
36 37 38
Page 23
Chrominance Block - Input Signals and Test Conditions
For each of the test items, set up the following conditions unless otherwise specified.
1. VIF and SIF blocks: No signal
2. Deflection block: Input a horizontal/vertical composite sync signal and verify that the deflection block is locked on the synchronizing signal. (See the section on input signals and test conditions for the deflection block.)
3. Bus control conditions: All conditions set to their initial values, unless otherwise specified.
4. Connect a crystal oscillator circuit to pin 16. Adjust the impedance (Z) of the series capacitance and resistance as shown below.
Z = 0 deg @ 3.579545 MHz ±10 Hz –40 ±1 deg @3.579345 MHz
5. Luminance (Y) input: No signal
6. Chrominance (C) input: Input the signal to the C1IN pin (pin 51).
7. The method for calculating the demodulation angle is shown below. B-Y axis angle = tan – 1 (B(0)/B(270)) + 270° R-Y axis angle = tan – 1 (R(180)/R(90)) + 90° G-Y axis angle = tan – 1 (G(270)/G(180)) + 180°
8. The method for calculating the AF angle is shown below. BR · · · · The B-Y/R-Y demodulation output ratio
θ
· · · · · · ANGBR: the B-Y/R-Y demodulation angle
R – Y/B – Y × BR – Cos
θ
AFXXX = tan – 1 ———————————
Sin
θ
No. 5841-23/39
LA7615
180°
270°
0°
90°
R (90)
G (270)
G (180)
R (180)
B (270)
B (0)
A10067
B-Y axis
R-Y axis
G-Y axis
Page 24
[Input Signal]
No. 5841-24/39
LA7615
40 IRE
40 IRE
Burst 0° 90° 180° 270°
3.58 MHz
0 IRE
77IRE
40IRE
Burst 3.58 MHz 364°
62.5IRE
Burst 3.48 MHz
CW
A10068
40 IRE
28° 73° 118° 163°
A10072
A10069
A10070
Burst 3.48 MHz
Chroma
35 µs
A10073
A10071
C-1
C-2
C-3
C-4
C-5
X IRE signal (L-X)
(However, when a frequency is specified, that frequency is to be used.)
Page 25
No. 5841-25/39
LA7615
(Test Conditions)
Parameter Symbol
Test point
Input signal Test procedure Bus condition
[Chrominance Block]
ACC amplitude characteristics 1
ACC amplitude characteristics 2
B-Y/Y amplitude ratio
Color control characteristics 1
Color control characteristics 2
Color control sensitivity
Tint center
Tint control (max)
Tint control (min)
Tint control sensitivity
Demodulation output ratio B-Y/R-Y
Demodulation output ratio G-Y/R-Y
ACC
M
1
ACC
M
2
CLR
BY
CLR
MN
CLR
MM
CLR
SE
TIN
CEN
TIN
MAX
TIN
MIN
TIN
SE
BR
GR
Bout
Bout
C-1 0 dB +6 dB
C-1 –14 dB
Y
IN
: L77
C-1: No signal
C-2
C-3
C-3
C-3
C-1
C-1
C-1
C-1
C-3
C-3
Measure the output amplitude when the chrominance input is set to 0 dB and the output amplitude when the input is reduced by – 6 dB, and calculate the ratio. ACC
M
1 = 20log(+6 dB data/0 dB data)
Measure the output amplitude when the chrominance input is set to –14 dB and calculate the ratio. ACC
M
2 = 20log(–14 dB data/0 dB data)
Measure the luminance (Y) output level(V1). Next, apply a signal to the C
IN
input (with only a sync applied to the Y input) and measure the output level (V2). Calculate the following formula. CLR
BY
= 100 × (V2/V1) +15%
Measure V1: the output amplitude when the color control is maximum, and V2: the output amplitude when the color control is normal (Color control:
1000000) and calculate CLR
MN
= V1/V2.
Measure V3: the output amplitude when the color control is minimum and calculate CLRMM= 20·log(V1/V3).
