Publ. nr. 2120 Dec. 66.
AB VOLVO PENTA
Compliments of the Privateer 26 Boatowners Association www.Privateer26.org
This Service Manual concerns Volvo Penta engines of the D1, MD1, D2 and MD2 types.
The instructions assume the use of certain special tools and since it is in your own interest as well as ours that repairs are properly carried out, we request you to study and carefully follow the instructions in this book.
We retain the right to carry out design modifications and for this reason the contents of this book are not to be considered binding.
AB VOLVO PENTA Technical Information Department
General 2 |
Description 2 |
General service work 4 |
Engine unit |
Description |
Cylinder head and valve system 5 |
Repair instructions |
Description, cylinder block and crankcase11 |
Repair instructions 11 |
Cylinder block 11 |
Pistons 12 |
Connecting rods |
Camshaft 15 |
Crankshaft |
Manual starter |
Lubricating system |
Description |
Repair instructions |
Lubricating oil nump |
Lubricating oil filter |
Eusificating off Interestion and an and a second se |
Fuel system |
Description 21 |
Repair instructions 21 |
Fuel injection pump 21 |
Injectors |
Fuel filter 25 |
Feed pump |
Centrifugal governor 27 |
Cooling system |
Description |
Repair instructions |
Reverse gear |
Description |
Repair instructions |
Specifications |
Tools |
Cut-away drawings |
Engines with type designations D1 and MD1 are one-cylinder, four-stroke Diesel engines with overhead valves. The total capacity is 445 c.c.
Engines with type designation D2 and MD2 are two-cylinder, four-stroke Diesel engines with overhead valves. The total capacity is 890 c.c.
MD1 and MD2 are marine Diesel engines. D1 and D2 are industrial Diesel engines. The combustion chambers in the engines are designed for direct fuel injection, this resulting in low fuel consumption, smooth running and immediate starting.
The engines are fitted with a manual or electric starter. A decompression device on the rocker arm cover facilitates starting.
The marine engines are sea-water cooled and the industrial engines are fitted with a cellular type radiator. A thermostat maintains the operating temperature of the engine automatically within the correct values.
The fuel system includes a filter with a replaceable element and is thus well protected from running interruptions. D2 and MD2 units are fitted with a feed pump.
Engine lubrication is through a pressure system where an oil pump supplies lubricating oil to all the points in the correct quantities at different speeds. The D2 and MD2 are fitted with a full flow oil filter. The big-end bearing shells are replaceable and are accessible through the oil sump crankcase covers. Major repair work can also be carried out through these covers.
The engines have closed circuit crankcase from getting out into the engine compartment. This device consists of a filter with connections and an oil trap located in the space above the valve tappets. Crankcase gases are then sucked directly into the engine induction manifold and into the cylinders.
Fig 1. MDl engine
Fig 4. D2 engine
All the repair instructions concern both one and two cylinder industrial and marine engines and these instructions should be applied according to the engine concerned.
A compression test is used to determine the condition of the engine in a simple and reliable way. The compression gauge is usually graduated in kg/cm2 or lb./sq.in.
The test is carried out by first running the engine warm and then removing the injectors and checking the compression on each cylinder in turn.
Move the speed control to the zero position or turn the fuel injection pump lever in a clockwise direction.
Engine with manual starter
Move the decompression handle so that it points upwards. Turn the engine over as fast as possible by using the starter crank and push down the decompression handle completely while continuing to turn the engine over.
Turn on the key switch. Then press the starter button. Make sure that the battery is in good enough condition to turn the engine over at 200-240 r.p.m. It is also important to ensure that the compression gauge connection is in good condition and that tightening is properly carried out if the test is to be reliable.
Compression pressure should normally be 21-24 kg/cm2 (300-340 lb./sq.in)
Level tube (fuel
Fig 5 Level control (Wilbär tube)
NOTE! It is absolutely useless to carry out this test without running the engine warm since engine temperature has two affects. To start with a warm engine rotates easier than a cold engine with its stiff oil. Secondly the compression value is higher when the engine runs easily and therefore rotates faster. The air expands due to this heat and produces higher pressure. With a higher initial temperature, the final temperature and therefore the pressure are also higher. Low compression pressure on cylinders indicates worn cylinders and piston rings.
If the compression pressure in one of the cylinders is lower, this can depend either on leaking valves, broken piston rings or a blown cylinder head gasket.
It is important that the fuel always has sufficiently high pressure when it is fed to the fuel injection pump and feed pressure should therefore be checked if engine output decreases or there is reason to suspect a blocked fuel filter.
Feed pressure is checked by using a pressure gauge which is attached to the air-venting screw on the fuel filter. While testing the engine should run at a speed slightly above idling. After the pump has been operating for some time, read off the pressure gauge. The pressure should be about 0.5 kg/cm2 (7 lb./sq.in.). The pressure should not be less than 0.1 kg/cm2 (1.4 lb./sq.in.) if the pump is to feed the injection pump under all conditions and also circulate the fuel in the system to eliminate air. If the feed pressure is too low, check the following possible causes in the given order.
The injection angle is checked by using a Wilbär tube and tool no. 884057. On D2 and MD2 engines, the test is carried out on the cylinder nearest the timing gear casing.
Fig 6. Cylinder head and valves
The cylinder heads, one for each cylinder, are made of special-alloy cast-iron with high heat resistance.
The injectors are fitted in thin copper sleeves directly flushed by the coolant. This design ensures effective cooling of the injectors.
The valves, rocker arms and rocker arm shaft are located in the cylinder head. Each cylinder head is fitted with a rocker arm shaft carried in a bearing bracket.
