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.
0.42
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.
In case of venturi meter, at the diverging section mach number is less than 1. however in diverging section of a nozzle mach number is greater than 1.
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.
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.
The velocity of gaseous or other particles in the exhaust stream of the nozzle of a reaction engine, relative to the nozzle.
Find out who makes the engine and ask them
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.
The engine and nozzle and thrust vectoring systems
exhaust
rocket engine seems to be of this type. as the air-fuel mixture is burned and flame is made to propogate through nozzle to provide thrust