Measure V4: the output amplitude when the color control is 90, and V5: the output amplitude when the color control is 38. Calculate the following formula. CLR
SE
= 100 × (V4 – V5) / (V2 × 52)
Measure each section of the output waveform and calculate the angle of the B-Y axis.
Measure each section of the output waveform and calculate the angle of the B-Y axis. Calculate the following formula. TIN
MAX
= (the B-Y axis angle) – TIN
CEN
Measure each section of the output waveform and calculate the angle of the B-Y axis. Calculate the following formula. TIN
MIN
= (the B-Y axis angle) – TIN
CEN
Measure A1: the angle when the tint control is 85, and A2: the angle when the tint control is 42. Calculate the following formula. TIN
SE
= (A1 – A2)/43
Measure Vb: the B
OUT
output amplitude and Vr: the
R
OUT
output amplitude, and calculate BR = Vb/Vr.
Measure Vg: the G
OUT
output amplitude and
calculate GR = Vg/Vr.
TR28: Color Control
1111111
1000000
TR28: Color Control
0000000
TR28: Color Control
1011010 Color Ctontrol 0100110
TR27: TINT
0111111
TR27: TINT
1111111
TR27: TINT
0000000
TR27: TINT
1010101 0101010
TR28: Color Control
1000000
TR28: Color Control
1000000
38
38
38
38
38
38
38
38
38
38
38 36
37
Continued on next page.
Page 26
No. 5841-26/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus condition
Demodulation angle B-Y/R-Y
Demodulation angle G-Y/R-Y
Killer operating point
Chrominance VCO free-running frequency
Chrominance pull-in range (+)
Chrominance pull-in range (–)
Auto Flesh characteristics 73°
Auto Flesh characteristics 118°
Auto Flesh characteristics 163°
Overload characteristics 1
ANG
BR
ANG
GR
KILL
C
VCOF
PUL
IN
+
PUL
IN
AF073
AF118
AF163
OVL1
C-1
C-1
C-3
CIN No signal
C-1
C-1
C-4
C-4
C-4
C-5
Measure the B
OUT
and R
OUT
output levels and calculate the angle between the B-Y and R-Y axes. Calculate ANG
BR
= (R-Y angle) – (B-Y angle).
Measure the GOUT output level and calculate the angle between the G-Y and R-Y axes. Calculate ANG
GR
= (R-Y
angle) – (G-Y angle).
Gradually decrease the amplitude of the input signal and measure the input level when the output level falls less than 150 mVpp.
Measure the oscillator frequency f and calculate the following formula. C
VCOF
= f – 3579545 (Hz)
Gradually decrease the input signal subcarrier frequency starting at 3.579545 MHz + 1000 Hz, and measure frequency at the point the output waveform locks.
Gradually raise the input signal subcarrier frequency starting at 3.579545 MHz – 1000 Hz, and measure frequency at the point the output waveform locks.
With Auto Flesh = 0, measure the level that corresponds to a B
OUT
and R
OUT
output waveform of 73° and calculate the angle AF073A. With Auto Flesh = 1, measure the angle AF073B in the same manner. Calculate the following formula. AF073 = AF073B – AF073A
With Auto Flesh = 0, measure the level that corresponds to a B
OUT
and R
OUT
output waveform of 118° and calculate the angle AF118A. With Auto Flesh = 1, measure the angle AF118B in the same manner. Calculate the following formula. AF118 = AF118B – AF118A
With Auto Flesh = 0, measure the level that corresponds to a B
OUT
and R
OUT
output waveform of 163° and calculate the angle AF163A. With Auto Flesh = 1, measure the angle AF163B in the same manner. Calculate the following formula. AF163 = AF163B – AF163A
Measure V1: the output amplitude when the input signal burst level is set to 40 IRE and the chrominance level is set to 8 IRE, and V2: the output amplitude when the input signal burst level is set to 40 IRE and the chrominance level is set to 40 IRE. Calculate the following formula. OVL1 = V2/V1
TR26: Auto Flesh :
**** 0 **
TR26: Auto Flesh :
**** 1 **
TR26: Auto Flesh :
**** 0 **
TR26: Auto Flesh :
**** 1 **
TR26: Auto Flesh :
**** 0 **
TR26: Auto Flesh :
**** 1 **
TR26: OverLoad :
****** 1
38 36
37
38
16
38
38
38 36
38 36
38 36
36
Continued on next page.