The overhead valves are fitted in the cylinder head and are actuated by the camshaft through tappets, push rods and rocker arms
The valves operate in replaceable valve guides. The clearance between the valve and the rocker arm is set by means of adjusting screws in the rocker arms.
A decompression device is incorporated in the rocker arm covers to make possible manual starting.
The rocker arms are lubricated by an oil pipe which is connected to the lubricating oil pump.
Insert puller no. 884081 in the injector sleeve until it bottoms with the yoke tubes over the stud bolts.
Fig 7. Removing the injector sleeve.
Fig 8. Pressing in the injector sleeve
Fig. 10 Adjusting the sleeve
To measure valve guide wear, fit a new valve in the guide and then measure the clearance with an indicator as shown in Fig. 11. See the specifications for wear tolerances. If these tolerances are exceeded, replace the valve guides.
Fig. 11. Checking valve guide wear.
guides.
Before starting grinding work, replace and ream the valve guides if the wear tolerances have been exceeded.
Reaming should be carried out manually but a Vibrocentric machine and grinding stones can also be used. The grinding stones are located by a self-centring pilot spindle which is fitted in the valve guides. Through the self-centring property of this pilot spindle, the work is always carried out correctly in relation to the centreline of the valve guide. To obtain the best possible result, make sure that the grinding stones are always dressed to ensure the correct angle.
Another point which is not to be neglected is the tightening of the pilot spindle. It must be firmly in position since the grinding stone must work in a position which is absolutely at rightangles to the longitudinal axis of the valve.
Make sure that not too much material is ground off and also make sure that the correct form and a good mating surface are obtained by removing the smallest possible amount of material.
The grinding stone used should be an aluminium - oxide grindstone with ceramic binding agent. The stone is dressed and the angle checked in a dressing unit, Fig. 13, in which a diamond gives the stone the right angle and surface. The stone must have the same angle as the mating surface of the valve seat.
Fig. 13. Dressing the grinding stone.
If the valve disc sealing surfaces are burned or damaged in any other way, the valves must be machine-ground, see Fig. 14.
Fig. 14. Grinding a valve
The grinding disc should be an aluminium oxide disc with ceramic binding agent. The grinding machine is set at an angle of 45.5° for the exhaust and inlet valves. The mating surface must be ground as little as possible and only until it is "clean". If there is less than 1.0 mm (0.04") edge left on the valve disc, scrap the valve. Also scrap valves with distorted spindles.
After machine-grinding, the valve disc should be ground in against the valve seat with grinding compound such as "Carborundum". The valve is then checked for leakage in the following way:
Fit the valve without its spring in the cylinder head and pour a little fluid onto the top of the valve disc. Press the valve against the seat and blow carefully from below with compressed air. Do not blow so hard that the valve lifts from its seat. If the valve is not sealing properly, air bubbles will form round the valve disc, see Fig. 15.
Fig. 15. Checking a valve for leakage.
The valve springs are checked for straightness, length and tension. This is carried out in a spring tester, see Fig. 16. The valve springs must have the values shown in the specifications.
Fig. 16 Checking a valve spring.
The push rods should be straight throughout their entire length. This can be checked by using a faceplate. If the deviations are not too large, the push rods can be rectified by using a rubber faced mallet. Check the ball ends and ball sockets for damage.
The tappets are located in holes in the crankcase above the camshaft, and they actuate the valves through the push rods and rocker arms. The contact surface of the tappets against the camshaft must not be worn or cracked. Severe pitting cannot be approved, excessively loose tappets or tappets with damaged contact surfaces must be replaced.
Remove the lock rings from the rocker arm shaft and remove the rocker arms from the rocker arm shaft.
NOTE. The rocker arms are not identical. Mark them so that they are correctly re-fitted.
Clean the parts, being particularly careful with the rocker arm shaft oil drillings and also the rocker arm oil holes.
Fig. 17. Rocker arm mechanism
1. Bearing bracket
3. Locknut
Fig. 18. Replacing a rocker arm bushing.
If the pistons, cylinder head or cylinder block have been replaced, assembly must be carried out according to special instructions. (See "Adjusting the compression ratio").
After the cylinder head and cylinder block have been assembled, the valves are adjusted before the engine is started.
Fig. 19.
Fig. 20. Adjusting the valves.
Watch the valves while turning the crankshaft with the manual starter. When the inlet valve starts to open and the outlet valve closes, the O-mark on the flywheel is at the top as shown in Fig. 19. Then turn the crankshaft one more turn forward and adjust the valve clearance on this cylinder. Repeat the same procedure for the other cylinder.
With a warm engine, the clearance should be 0.30 mm (0.12") for the inlet value and 0.35 mm (0.014") for the exhaust value.
Since the pistons are designed with the combustion chamber in the piston crown, the pistons go so high against the valves that valve adjustment must never be carried out while the engine is running, since there is risk of the valves coming into contact with the piston and serious damage resulting.
Adjustment is carried out by means of a slotted screw which is secured by a locknut.
The degree to which the decompression device presses down the outlet valve must always be checked when valve clearance is checked. If the downward movement exceeds 0.5 mm (0.02') there is risk for piston damage.
Adjustment is carried out with the exhaust valve off-loaded. Remove the oil filler plug. Loosen the locknut and unscrew the adjusting screw. Then re-tighten the adjusting screw until it just reaches the rocker arm. Tighten the adjusting screw one further half turn corresponding to a downward movement of 0.5 mm (0.02"). Then tighten the locknut.
The engine cylinder block is fitted in the upper part of the crankcase. It is held in position by the cylinder head which is bolted to the crankcase by long stud bolts.
