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On the front of the engine, under the intake manifold, behind the ac compressor.
Front of the engine, under the intake and behind the ac compressor.Front of the engine, under the intake and behind the ac compressor.
engine speed, engine load, coolant temp, throttle posision and intake manifold pressure
the engine is having high pressure inside the combustion chamber.the flow has to move trough nozzle.incase the pressure is very high at nozzle compared to the intake pressure the flow moves forward.then the compressors shape changed it is not enough to compress the intake air.it is compressor stall
when pressure increases in compressor side than turbine side in turbo then a waste gate is opened and allows the exhaust to bypass through exhaust pipe until both side pressure not comes equal. As the result intake pressure reduced.
A turbine is connected to a compressor with a shaft. When the hot exhaust gases flow through the turbine, it spins the compressor, which is connected to the air intake, adding pressure and airflow (or "boost") to the intake.
Commonly referred to as the heart of the system, the compressor is a belt driven pump that is fastened to the engine. It is responsible for compressing and transferring refrigerant gas. The a/c system is split into two sides, a high pressure side and a low pressure side; defined as discharge and suction. Since the compressor is basically a pump, it must have a intake side and a discharge side. The intake, or suction side, draws in refrigerant gas from the outlet of the evaporator. In some cases it does this via the accumulator.
IT IS LOCATED IN THE REAR OF THE INTAKE... YOU HAVE TO REMOVE THE INTAKE TO CHANGE IT....
Compressor stall and a wing stall are different and unrelated. Compressor stall refers to the compressor section of a jet engine. The compressor section is comprised of several spinning round discs attached to a shaft that runs through the engine. Blades attached to each disc compress the intake air, which is later mixed with fuel and burned in the combustion chamber. If the intake flow of air is disrupted, compressor stall can occur, allowing high pressure gasses to move forward through the engine, making a loud banging noise. Compressor stalls are usually momentary and do not cause any damage or significant reduction in power. A wing stalls when the angle between the chord of the wing and the relative wind becomes excessive and the airflow over the top of the wing is disrupted. The disruption results in a sudden loss of lift and the aircraft will descend and may become uncontrollable.
It is on the front of the engine, under the intake manifold and behind the ac compressor. either the intake or ac has to be removed to access.
A compressor is located between intake manifold and air filter.
Under the upper intake assembly