Page 27
No. 5841-27/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus condition
Overload characteristics 2
Overload characteristics 3
Peaking amplitude characteristics: 3.08 MHz
Peaking amplitude characteristics: 3.88/3.28 MHz
Peaking amplitude characteristics: 4.08/3.08 MHz
Bandpass amplitude characteristics: 3.08 MHz
Bandpass amplitude characteristics: 3.88/3.28 MHz
Bandpass amplitude characteristics: 4.08/3.08 MHz
OVL2
OVL3
CPE308
CPE
CPE05
CBE308
CBE
CBE05
C-5
C-5
C-3
C-3
C-3
C-3
C-3
C-3
Measure V3: the output amplitude when the input signal burst level is set to 40 IRE and the chrominance level is set to 80 IRE. Calculate the following formula. OVL2 = V3/V1
Measure V4: the output amplitude when the input signal burst level is set to 20 IRE and the chrominance level is set to 80 IRE. Calculate the following formula. OVL3 = V4/V1
Measure V0: the output amplitude. Next, set the input chrominance signal (CW) frequency to 3.08 MHz and measure V1: the output amplitude. Calculate the following formula. CPE308 = 20log(V1/V0)
Measure V2: the output amplitude when the input chrominance signal (CW) frequency is 3.28 MHz, and V3: the output amplitude when the input chrominance signal (CW) frequency is 3.88 MHz. Calculate the following formula. CPE = 20log(V3/V2)
Measure V4: the output amplitude when the input chrominance signal (CW) frequency is 4.08 MHz. Calculate the following formula. CPE05 = 20log(V4/V1)
Measure V5: the output amplitude. Next, measure V6: the output amplitude when the input chrominance signal (CW) frequency is set to
3.08 MHz. Calculate the following formula. CPE308 = 20log(V6/V5)
Measure V7: the output amplitude when the input chrominance signal (CW) frequency is 3.28 MHz, and V8: the output amplitude when the input chrominance signal (CW) frequency is 3.88 MHz. Calculate the following formula. CPE = 20log(V8/V7)
Measure V9: the output amplitude when the input chrominance signal (CW) frequency is set to 4.08 MHz. Calculate the following formula. CPE05 = 20log(V9/V6)
TR26: Overload
******1
TR26: Overload
******1
TR26: CHR.BPF:
***1***
TR26: CHR.BPF:
***1***
TR26: CHR.BPF:
***1***
TR26: CHR.BPF:
***0***
TR26: CHR.BPF:
***0***
TR26: CHR.BPF:
***0***
36
36
38
38
38
38
38
38
[Chrominance Bandpass Filter Characteristics]
Page 28
Deflection Block - Input Signals and Test Conditions
For each of the test items, set up the following conditions unless otherwise specified.
1. VIF and SIF blocks: No signal
2. Luminance (Y) input and chrominance (C) input: No signal
3. Sync input: Horizontal/vertical composite sync signal (DC offset: 3.8 V, 40 IRE. Other timing and other parameters must conform to the FCC broadcast standards.) Caution: There must be no burst or chrominance signal under the pedestal level.
4. Bus control conditions: All conditions set to their initial values, unless otherwise specified.
5. The delay time from the rise of the horizontal output (the pin 26 output) to the rise of the F.B.P IN (pin 27 input) must be 9 µs.
6. The pin 18 (the vertical size correction circuit input pin) voltage must be VCC(7.6 V).
7. Pin 28 (the x-ray protection circuit input pin) must be connected to ground.
Notes: Perform the following operations if the horizontal output pulse signal was stopped.
1. Set the bus on/off bit to off (0) temporarily, and then set it to on (1) again. (If the x-ray protection circuit and/or the PON-RES circuit operate, an IC internal latch circuit will be set. The on/off bit must be set to off (0) to reset that latch circuit, even if the horizontal output signal is not output. Since the PON­RES circuit operates when the horizontal supply voltage rises, the on/off bit must be set to off (0).)