The cylinder block is made of cast-iron, on twocylinder engines the blocks are identical and interchangeable. The cylinders are surrounded by a cooling jacket. The crankcase is made of cast-iron and fitted with an inspection cover.
The connecting rods are made of drop-forged steel and are fitted at the top with a precisionmachined bushing which acts as a bearing for the gudgeon pin. The big-end bearing shells are precision-manufactured and replaceable. The bearing metal on them consists of indium-plated lead-bronze. The pistons are made of lightalloy and each has three compression rings and two oil control rings. The upper compression ring on each piston is chromed to reduce cylinder wear. The crown of each cylinder has a cardioid recess which is the combustion chamber.
The gudgeon pins make up the bearing unit for the pistons on the connecting rods. Due to the comparatively high pressure under which Diesel engines operate, the gudgeon pins must transfer considerable forces and this means that they must be constructed with particular care and made of the best material. The gudgeon pins are made of case-hardened steel. Casehardening gives the pins a very hard and durable surface layer at the same time as thecore retains its toughness, this ensuring resistance to fracture.
The crankshaft is made of forged steel, on D2 and MD2 engines it is carried in three main bearings fitted with replaceable bearing shells for the centre bearing and bushings for the end bearings. On D1 and MD1 engines the crankshaft is carried in two main bearings. The bearing consists of white metal. The rear main bearing is fitted with an axial washer to locate the crankshaft axially. At the flywheel there is a seal ring of rubber and inside this a labyrinth type seal.
After the block has been thoroughly cleaned and all deposits removed, make sure that all channels are free from dirt and deposits, and also that there are no cracks in the block.
The cylinder bore is subject to most wear at the upper part and it therefore becomes tapered. The cylinders also become out-of-round. To obtain a complete picture of the condition of the cylinders, measurement must therefore be carried out at several different points both laterally and longitudinally. Measurement is carried out by using a special cylinder bore indicator, Fig. 21.
The degree of wear decides the measures to be taken. If there are scratches or scoring in the cylinder walls or the wear exceeds the values stated in the specifications, re-boring should be carried out.
Fig. 21. Measuring cylinder bore wear.
Re-boring must be carried out with special machines. Since exceptionally severe demands are made on the result of this work, experience and skill are needed on the part of the mechanic carrying out the operation. It is essential for the bore to be round, cylindrical and at rightangles to the crankshaft within very close tolerances. The surfaces of the cylinder bore must also be finely machined to the greatest possible smoothness to ensure a short runningin time. We therefore recommend that this work is carried out by a specialized company.
After removing the piston rings and washing the pistons, examine the pistons to decide as to whether they are in such good condition so that they can be re-fitted.
Measurement is carried out by using a micrometer at right-angles to the gudgeon pin hole at the lower edge of the piston. See Fig. 22.
In a Diesel engine it is very important for the piston rings to be in good condition since they must seal against high pressure and withstand high temperatures.
The point at which piston ring replacement is carried out depends on oil consumption and the condition of the engine in general.
If the piston rings must be removed for one reason or another, they should always be replaced as a rule by new rings.
The fit of the piston rings must always be checked concerning ring gap and axial clearance in the piston ring groves. If the seal is to be "gas-tight", in addition to good contact against the cylinder bore, the rings must also provide a gas-tight seal against the ring groove in the piston as the piston moves up and down. This means that the rings must move freely in the grooves at all temperatures since they must follow the cylinder bore even when this has become worn.
Concerning piston ring gap and axial clearance, see the specifications on page 33.
Fig. 22. Measuring a piston.
If the pistons, cylinder block or cylinder head special way. (See "Adjusting the compression ratio").
fitted so that it is directly under the 4. Install and tighten the bearing caps. The
Fig. 25. Fitting the piston rings
Fig. 26. Piston ring location
Fig. 27. Gudgeon pin fit
Carry out a careful control after the connecting rods have been thoroughly cleaned. Fit new connecting rod bolts when reconditioning since they are subjected to great stresses. Check the connecting rod bushings, preferably using a gudgeon pin as gauge. There must be no noticeable looseness.
Before fitting check the connecting rods for straightness and distortion. Rectify if necessary. Checking and rectification is carried out in a special apparatus as follows:
Fig 28. Checking straightness
Fig. 29. Checking for distortion
If the pistons, cylinder block or cylinder head have been replaced, assembly is carried out a special way. (See "Adjusting the compression ratio").
When replacing pistons, cylinder head and cylinder block, the clearance between the piston and the cylinder head must be measured. If this is not done, there is risk for the engine labouring or not providing the right output.
7. Then measure the height difference between the downward projecting part of the cylinder head and the mating surface, see Fig. 31. This corresponds to "B" in Fig. 32. From the value "A" + 1.3, subtract "B". The resulting value should be 0.4 - 0.5 mm (0.016 - 0.020")
Try to be as near 0.4 mm as possible. Example: "A" = 2.5 mm and "B" = 3.5 mm
5.0 - 3.5 = 0.3 (tol. 0.4 - 0.5) 0.5 - 0.3 = 0.2
This means that a further 0.2 mm (0.008") shim must be fitted.
If it found that measurement "A" is so large that the clearance 0.4 - 0.5 mm cannot be obtained with an 0.2 mm shim the upper surface of the cylinder block must be ground. This work requires great precision and should be carried out by a specialized workshop.
Check the camshaft for wear on the bearing journals and cams. To ensure a smooth running engine after reconditioning, it is important to
pay special attention to the camshaft cams so that there is no uneven wear. In case of wear, replace the camshaft.
