I am unsure what you are asking but:
The cooling oil nozzle is arraigned so the underside of the piston is sprayed with oil to cool the piston crown.
This is done on high stress engines as the pistons could and would overheat leading to detonation and other problems leading to engine failure.
This system is also used on Cumin's diesel engines as used in Dodge Trucks, race cars, heavy trucks and so on.
It is a little nozzle which is pointed towards the beneath of a piston in an internal combustion engine. It is linked to the pressurised side of the oil system, so cool oil coming directly from the oilcooler will spray onto the piston and cooling it instead of just cooling around the cylinder. This enables the engine to run a much more efficient combustion without the chance of melting a piston or overheating the engine which could lead to engine failure.
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The Wedco Nozzle is a CARB compliant spill-proof gas can nozzle. With the nozzle in place you can invert your gas can and it will not leak. Then simply push the nozzle lock and push the nozzle against the rim of the filling throat of the tank you're filling to start the flow of fuel. If you lift the nozzle away from the rim the flow stops.
in reaction turbine pressure compounding is employed as every stage has a set of nozzle ring nozzle control is not feasible.
a compressor does work on the gas , raising its pressure and temperaturea turbine does the reverse , it expands the gas as it passes through the turbine, extracting energy from the gas to do mechanical work.For a typical jet engine , the flow track on a compressor is of a converging cross section while is it diverging for the turbine, which is as per gas dynamic laws.The Turbine does two things here in the jet engine, one ,it runs the compressor and two, expands the gas to the propelling nozzle which produces thrust by accelerating the gas upto its exit.
aircraft powerplant consist of engine, plus inlet and exhaust nozzle.
It is a little nozzle which is pointed towards the beneath of a piston in an internal combustion engine. It is linked to the pressurised side of the oil system, so cool oil coming directly from the oilcooler will spray onto the piston and cooling it instead of just cooling around the cylinder. This enables the engine to run a much more efficient combustion without the chance of melting a piston or overheating the engine which could lead to engine failure.
the simplest engine that is made up of a burning chamber and a nozzle is a rocket.
Rocket engine.
The engine of an airplane creates thrust by accelerating air and expelling it at high speed through a nozzle at the back of the engine, according to Newton's third law of motion. This action propels the aircraft forward.
rocket engine
One means by which a nozzle can be forced to operate at maximum thrust or "on design" under many different flight conditions is through a.variable geometry. For such a nozzle, the area of the exit, throat, or both is varied so that the optimum exit pressure can be obtained. Two nozzle shapes are usually used: a simple circular (iris) nozzle or a plug nozzle. Note that variable nozzles are typically not used on commercial aircraft because of the limited flight envelope -that is, the craft and engine basically are optimally designed for one altitude and flight condition. Military fighters, on the other hand, must be designed to operate under a variety of conditions, including aircraft carrier takeoff. As a result, most of these engines have variable nozzles.
Air intake and exhaust. Air comes into the intake located at the front of the aircraft and exits at the rear of the aircraft. This is such a load of crap! A jet pipe is located at the back of an engine, just after the exhaust! It is connected with a gas tight sealing ring and just before the propelling nozzle. And pipes the exhaust gasses out of the fuselage/Wing... A/C engineer.
Find out who makes the engine and ask them
A jet engine works on the principle of conservation of momentum. Bernoulli's Principal is the basis for jet propulsion. It states that pressure in a tube remains the same unless the tube expands in size (divergent) or contracts (convergent). A gas that is forced from a larger to smaller will be low pressure on the larger side of the constriction and high velocity at the other. the reverse is true if you switch things around. This does for the jet engine what the pistons do for a reciprocating engine. Two easy examples of this principal would be 1. a balloon let go fly and 2. a garden hose spray nozzle.
The engine and nozzle and thrust vectoring systems
exhaust