2. Note on video muting If the horizontal output pulse signal was stopped, after performing the operation described in paragraph 1 above, clear the video muting bit to 0. (This is because the video muting bit is forcibly set to 1 when the on/off bit is set to 0 or when either the x-ray protection circuit or the PON-RES circuit operate. This also applies at power on.)
No. 5841-28/39
LA7615
A10074
Signal inappropriate for use as a sync input
Chrominance signal
Signal appropriate for use as a sync input
Burst signal
Page 29
No. 5841-29/39
LA7615
Parameter Symbol
Test point
Input signal Test procedure Bus condition
[Deflection Block]
Sync separator circuit sensitivity
Horizontal free-running frequency deviation
Horizontal pull-in range
Horizontal output pulse width @0
Horizontal output pulse width @1
Horizontal output pulse width @2
Horizontal output pulse width @3
Horizontal output pulse saturation voltage
Horizontal output pulse phase
Ssync
f
H
fHPULL
Hduty 0
Hduty 1
Hduty 2
Hduty 3
V
H
sat
HPH
CEN
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: no signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
Gradually decrease the level of the synchronizing signal input to SYNC IN (pin 44) and measure the level of the synchronizing signal when the synchronization is unlocked.
Connect the pin 26 output (Hout) to a frequency counter and measure the horizontal free-running frequency. Calculate the following formula. f
H
= <measured value> – 15.743 kHz
Monitor the horizontal synchronizing signal input to SYNC IN (pin 44) and the pin 26 output (Hout) with an oscilloscope. Vary the frequency of the horizontal synchronizing signal and measure the pull-in range.
Measure the low-level period in the pin 26 horizontal pulse waveform.
Measure the low-level period in the pin 26 horizontal pulse waveform.
Measure the low-level period in the pin 26 horizontal pulse waveform.
Measure the low-level period in the pin 26 horizontal pulse waveform.
Measure the voltage during low-level period in the pin 26 horizontal pulse waveform.
Measure the delay time from the rise of the pin 26 horizontal output pulse waveform to the fall of the SYNC IN horizontal synchronizing signal.
HDUTY: 00
HDUTY: 01
HDUTY: 11
44
26
44
26
26
26
26
26
26
44
Horizontal output
Continued on next page.
HPH
CEN
20 IRE
3.8V
A10075
Page 30
No. 5841-30/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus condition
Horizontal position adjustment range
Maximum horizontal position adjustment variability
X-ray protection circuit operating voltage
POR circuit operating voltage
[Vertical Screen Size Adjustment]
Vertical ramp output amplitude @64
HPHrange
HPHstep
VX
RAY
V
POR
Vsize64
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
Measure the delay time from the rise of the pin 26 horizontal output pulse to the fall of SYNC IN horizontal synchronizing signal with H
PHASE
set to both 0 and 15 and calculate the difference with respect to HPH
CEN
.
Measure the delay time from the rise of the pin 26 horizontal output pulse to the fall of SYNC IN horizontal synchronizing signal while varying H
PHASE
from 0 to 15, and measure the amount of variation at each step. Find the step with the largest value of the data.
Connect a DC voltage source to pin 28, and gradually increase that voltage starting at 0 V. Measure the pin 28 DC voltage at the point the pin 26 horizontal output pulse stops.
Replace the current source connected to pin 24 with a DC voltage source, and gradually decrease the voltage starting at 7.3 V. Measure the pin 24 DC voltage at the point the pin 26 horizontal output pulse stops.
Monitor the pin 19 vertical ramp output and measure the voltages at the 22nd line and at the 262nd line. Calculate the following formula. Vsize64 = Vline262 – Vline22
H
PHASE
: 0000
H
PHASE
: 1111
H
PHASE
: 0000
to
H
PHASE
: 1111
26 44
26 44
26 28
26
19
Measurement
20 IRE
A10077
A10078
262nd line
24
Continued on next page.