The bearings are pressed into their recesses and are line-bored after pressing in, so that camshaft bearing replacement can only be carried out when the engine is fully reconditioned.
When pressing in the bearings make sure that they are pressed in so that the oil holes index with the corresponding oil drillings in the block.
Concerning the cylinder head, cylinder block and pistons, see under these headings.
Fig. 33. Timing gear markings.
Fig. 34. Removing the gear.
Before inspecting, remove the centre bearing from the crankshaft. Then clean all the crankshaft drillings thoroughly. After this examine and measure the crankshaft. See the specifications on page 32.
Fig. 35. Crankcase and bearing cover sealing.
It is possible to grind the crankshaft to an undersize (see specifications). Use standard size main bearing bushings which are dimensioned to permit this.
The crankshaft is ground in a special machine and requires great precision. Have this work done by a special firm.
NOTE. If the camshaft gear is not removed, the axial washer and thrust washer are fitted on the crankshaft before it is pushed into position.
into the bearing housing so as not to damage the seal rings.
Fit the flywheel, cylinder block and cylinder head.
Fig. 37. Removing the flywheel.
If only the seal ring (5) and O-ring (6) are to be replaced, follow points 4,5,6 and 8. Removal of the ball bearing (7) is not necessary. Re-fit in the reverse order.
Before fitting clean all parts. Re-fit in reverse order. Before pressing the shaft into the housing, fill the space between the seal ring and ball bearing and the large space behind the ball bearing with heat-resistant grease.
Fig. 38. Lubricating system, D1 and MD1
4. Relief valve 5. Oil pump
The engines are fitted with complete pressure lubrication systems shown in Fig. 38 and 39. Pressure is produced by a wing type pump forcing oil through the drillings to the lubricating points. The pump is driven through a dog clutch from the camshaft.
Oil is sucked from the sump through the strainer and then forced past a relief valve in the pump which prevents excessively high oil pressure. The oil is then forced out to an oil gallery which feeds all the main, big-end and camshaft bearings as well as the valve mechanism. An oil pressure contact with a warning lamp or a pressure gauge is also included in the system so that oil pressure can be checked.
The pump is of the wing pump type, see Fig. 40. It is driven by a dog clutch from the camshaft. It sucks oil through a strainer and suction pipe and the oil is then fed by wings in contact with the pump housing. From the pressure side oil is fed through the filter to the various lubricating drillings. Oil pressure is limited by a relief valve in the pump. Oil pressure should be 1.5 - 2.5 kg/cm2 (20 - 35 lb./sq.in.).
The engine has a closed circuit crankcase breather and this prevents crankcase cases from com. 1g out into the engine compartment. This breather consists of a filter with connections and oil trap in the space above the tappets, see Fig. 41. Crankcase gases are sucked directly into the engine induction manifold and into the cylinders.
On D2 and MD2 engines there is an oil cleaner, see Fig. 42. A cleaner together with the insert and relief valve makes up one unit bolted to the crankcase. Replace after every 50 hours of operation and when changing the oil. With a new or reconditioned engine also change the cleaner for the first time after 20 hours of operation.
The strainer, of wire mesh, traps any large particles in the oil before the oil passes to the pump.
Fig. 39. Lubricating system, D2 and MD2
1. Pressure gauge (with manual starter) 2. Oil cleaner
6. Oil pump
4. Oil dipstick
Fig. 40. Lubricating oil pump
The strainer should be removed and cleaned after every 100 hours of operation.
Removing and disassembling
1. Loosen the three attaching bolts.
Fig. 41. Crankcase ventilation
Fig. 42. Oil cleaner.
Clean all parts thoroughly and check the housing, spindle and wings for scoring and wear. Scoring is not permissible.
After checking all parts, test the oil pump springs, i.e. the spring between the wings and the relief valve spring. See specifications for test figures.
Fig. 43. Removing the oil strainer
Fig. 44. Location of wings
Fig. 45. Removing the oil filter
The fuel system consists of the fuel pump with pre-filter (only D2 and MD2), the fuel injection pump with governor, injectors as well as pipe lines and fuel tank. Fuel is sucked by the feed pump from the fuel tank through the pre-filter and forced through the fuel filter to the injection
pump. On D1 and MD1 engines there is gravity feed from the fuel tank. This means that the fuel tank must be at least 150 mm (6") higher than the inlet on the engine fuel filter to obtain a gravity feed.
Fig. 46. Fuel system D1 and MD1
Fig. 47. Fuel system, D2 and MD2
THE GREATEST CLEANLINESS MUST BE OBSERVED IN ALL WORK ON THE FUEL SYSTEM AND ITS EQUIPMENT.
IRST
-> REMOJE INSPECTION COVER (* ABOVE) AND STUFF A "HAND TOWEL" SIZE RAG IN THE HOUSING UNDER NEITH THE PUMP -TO CATCH ANY PARTS THAT FALL PURING PUMP REMOVAL
NOTE. Repair work including adjustment to the internal pump components and which can alter their settings may only be carried out by authorized Diesel workshops with the required tools and test devices.
Fig. 48. Injection pump, Dl and MDl
between the pump flange and the timing gear casing. This measurement must agree if the injection angle is to be correct, Fig. 50.
Fig. 49. Injection pump, D2 and MD2
Figs. 48 and 49. Injection pump
1. | Delivery pipe | 7. | Roller tappet |
---|---|---|---|
2. | Spring | 8. | Spring |
3. | Off-loading valve | 9. | Control rod |
4. | Seal | 10. | Pump housing |
Fig. 50. Measuring the timing gear casing
If there is reason to believe that an injector is faulty, it should be removed from the engine and tested in a special apparatus.
