09180-00730 TIMER ASSY, AUTOMA Denso Cross


 

Information timer assy, automa

09180-00730 TIMER ASSY, AUTOMA
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Scheme ###:

000. [01] 09180-00730 TIMER ASSY, AUTOMA
000. [01] 09180-00730 TIMER ASSY, AUTOMA 22610-77052
001. [01] 09181-00761 HUB ASSY, TIMER
001. [01] 09181-00761 HUB ASSY, TIMER
002. [02] 09181-90590 SPRING, TIMER 90501-77052
002. [02] 09181-90590 SPRING, TIMER
003. [1C] 94901-33790 WASHER, PLATE, SK
003. [1C] 94901-33770 WASHER, PLATE, SK
003. [1C] 94901-33760 WASHER, PLATE, SK
003. [1C] 94901-33760 WASHER, PLATE, SK 22621-77020
003. [1C] 94901-33770 WASHER, PLATE, SK 22622-77020
003. [1C] 94901-33780 WASHER, PLATE, SK 22623-77020
003. [1C] 94901-33790 WASHER, PLATE, SK 22624-77020
003. [1C] 94901-33800 WASHER, PLATE, SK 22625-77020
003. [1C] 94901-33810 WASHER, PLATE, SK 90099-01442
003. [1C] 94901-33780 WASHER, PLATE, SK
003. [1C] 94901-33800 WASHER, PLATE, SK
003. [1C] 94901-33810 WASHER, PLATE, SK
004. [01] 94914-00010 O-RING
004. [01] 94914-00010 O-RING 90099-14001
005. [02] 09183-70011 WEIGHT, TIMER 22614-77020
005. [02] 09183-70011 WEIGHT, TIMER
006. [01] 09184-00411 FLANGE, TIMER DRIV 22613-77052
006. [01] 09184-00411 FLANGE, TIMER DRIV
007. [01] 94915-00080 SEAL, OIL 90099-15005
007. [01] 94915-00080 SEAL, OIL
008. [01] 94915-00070 SEAL, OIL 90099-15004
008. [01] 94915-00070 SEAL, OIL
009. [01] 09185-60172 COVER, TIMER
009. [01] 09185-60172 COVER, TIMER
010. [02] 94901-81020 WASHER, COPPER PLA 90201-08106
010. [02] 94901-81020 WASHER, COPPER PLA 90201-08106
011. [02] 09186-20010 SCREW, TIMER HUB
011. [02] 09186-20010 SCREW, TIMER HUB 22617-77020

Cross reference number



Part num Firm num Firm Name
09180-00730  22610-7705  TIMER ASSY, AUTOMA
22610-77052    TOYOTA TIMER ASSY, AUTOMA




Information:

Operation of ATAAC
Inlet air is pulled through the air cleaner, compressed and heated by the compressor wheel in the compressor side of the turbocharger to about 150°C (300°F). The heated air is then pushed through the air to air aftercooler core and moved to the air inlet manifold in the cylinder head at about 43°C (110°F).
Radiator Core (1) and Aftercooler Core (2).Cooling the inlet air increases combustion efficiency, which helps to lower fuel consumption and increase horsepower output. The aftercooler core (2) is a separate cooler core installed behind the standard radiator core (1). Ambient temperature is moved across both cores by the engine fan- this cools the turbocharged inlet air and the engine coolant.Lower inlet air temperature allows more air to enter the cylinder. More complete fuel combustion and reduced exhaust emissions are the results. Air-to-air aftercoolers can achieve charge air temperatures lower than water-to-air systems. The lower air temperatures provide improved efficiency.
To maintain an adequate water pump cavitation temperature for efficient water pump performance in an Air-to-Air Aftercooled engine: Caterpillar recommends that the coolant mix contain a minimum of 30 percent Caterpillar Antifreeze, or equivalent.
Air Inlet System
An air hose failure or a significant air inlet system leak will cause a large drop in boost pressure and power. The engine can be operated at this power level for a short period of time, however, sustained operation under this condition should be avoided.A slight reduction in power or response, or a small increase in exhaust temperature may indicate a small air leak in the charge air cooler core or piping.If air leaking is suspected, inspect the air inlet hoses, elbows and gaskets for cracks or damage. Replace the parts as needed. Check for loose clamps and tighten the clamps as needed.Radiator Restrictions
Caterpillar discourages the use of air flow restriction devices mounted in front of radiators with air-to-air aftercooled engines. Air flow restriction can cause higher exhaust temperatures, power loss, excessive fan usage, and a reduction in fuel economy.If an air flow restriction device must be used, the device should have a permanent opening directly in line with the fan hub. The device must have a minimum opening dimension of at least 770 cm2 (120 in2).A centered opening, directly in line with the fan hub, is specified to provide sensing when viscous fan drives are used and/or to prevent an interrupted air flow on the fan blades. Interrupted air flow on the fan blades could cause a fan failure.Caterpillar recommends that a package include an inlet manifold temperature device, such as a light indicator, buzzer, etc., set at 65°C (150°F) and/or installation of an inlet air temperature gauge. For the ATAAC (Air-To-Air Aftercooled) engines, air temperature in the inlet manifold should not exceed 65°C (150°F). Temperatures exceeding this limit can cause power loss and potential engine damage.This temperature provides engine protection for full restriction device closure. This temperature can also serve as a diagnostic tool for a malfunction of the charge air cooling system. It is not anticipated that

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