Horizontal output
Measurement
Horizontal output
22nd line
Vertical ramp output
20 IRE
3.8V
A10076
Page 31
No. 5841-31/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus condition
Vertical ramp output amplitude @0
Vertical ramp output amplitude @127
Vertical size correction @7 (maximum)
Vertical ramp DC voltage @32
Vertical ramp DC voltage @0
Vsize0
Vsize127
Vsizecomp
Vdc32
Vdc0
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
Monitor the pin 19 vertical ramp output and measure the voltages at the 22nd line and at the 262nd line. Calculate the following formula. Vsize0 = Vline262 – Vline22
Monitor the pin 19 vertical ramp output and measure the voltages at the 22nd line and at the 262nd line. Calculate the following formula. Vsize0 = Vline262 – Vline22
Monitor the pin 19 vertical ramp output and measure the voltages at the 22nd line and at the 262nd line. Calculate Va from the following formula. Va = Vline262 – Vline22 Next, apply 3.8 V to pin 18, and once again measure the voltages at the 22nd line and at the 262nd line. Calculate Vb from the following formula. Vb = Vline262 – Vline22 Finally, calculate Vsizecomp from the following formula. Vsizecomp = (Va – Vb)/Va × 100
Monitor the pin 19 vertical ramp output and measure the voltage at the 142nd line.
Monitor the pin 19 vertical ramp output and measure the voltage at the 142nd line.
V
SIZE
: 0000000
V
SIZE
: 1111111
V
COMP
: 111
V
DC
: 000000
19
19
19
19
19
[High-Voltage Dependency Vertical Size Correction]
[Vertical Screen Position Adjustment]
Continued on next page.
262nd line
22nd line
Vertical ramp output
262nd line
22nd line
Vertical ramp output
142nd line
Vertical ramp output
Vertical ramp output
142nd line
A10079
A10080
A10081
A10082
Page 32
No. 5841-32/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus condition
Vertical ramp DC voltage @63
Vertical linearity @8
Vertical linearity @0
Vertical linearity @15
Vdc63
Vlin8
Vlin0
Vlin15
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
Monitor the pin 19 vertical ramp output and measure the voltage at the 142nd line.
Monitor the pin 19 vertical ramp output and measure the voltages at the 22nd line, the 142nd line, and the 262nd line. Let Va, Vb, and Vc be these measurements, and calculate the following formula. Vline8 = (Vb – Va)/(Vc – Va)
Monitor the pin 19 vertical ramp output and measure the voltages at the 22nd line, the 142nd line, and the 262nd line. Let Va, Vb, and Vc be these measurements, and calculate the following formula. Vline0 = (Vb – Va)/(Vc – Va)
Monitor the pin 19 vertical ramp output and measure the voltages at the 22nd line, the 142nd line, and the 262nd line. Let Va, Vb, and Vc be these measurements, and calculate the following formula. Vline15 = (Vb – Va)/(Vc – Va)
V
DC
: 111111
VLIN: 0000
VLIN: 1111
19
19
19
19
Continued on next page.
Vertical ramp output
142nd line
Vertical ramp output
142nd line
262nd line
22nd line
Vertical ramp output
142nd line
262nd line
22nd line
Vertical ramp output
142nd line
262nd line
22nd line
A10083
A10084
A10085
A10086
Page 33
No. 5841-33/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus condition
Vertical S-curve correction @8
Vertical S-curve correction @0
Vertical S-curve correction @15
VScor8
VScor0
VScor15
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
Monitor the pin 19 vertical ramp output and measure the voltages at the 32nd line, the 52nd line, the 132nd line, the 152nd line, the 232nd line, and the 252nd line. Let Va, Vb, Vc, Vd, Ve, and Vf be these measurements, and calculate the following formula. VScor8 = 0.5[(Vb – Va) + (Vf – Ve)] / (Vd – Vc)
Monitor the pin 19 vertical ramp output and measure the voltages at the 32nd line, the 52nd line, the 132nd line, the 152nd line, the 232nd line, and the 252nd line. Let Va, Vb, Vc, Vd, Ve, and Vf be these measurements, and calculate the following formula. VScor0 = 0.5[(Vb – Va) + (Vf – Ve)] / (Vd – Vc)
Monitor the pin 19 vertical ramp output and measure the voltages at the 32nd line, the 52nd line, the 132nd line, the 152nd line, the 232nd line, and the 252nd line. Let Va, Vb, Vc, Vd, Ve, and Vf be these measurements, and calculate the following formula. VScor15 = 0.5[(Vb – Va) + (Vf – Ve)] / (Vd – Vc)
VS: 1000
VS: 1111
19
19
19
Continued on next page.