Wash the injector until clean and fit in the test apparatus, see Fig. 52.
Fig. 51. Injector
Pump up the pressure until the injector needle opens and then read off the opening pressure. This varies depending on the type of injector. See the specifications on page 32.
The opening pressure can be adjusted by means of washers located between the upper spring retainer and the protective casing, see 10, Fig. 51. Remember that the spring retainer must be pulled right down to the bottom for each new test.
If these tests are satisfactory, the injectors should not be disassembled but should instead be re-fitted on the engine. If insatisfactory, disassemble, clean and adjust the injectors.
rong
Right
Fig. 53.
Fig. 54. Cleaning a nozzle needle
If the injector is to lie disassembled for some time, it should be kept in fuel oil. Finger prints can cause rusting which ruins the precision grinding work with which the parts are manufactured.
The nozzle and nozzle needle are matched together and should therefore not be mixed up with parts from other nozzles.
Fig. 55. Cleaning the pressure chamber
Fig. 56. Cleaning the nozzle chamber
Fig. 57. Cleaning the nozzle seat
Fig. 58. Cleaning the nozzle holes
The following points should be checked when inspecting injectors and cover most faults that may occur.
With the pressure gauge operating, pump fuel up to and out through the injector. The opening pressure varies due to the type of injector. See the specifications on page 32.
The setting is adjusted by using shims, 10, Fig. 51. If pressure is too low, fit more shims. If pressure is too high, remove one or more shims. Check the spray pattern as already described.
Correctly fitted Surfaces (a) parallel
Wrongly fitted Surfaces (b) not parallel
See "Testing". Make sure that there is no leakage at any joint. When the opening pressure has been set, shut off the pressure gauge. Then press slowly down on the arm of the injector tester until the injector opens. At this point the test oil should spray out in spurts with a "creaking" noise. The shorter the spurts are, the better the condition of the injector.
Fig. 60. Fuel filter.
Close the air-venting screw when there are no more air bubbles in the fuel oil.
53. Open the air-venting screw on the injection pump and repeat operation two above. Close the air-venting screw when there are no more air bubbles.
* See arrows below_
A feed pump is fitted only on D2 and MD2 engines, see 1, Fig 47, this being installed beside the injection pump and driven directly from the camshaft.
Fig. 61. Air-venting the fuel system
8. Lever 9. Lower pump housing 10. Diaphragm 11. Upper pump housing
7. Return spring
12. Gasket
The feed pump is fitted with a hand primer. This is used, for example after adjusting work. to pump fuel to the filter and injection pump. A pre-filter is incorporated in the feed pump housing.
Check the diaphragm and gasket for leakage and check the moving parts for wear. Remove damaged and worn parts.
1. Fit the leaf spring, Fig. 63, and the stop arm.
Tighten the screw, but only so hard that the leaf spring is in good contact with the pump housing.
Cleaning the strainer JOT ON MY ENCINE Loosen and remove the lid. Remove and blow clean the strainer. Check before fitting the lid that the gasket is in good condition and seals properly. Fit a new gasket if necessary. See Fig.
Fig. 64. Cleaning the strainer.
Fig. 65. Centrifugal governor
1. Injection pump
The governor on these engines is of the centrifugal type and gear-driven from the camshaft. The governor weights (11) are journalled on the gear (9, Fig. 65). The weights are connected by damping springs (8). When the governor rotates, the weights are thrown outwards by centrifugal force and displace the friction sleeve (12) axially. The sleeve exerts the pressure on the governor lever (14). The lever can twist relative to its spindle but this twisting is counteracted by a spring.
The control lever has two functions, to regulate speed and to stop the engine.
Since the lever tensions a spring (7) when it turns anti-clockwise, the governor lever is twisted and the injection pump rack (16) displaced so that the engine obtains maximum fuel
started, the injected quantity is controlled by the position of the weights. When the lever is moved in the opposite direction, spring tension decreases and engine speed decreases too. If the lever is turned further, the injection pump rack is taken by the governor lever to the stop position and the engine stops. Maximum turning is determined by an adjusting screw (13) which contacts a stop sleeve. Maximum engine speed is set with this screw.
The control lever (4) position determines engine speed. If the engine tends to increase its speed when the loading decreases, the governor weights are swung out more, the friction sleeve presses against the governor lever. This is then turned relative to the spindle without the governor lever moving since the spring is tensioned. The other arm of the governor lever then displaces the injection pump rack so that injected fuel decreases and engine speed goes down. When engine speed decreases, the governor weights move in again, the sleeve is pulled back and the governor lever is turned by the spring back to its original position.
The adjusting screw (15) determines the maximum fuel feed to the engine by stopping the governor lever movement. The adjusting screw is threaded into the rod on the cold starting button (2). When the rod is pressed down, the adjusting screw is displaced past the governor lever so that the arm instead rests against the cylindrical part of the rod whereby governor lever movement becomes greater. This also displaces the injection pump rack so that a larger fuel quantity than normal is supplied to the engine when starting.
When the engine starts, through the pressure exerted by the governor weights through the friction sleeve on the governor lever, this lever is moved back from the cold starting position and the cold starting rod is returned by a spring to its original position.
Fitting is carried out in the reverse order. Make sure that moving parts run easily and grease them 27
Fig. 66. Cooling system MD1
To provide effective cooling water circulation the engine is fitted with a sea-water pump. This pump is fitted on the timing gear casing and driven by the camshaft through a flange. Its function is shown in Fig. 66. The impeller in the sea-water pump is made of neoprene rubber and operates against a cam.
