Eaton Aeroquip Rynglok Fitting System Installation Manual

Aeroquip
Rynglok
®
®
Fittings
Rynglok
Fitting System
Installation Guide
1.0 Initial Preparation .................................................................................... 3
1.1 Cutting Tubes
1.2 Tube End Preparation
1.2.1 Painted Tube End Preparation
1.3 Pre-applied Tube End Marking
1.4 Marking Gauge Positioning
2.0 Fitting Installation ................................................................................... 4
2.1 Positioning Mark
2.1.1 End Fittings
3.0 Fitting Assembly ..................................................................................... 5
3.1 Assembly Tool Selection
3.1.1 Assembly Tool/Fitting Compatibility
3.2 Assembly Tool Pressure Connection
3.3 Tool Installation
3.4 Tool Pressure
3.4.1 Pressure Level
4.0 Assembled Fitting Inspection ................................................................. 6
4.1 Ring Advancement Inspection
4.1.1 Insertion Inspection Mark Position
4.2 Shared Insertion - Unions
4.2.1 Over Insertion Condition - Fittings Other Than Unions
5.0 Tubing Repair With Rynglok Unions ........................................................ 7
5.1 Single Union Repair
5.1.1 Cutting Through Center Of Defect
5.1.2 Cutting Out Defect
5.2 Two Union Repair
6.0 Special Considerations ........................................................................... 8
6.1 Using The “Reversed Tool”
6.2 Special Considerations When Using The “Reversed Tool”
6.3 Special Considerations When Using The -20 and -24 Tools
7.0 Tube Cut Dimensions ............................................................................. 9
7.1 Female Arcseal™ Fitting
7.2 Female Flareless Fitting
7.3 Female Flared Fitting
8.0 Fitting Selection Chart ........................................................................10 – 11
2 EATON Aerospace Group TF100-67A March 2013
1.0 Initial Preparation
1.1 Cutting Tubes
Tubes may be cut using any appropriate cutting tool whether by hand or by a production method. Tube ends should be reasonably square, recognizing that any out-of-squareness condition will detract from the amount of positioning tolerance allowed. (See paragraph
1.4)
1.2 Tube End Preparation
The tube ends should be deburred with appropriate deburring tools on the O.D. and I.D. to prevent damage of the fitting I.D. during tube insertion and to prevent FOD (Foreign Object Damage) from entering and contaminating the fluid system.
1.2.1 Painted Tube End Preparation
Painted tube ends shall be deburred in accordance with paragraph
1.2. Painted tube ends do not require the paint to be removed when the tubing O.D. is in accordance with Table 1. The max. tubing O.D. (dim. A) must be held a min. distance (dim. B) per Table 1 for proper fitting installation. If paint removal is necessary, the tube shall be sanded in a radial direction using a mild grit paper. Care should be taken to prevent longitudinal marks. It will be necessary to reclean and remark tube ends. It is recommended to repaint the exposed tubing after installation. Please contact Eaton’s Jackson, MI facility at (517) 787-8121 if there are any questions regarding this procedure.
1.3 Pre-applied Tube End Marking
A pair or pairs of marks, (positioning marks and inspection marks) as shown in Figure 1, should be pre-applied with the given dimensions from Table 1 to each prepared tube end prior to fitting installation. A suitable method such as ink stamp, electro-etch, laser, etc. may be used. Should the tube ends be unmarked, the appropriate marks should be applied using Eaton’s Aeroquip brand tube marking gauge P/N RTSG0-01-SIZE as shown in Figure 2, and using a suitable per­manent ink felt tipped pen.
Notice: Due to the possibility of contaminating titanium tubing, inks which contain lead or free halogens should not be used for marking.
Table 1
Dimensions for electro-etch, ink stamp, or laser marking.
Dash Size
-03 .190 .453 .300 .453 .644
-04 .254 .525 .300 .525 .717
-05 .316 .588 .300 .588 .780
-06 .379 .656 .300 .656 .843
-07 .441 .730 .300 .730 .918
-08 .505 .773 .350 .773 .963
-09 .567 .836 .350 .836 1.026
-10 .630 .899 .350 .899 1.088
-11 .692 .983 .350 .983 1.175
-12 .755 1.042 .350 1.042 1.232
-13 .817 1.110 .350 1.110 1.303
-14 .880 1.178 .350 1.178 1.369
-15 .942 1.249 .400 1.249 1.448
-16 1.006 1.299 .400 1.299 1.498
-20 1.256 1.572 .400 1.572 1.781
-24 1.507 1.882 .400 1.862 2.086
A Max.
B Min.
C ± .005D ± .005E ± .005
Figure 1
Tube marking using electro-etch, ink stamp, or laser marking.
1.4 Marking Gauge Positioning
The RTSG0-01-SIZE series of marking gauges is common for all pressure classes of Rynglok fittings. The marking gauge should be bottomed on the end of the cut tube. If an out-of-square condition exists, the marking gauge should be positioned toward the end that is most square. This is only for fittings which require shared inser­tion, such as in the case of a union fitting. This allows minimum tube insertion on the opposite end of a union configuration should the skew end be inserted to the maximum tube insertion condition. (See paragraph 4.1.1 and Figure 7).
(All tubes should be marked prior to assembly in insure proper tube insertions.)
Figure 2
Application of tube insertion marks using RSTG0-01-SIZE marking gauge and pen.
EATON Aerospace Group TF100-67A March 2013 3
2.0 Fitting Installation
2.1 Positioning Mark
The installer must use this positioning mark to position the edge of the unswaged fitting “ring” over the marks as shown in Figure 3. The length of the positioning mark is the amount of positioning toler­ance allowed. The edge of the fitting “ring” may be anywhere along the length of the positioning mark.
Figure 3
Fitting position for tube insertion
2.1.1 End Fittings
In general, end fittings are designed to have the tube end bottomed into the fitting, and do not have as much positioning allowance. See Figure 5. Even with this condition, the tube end should be marked for inspection purposes to verify that the tube was inserted to at least the minimum insertion depth. Refer to section 7.0 when install­ing fittings of this type.
Figure 4
End fitting tube positioning. Note: Tube is bottomed into fitting.
4 EATON Aerospace Group TF100-67A March 2013
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