Vertical ramp output
252nd line
232nd line
152nd line
132nd line
52nd line
32nd line
Vertical ramp output
252nd line
232nd line
152nd line
132nd line
52nd line
32nd line
Vertical ramp output
252nd line
232nd line
152nd line
132nd line
52nd line
32nd line
A10087
A10088
A10089
Page 34
No. 5841-34/39
LA7615
Parameter Symbol
Test point
Input signal Test procedure Bus condition
[Horizontal Size Adjustment]
East/west DC voltage @16
East/west DC voltage @0
East/west DC voltage @31
East/west parabola amplitude @8
East/west parabola amplitude @0
EWdc16
EWdc0
EWdc31
EWamp8
EWamp0
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltage at the 142nd line.
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltage at the 142nd line.
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltage at the 142nd line.
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltages at the 22nd line and at the 142nd line. Let Va and Vb be these measurements, and calculate the following formula. EWamp8 = Vb – Va
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltages at the 22nd line and at the 142nd line. Let Va and Vb be these measurements, and calculate the following formula. EWamp0 = Vb – Va
EW
DC
: 00000
EW
DC
: 11111
EW
AMP
: 0000
21
21
21
21
21
East/west output
A10091
A10092
A10093
A10094
[Pin-Cushion Distortion Correction]
Continued on next page.
142nd line
East/west output
142nd line
East/west output
142nd line
East/west output
142nd line
22nd line
East/west output
142nd line
22nd line
A10090
Page 35
No. 5841-35/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus condition
East/west parabola amplitude @15
East/west parabola tilt @8
East/west parabola tilt @0
East/west parabola tilt @15
EWamp15
EWtilt8
EWtilt0
EWtilt15
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltages at the 22nd line and at the 142nd line. Let Va and Vb be these measurements, and calculate the following formula. EWamp15 = Vb – Va
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltages at the 22nd line and at the 262nd line. Let Va and Vb be these measurements, and calculate the following formula. EWamp8 = Va – Vb
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltages at the 22nd line and at the 262nd line. Let Va and Vb be these measurements, and calculate the following formula. EWtilt0 = Va – Vb
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltages at the 22nd line and at the 262nd line. Let Va and Vb be these measurements, and calculate the following formula. EWtilt15 = Va – Vb
EW
AMP
: 1111
EW
TILT
: 0000
EW
TILT
: 1111
21
21
21
21
[Trapezoidal Distortion Correction]
Continued on next page.
East/west output
142nd line
22nd line
East/west output
262nd line
22nd line
East/west output
262nd line
22nd line
East/west output
262nd line
22nd line
A10095
A10096
A10097
A10098
Page 36
No. 5841-36/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus condition
[Corner Distortion Correction]
East/west parabola corner: Top
East/west parabola corner: Bottom
[Sandcastle Output]
Burst gate pulse peak value
Burst gate pulse phase
Burst gate pulse width
EWcortop
EWcorbot
V
BGP
Td
BGP
PW
BGP
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
SYNC IN: horizontal and vertical synchronizing signal
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltage at the 22nd line under the conditions with COR
TOP
set to 111 and to 000. Let Va and Vb be these measurements. Calculate the following formula. EWcortop = Va – Vb
Monitor the pin 21 east/west output (parabola waveform output) and measure the voltage at the 262nd line under the conditions with COR
BOT
set to 111 and to 000. Let Va and Vb be these measurements. Calculate the following formula. EWcorbot = Va – Vb
Measure the pin 29 output burst gate pulse peak value.