The pump (i. Fig. 66) sucks cooling water from outside the boat through the externally located sea-cock strainer and forces the water to the distribution housing (thermostat housing).
The cooling water has the possibility of following two ways from the distribution housing. The thermostat (2) in the thermostat housing keeps the passage from the engine closed at the same time as it opens the passage from the distribution housing above the thermostat. The water in the engine is therefore warmed up rapidly while the water supplied by the sea-water pump passes the engine through the bypass without cooling it.
When the engine has obtained its normal operating temperature, the thermostat opens the outlet from the engine at the same time as it closes the bypass line from the distribution housing above the thermostat.
In this way the thermostat balances cooling water circulation through the engine so that engine temperature is always correct independent of loading.
D1 and D2 engines are fitted with cellular radiators of the pressure type. Coolant is sucked by the pump from the bottom of the radiator and coolant is taken through drillings to the cylinder block and cylinder head. The flow of coolant is the valve seats and the cylinders. When the engine has attained its normal operating temperature, the thermostat opens.
Fig. 67. Cooling system, D2
Fig. 68. Sea-water pump
If the bearings are also to be replaced, carry out the following.
Clean all component parts and always replace the seal ring (7) if the pump has been disassembled.
On the MD1 the thermostat is located in the cylinder head and on the MD2 it is located in the exhaust manifold.
On the D1 the thermostat is located in the cylinder head behind the cooling water pump. On the D2 it is located in the exhaust manifold.
If the thermostat is fully open or has any other defect, fit a new thermostat. Fit in the reverse order.
Fig. 69. Cooling water pump.
The Volvo Penta type RB reduction - reverse gear has a built-in reduction gear with ratio 1.87:1. Engagement of "ahead" or "astern" is carried out by self-adjusting cones which are retained in the engaged position by the propeller pressure. The reverse gear and engine have the same lubricating system.
When "ahead" is engaged, the outgoing shaft with its cone is moved forward and engagement occurs against the front cone. Engine driving power is transmitted from the crankshaft gear to the internally toothed ring on the front cone.
When "astern" is engaged, the outgoing shaft is moved backwards and engagement occurs against the inner cone. This functions through an idler gear and this means that the direction of rotation of the outgoing shaft is therefore reversed.
Fig. 70. Reduction - reverse gear
"Ahead" = Thick unbroken black line "Astern" = Thick black broken line P = Propeller pressure
Before re-fitting the reverse gear, clean all parts carefully. Inspect all the parts and replace all worn units (washers, O-ring, spring washers). Check the seal rings carefully for damage. Wear on the friction facing on the gear (16), which is most subjected to wear. is compensated by increasing the thickness of the shims (24) as
Place the cone (10) in the gear (16) and measure "X", see Fig. 69. The difference between "X" and 85 mm decides the thickness of shims. If the measurement, for example, is 83 mm, fit a washer with a thickness of 2 mm. If wear is so great that "X" is less than 81 mm, the worn parts must be replaced. The friction facing in the gear and the cone are not replaceable.
Fig. 71. Rear section of reverse gear
If the flange is fitted so that the projecting side is turned forwards, this reduces the movement of the reverse gear lever from "ahead" to neutral. If the pin is given a half turn so that the projecting side faces rear wards, the movement of the lever from neutral to "astern" is reduced.
Then check that the reverse gear engages in both "ahead" and "astern".
The clutch mechanism can be placed in different positions with the shaft straight up, to port or starboard. Modification is carried out as follows:
If the keyway is in such a position after adjustment that the reverse gear lever cannot be fitted, turn the shaft and the flange as follows. There is a keyway on the shaft so both the gear retainer and shaft must be turned.
The output of the D1 which has been increased on two occasions means that the specifications have been divided up into 5, 6 and 7 h.p. at certain places.
From 5 to 6 h.p.: | From 6 to 7 h.p.: | |
---|---|---|
MD1, specification 9331 with effect from engine
number 2554 MD1, specification 9382 with effect from engine number 2599 D1, Specification 9399 with effect from engine number 2629 D1, specification 9410 with effect from engine number 2639 |
D1 and MD1 with effect |
from engine number
10366-10385 10398-10400 10407-10408 10422-10423 10426-10428 10431 onwards. |