Measure the delay time from the rise of the horizontal synchronizing signal to the rise of the pin 29 burst gate pulse.
Measure the width of the pin 29 burst gate pulse.
CORT
OP
: 111-000
CORBOTTOM:
111-000
21
21
29
29 44
29
Pin 29 output
TdBGP
BGP
A10102
Horizontal synchronizing signal
PWBGP
BGP
A10103
Continued on next page.
East/west output
22nd line
East/west output
262nd line
Pin 29 output
Pin 29 output
A10099
A10100
VBGP
BGP
A10101
Page 37
No. 5841-37/39
LA7615
Continued from preceding page.
Parameter Symbol
Test point
Input signal Test procedure Bus condition
Blanking pulse peak value
[D/A Converter Output] Pin 30 D/A converter output
voltage @0 Pin 30 D/A converter output
voltage @8 Pin 30 D/A converter output
voltage @15
V
BLK
V
DAC
0
V
DAC
8
V
DAC
15
SYNC IN: horizontal and vertical synchronizing signal
Measure the peak value of the pin 29 output blanking pulse.
Measure the pin 30 D/A converter output DC voltage.
Measure the pin 30 D/A converter output DC voltage.
Measure the pin 30 D/A converter output DC voltage.
+B
TRIM
: 0000
+B
TRIM
: 1111
29
30 30 30
Blanking pulse
Pin 29 output
V
BLK
A10104
Page 38
No. 5841-38/39
LA7615
Test Circuit Diagram
1
FM
DISCRI
2
IF
V
CC
3
AUX
VIDEO
IN
4
RF
AGC
OUT
5
WB
AUDIO
OUT
6
PIF
APC
FILTER
7
IF
GND
8
PIF
IN1
VIF
IN
9
PIF
IN2
10
PIF
AGC1
11
PIF
AGC2
12
SIF
IN
13
SIF
AGC
14
AFT
OUT
15
CHROMA
APC
16
XTAL
17
VERT
V
CC
18
SIZE
COMP
19
VERT
OUT
20
RAMP
ALC
FILTER
21
E-W
OUT
22
HORIZ
RES
23
HORIZ
GND
24
STANDBY
V
CC
25
HORIZ
AFC
FILTER
26
HORIZ
OUT
39 38 37 36 35 34 33
FAST
SWITCH
IN
40
RED
IN
41
GRN
IN
42
BLU
IN
43
BLACK
LEVEL
DET
44
SYNC
IN
45
ADAPTIVE
CORING
46
SELECTED
Y
OUT
47
Y2
IN
48
C2
IN
49
CHROMA
KILLER
50
Y1
IN
51
C1
IN
52
TEST
IT
FILTER
53
SELECTED
VIDEO
OUT
54
BUS
CLOCK
55
BUS
DATA
56
VIDEO
OUT
57
EQ
FILTER
58
BUS
GND
59
SND
IF
OUT
60
FM
V
CC
61
SND
IF
IN
62
F0
FILTER
63
VCO
TANK2
64
VCO
TANK1
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
3 4 5 62
+
9 13
16 17 18
19 24
26
28
36
11 12 14
+
21 30 31
27
FLYBACK
BLU
OUT
+
3229
28
X
RAY
GRN
OUT
29
SAND
CASTLE
OUT
RED
OUT
30
DAC
OUT
BRT
ABL
FILT
31
IB
IN
CONTRAST
(PIX)
ABL
FILT
+
32
VID
CHROMA
V
CC
VID/
CHROMA
GND
43 5 6 7 821
1314 12 11 10 91516
LC4528B
373853
+
40
+
41
+
4246
+
47485455
+
5051 44 395660 5961
+
+
LA7615
A10105
R75
R76
3.9 k
1744
C118
C2
C1
C7
C6
C4
C8
C9
C3
C119
R1
R2
R5
R3
R7
R4
75
100
50 k
150
16
R10
820
R11
50
R12
R13
100 k
R16
3 k
R18
R26
6.2 k
1 k
3.3 k
10 k
10 k
1.8 k
16 pF
R15
R25
R27
R28
R36
CSB503F (44)
750
CHR1
R22
7.5 k
R17
C16
C117
C21
C23
C24
C26
C27
C29
R40
R42
R43
C34
C35
R41
C31
C28
C22
0.01 µF
0.01 µF
100 µF
10 µF
0.47 µF
10 µF
10 µF
1 µF
C36
C37
R46
R47
R48
R49
R51
R52
R53
R50
16 k
16 k
16 k
75
75
75
75
1100
1.5 µF
C39
C40
C41
C42
C44
R57
R56
560
C43
470 k
1 µF
C50
C45
C46
C47
C48
C49
C51
C55
C56
C58
C59
R74
50
R67
2.2 µF
1 µF
100 pF
10 µF
1 µF
0.01 µF
0.01 µF
1 µF
R60
R59
R61
R62
R62
R63
R64
R65
R68
R69
R70
R58
0.01 µF
1 µF
100 pF
100
75
75
15 k
2 k
15 k
100
75
75
100
100
24 k
100 pF
10 k
R54
680 k
22 µF
C38
1 µF
1 µF
1 µF
47 pF
1 µF
0.01 µF
0.033 µF
2.2 k
10 k
100 µF
0.01 µF
1 k
1 k
0.01 µF
470
R21
1.6 k
R14
100 k
R9
50
R8
68
R6
16
IF1
7.5 k
1T363
0.01 µF
0.01 µF
1 µF
0.01 µF
0.47 µF
0.01 µF
0.01 µF
C10
0.022 µF
C12
0.01 µF
C11
0.047 µF
C13
1 µF
C14
0.01 µF
C15
C17
C19
10 µF
0.033 µF
100 µF
1 µF
0.01 µF
100 k
+9 V
T101
M
+7.6 V
+7.6 V
+9 V
C25
+7.6 V
0.47 µF
*
+9 V
Tr1
V101
766-2
+7.6 V
+7.6 V
+7.6 V
R33
C22
R38
5 k
2200 pF
1 k
R32
8.2 k
C30
1500 pF
+7.6 V
NC
NC
R37R34
8.2 k5 k
+7.6 V
WIDTH (12US)
DELAY2
(9US)
+7.6 V
+7.6 V
+
7.6 V
C53
C52
100 pF
100 pF
L102
M
*: Used for adjusting the characteristics of the crystal oscillator.
(Includes two monostable multivibrators.)
Page 39
PS No. 5841-39/39
LA7615
This catalog provides information as of September, 1999. Specifications and information herein are subject to change without notice.
Specifications of any and all SANYO products described or contained herein stipulate the performance, characteristics, and functions of the described products in the independent state, and are not guarantees of the performance, characteristics, and functions of the described products as mounted in the customer’s products or equipment. To verify symptoms and states that cannot be evaluated in an independent device, the customer should always evaluate and test devices mounted in the customer’s products or equipment.
SANYO Electric Co., Ltd. strives to supply high-quality high-reliability products. However, any and all semiconductor products fail with some probability. It is possible that these probabilistic failures could give rise to accidents or events that could endanger human lives, that could give rise to smoke or fire, or that could cause damage to other property. When designing equipment, adopt safety measures so that these kinds of accidents or events cannot occur. Such measures include but are not limited to protective circuits and error prevention circuits for safe design, redundant design, and structural design.
In the event that any or all SANYO products (including technical data, services) described or contained herein are controlled under any of applicable local export control laws and regulations, such products must not be exported without obtaining the export license from the authorities concerned in accordance with the above law.
No part of this publication may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopying and recording, or any information storage or retrieval system, or otherwise, without the prior written permission of SANYO Electric Co., Ltd.
Any and all information described or contained herein are subject to change without notice due to product/technology improvement, etc. When designing equipment, refer to the “Delivery Specification” for the SANYO product that you intend to use.
Information (including circuit diagrams and circuit parameters) herein is for example only; it is not guaranteed for volume production. SANYO believes information herein is accurate and reliable, but no guarantees are made or implied regarding its use or any infringements of intellectual property rights or other rights of third parties.
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