ENGINE | ||
GENERAL | ||
Type designation
Output, h.p. at r.p.m. Number of cylinders. Bore Stroke Capacity Compression ratio Compression pressure, kg/cm 2 (lb./sq.in.) at r.p.m. |
D1, MD1
5/2000 6/2000 7/2300 1 79.37 mm (3.125") 90 mm (3.54") 445 c.c. 17.5:1 21 - 24 (300 - 340)/200 - 240 |
D2, MD2
15.5/2300 2 79.37 mm (3.125") 90 mm (3.54") 890 c.c. 17.5:1 21 - 24 (30° - 340)/ 200 - 24 |
Direction of rotation
Maximum engine speed, r.p.m Idling speed, r.p.m. |
Clockwise
2300 500-600, 400-500, 400-500 |
Clockwise
2300 400-500 |
CILINDERS | 17111 | |
Material
Cylinder bore standard 0.02" oversize 0.04" oversize PISTONS |
Cast-1
79.37 79.88 80.39 |
mm (3.125'')
mm (3.145'') mm (3.165'') |
Material
Height, total. Height from gudgeon pin centre to piston top Piston clearance in cylinder SoRRECTION : |
AMMENDED: |
alloy
m (4.06") (2.56") 0.09 mm (0.0028" - 0.028 - 0.00(3") 0.0035") |
Pistons available as:
Standard 0.02" oversize 0.04" oversize |
79.28
79.79 80.30 |
mm (3.121")
mm (3.141") mm (3.161") |
PISTON KINGS | ||
Compression rings
Oil control rings The upper compression ring on each cylinder is chromed. Piston rings available as: |
2 | |
Standard
0.02" oversize |
~ |
* Conection Page 32, Pistons sheet Pages:
32
e - | Reads: | Piston clearance in cylinder | 0,07 - 0,09 mm (0.0028-0.0035") |
---|---|---|---|
Should read: | Piston clearance in cylinder | 0,07 - 0,11 mm (0.0028-0.0043") |
Reads: | Big end bearing radial clearance | 0.079 - 0.114 (0.0031-0.0045") |
---|---|---|
Should read: | Big end bearing radial clearance | 0.066 - 0.098 (0.0026-0.0039") |
D1, MD1 DZ, MD2 | |
---|---|
· | |
Piston ring clearance in groove, axially: | |
lst compression ring |
0.069-0.097 mm (0.0027''-0.0038'')
0.069-0.097 mm (0.0027''-0.0038') |
3rd " | 0.054-0.082 mm (0.0021''-0.0032'') |
lst oil control ring | 0.033-0.063 mm (0.0013''-0.0025'') |
Piston ring gap in cylinder | 0.25 - 0.50 mm (0.01 - 0.02'') |
CYLINDER HEAD | A set of the |
Material
Tightening torque |
Special-alloy cast-iron
See heading "Tightening torque" |
CRANKSHAFT AND BEARINGS | |
Crankshaft axial clearance
Main bearing radial clearance |
0.08 - 0.18 mm (0.003 - 0.007")
0.038 -0.109 mm (0.0015 0.0043") |
See heading "lightening torque" | |
BIG-END BEARING JOURNALS SHOULD | READ = 0.066-0.098 MM (0.0026-0.0039") |
Big-end bearing radial clearance CC2PECTICN= | AMMENDED 0.079-0.114 mm (0.0031-0.0045'') |
Diameter, standard | 53.950-53.960 mm (2.1240-2.1244") |
0.010" undersize | 53.696-53.706 mm (2.1140-2.1144'') |
0.030" undersize |
53. 442-53. 452 mm (2. 1040-2. 1044'')
53. 188-53. 198 mm (2. 0940-2. 0944'') |
BIG END BEARING SHELLS | |
Thickness standard | 1 384-1 391 mm (0.0545.0.05481) |
0.010" undersize | 1.511-1.518 mm (0.0595-0.0598'') |
0.020" undersize | 1.638-1.645 mm (0.0645-0.0648") |
1.765-1.772 mm (0.0695-0.0698") | |
MAIN BEARING JOURNALS | |
Diameter, standard
Diameter, undersize |
66.645-66.665 mm (2.6238-2.6246'')
66.445-66.465 mm (2.6159-2.6167'') |
GUDGEON PINS | |
Diameter
Gudgeon pin bushing, diameter Clearance, gudgeon pin - bushing |
28.00-28.004 mm (1.1024-1.1025")
28.014-28.025 mm (1.1029-1.1033") Close running fit |
CONNECTING RODS | |
bearing shells. | |
Axial clearance at crankshaft | 0.05 0.25 mm (0.002'' - 0.010'') |
Tightening torque | See heading "Tightening torque. |
CAMSHAF T | |
Drive | Gear |
Radial clearance | 0.025 - 0.076 mm (0.002' - 0.003'') |
VALVE SYSTEM | |
Inlet | |
Disc diameter | 32 mm (1.26") |
Spindle diameter | 7.857 - 7.877 mm (0.3093'- 0.3101'') |
Seat angle in cylinder head | 450 |
Clearance, warm engine | 0.30 mm (0.012") |
EXHAUST | |
Disc diameter | 32 mm (1.26") |
Spindle diameter | 7.830 - 7.845 mm (0.3083'' - 0.3088'') |
Seat angle in cylinder head | 450 |
Clearance, warm engine | 0.35 mm (0.014") |
DECOMPRESSION DEVICE | |
Maximum depression of exhaust valve | 0.5 mm (0.020") |
Length, inlet valve guide
Length, exhaust valve guide Inner diameter, inlet Inner diameter, exhaust |
---|
Clearance, valve spindle - guide
inlet valve exhaust valve |
VALVE SPRINGS |
Length, unloaded
with 30 ± 0.2 kg (66 ± 0.4 lb.) loading with 56 ± 0.2 kg (123 ± 0.4 lb.) loading |
LUBRICATING SYSTEM |
Oil capacity, excluding cleaner |
Oil capacity, including cleaner |
Oil grade
Viscosity between - 10°C (+ 15°F)and + 20°C (+ 70°F) |
Viscosity above + 20°C (+ 70°F)
Oil pressure, warm engine, idling speed, kg/cm 2 (lb./sq.in.) |
LUBRICATING OIL PUMP |
Type
Spring for relief valve: Length, unloaded Loaded with 2.5 + / 2 0.2 kg (5.5 + / 2 0.4 lb.) Loaded with 3.5 + / 2 0.2 kg (7.7 + / 2 0.4 lb.) Spring for oil pump wings: Length unloaded |
Loaded with 2 ± 0.2 kg (4.4 ± 0.4 lb.) |
FUEL SYSTEM |
Fuel injection pump, Bosch
Injector (nozzle holder), Bosch Injector (nozzle), Bosch Hole diameter |
Injector opening pressure, kg/cm
2
(lb./sq.m.)
Pre-injection angle |
Fuel injection pump, Bosch
Injector (nozzle holder), Bosch Injector (nozzle), Bosch Hole diameter |
Injector opening pressure, kg/cm
2
(lb./sq.in.)
Pre-injection angle |
Fuel injection pump, Bosch
Injector (nozzle holder), Bosch Injector (nozzle), Bosch Hole diameter |
Injector opening pressure, kg/cm
2
(lb./sq.in.)
Pre-injection angle |
FUEL FILTER |
Type
Filter insert FEED PUMP |
Type |
62 mm (2.44") 62 mm (2.44') 62 mm (2.44'') 7.905 - 7.927 mm (0.311'' - 0.312'') 7.905 - 7.927 mm (0.311'' - 0.312'') 21 mm (0.83") 0.028 - 0.070 mm (0.0011" - 0.0027") 0.060 - 0.097 mm (0.0024" - 0.0038") approx. 50 mm (2") 1.5 litres (D1 and MD1) , 3.0 litres (D2 and (1.3 Imp quarts = 1.6 US MD2) 2.6 Imp quarts = MD2 (2.9 Imp quarts = 3.4 US quarts) Service DS SAE 10 W SAE 20 1.5 - 2.5 (21-35) Wing pump 40 mm (1.57") 34 mm (1.34") 31.5 mm (1.24") 31 mm (1.22") 24.5 mm (0.96") PFR 1K65/264/11 PFR2K65/291/11 KBL52S58/4 DLLA150S164 DLLA 150S245 Three, 0.23 mm Three, 0.23 mm (0. 009") (0. 009") 135-140 (1720-1990) 25 - 280 135-140 (1920-1990) 25 - 28° PFR1K60/127/11 KBL52S42/4 DLLA150S120 Three, 0.25 mm (0. 0098" 175 (2485) 26° PFR1K65/264/11 DLLA150S245 (0.0098") 135-140 (1920-1990) 25 - 280 Bosch FJ/DW 2/3 • Bosch FJSJ 32 U7
Pierburg PE15246 Approx. 0.5 kg/cm2 (7 lb./sq.in.)
1.2 - 1.3 kg/cm2
D2, MD2
(17 - 18 lb./sq. in.) 3.5 litres (3.0 Imp quarts = 3.7 US quarts)
Wax thermostat 71°C (160°F) 89°C (193°F)
Bellows thermostat 75 - 78°C (167 - 173°F) 90°C (195°F)
Sea-water cooled
Bellows thermostat 62 - 67°C (144 - 153°F 78°C (173°F)
Volvo Penta RB 1.87:1 Same as engine Left hand thread
0.20 mm (0.008")
Main bearing journals: Permissible out - of round ..... Main bearing journals: Permissible taper ..... Big and bearing journals: Permissible out- of - round ..... Big-end bearing journals: Permissible taper ... Maximum axial clearance on crankshaft.....
Valve spindles, permissible wear | |||
---|---|---|---|
Permissible clearance between valve s | sp | indl | e |
and valve guide: | |||
Inlet valves | |||
Exhaust valves | |||
The valve disc edge must be at least . |
Bearing journals, | permissible | out - | of | - | round |
---|---|---|---|---|---|
with new bushings | |||||
Bushings, permis | sible wear |
Cylinder head nuts |
---|
Centre bearing |
Crankshaft gear bolts |
Flywheel |
Connecting rod bolts |
Injectors |
Oil filter nipple |
Water pump flange |
Main bearing cover |
Bolt | for | clutch | half | ٠ | ٠ | ٠ | ٠ | ٠ | • | ٠ | ٠ | ٠ | ٠ | ٠ | ٠ | ٠ | ٠ | ٠ |
---|
0.06 mm (0.0024") 0.05 mm (0.0020") 0.06 mm (0.0024") 0.05 mm (0.0020") 0.35 mm (0.0140")
0.02 mm (0.0008")
0.15 mm (0.0060'') 0.17 mm (0.0067'') 1. 0 mm (0. 040'')
0.03 mm (0.0012") 0.05 mm (0.0020")
11 kgm (80 lb.ft.) 8 kgm (60 lb.ft.) 8 kgm (60 lb.ft.) 70 kgm (500 lb.ft.) 6.5 kgm (47 lb.ft.) 2 kgm (14 lb.ft.) 4 kgm (30 lb.ft.) 8 kgm (60 lb.ft.) 4.5 kgm (33 lb.ft.)
× .
14 kgm (100 lb. ft.)
art no. | Description |
---|---|
84047 | Cleaning tool for injectors |
84057 | Control tool for injection angle |
84077 | Drift for fitting copper sleeve |
84078 | Puller for flywheel and crankshaft gear |
84081 | Puller for copper sleeve |
84085 | Spreader tool for copper sleeve |
84200 | Holder for cleaning needle |
84201 | Cleaning needle for injector |
001450 | Drift for removing valve guide |
004129 | Reamer for valve guide |
994154 | Drift for removing and fitting rocker arm bushing |
004159 | Drift for fitting valve guide |
MD2 Engine
NOTES VOLVO PENTA ENGINE: MDI-445CC
PG 34 - FUEL FILTER - BOSCH # FJSJ 32 U7 *PG 25 - AIR VENTING THE FUEL FILTER AND SYSTEM PG 29 - WATER PUMP IMPELLER - # 875807 PG 34 - OIL TYPE AND AMOUNT - SAE 20 / 1.5 LITRES PG 35 - THERMOSTAT - BELLOWS 75° to 78°C (167-173°F)
CLEAN OIL SCREEN -
LUBRICATOR CUP (BEHIND WATER PUMP IMPELLER)
GOTEBORG SWEDEN