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  2. Oil burner - Wikipedia

    en.wikipedia.org/wiki/Oil_burner

    Used nozzles from an oil burner. Fuel is injected into the combustion chamber at high pressure by a spray nozzle. Fuel nozzles are usually rated in fuel volume flow per unit time e.g. US gallons per hour. A fuel nozzle is characterized by three features: Flow at 100 psi pump pressure (e.g. 0.65 gallons per hour)

  3. Spray nozzle - Wikipedia

    en.wikipedia.org/wiki/Spray_nozzle

    This type of spray nozzle may require more atomizing air and a higher atomizing air pressure drop because the mixing and atomization of liquid takes place outside the nozzle. The liquid pressure drop is lower for this type of nozzle, sometimes drawing liquid into the nozzle due to the suction caused by the atomizing air nozzles (siphon nozzle).

  4. Nozzle - Wikipedia

    en.wikipedia.org/wiki/Nozzle

    Convergent nozzles accelerate subsonic fluids. If the nozzle pressure ratio is high enough, then the flow will reach sonic velocity at the narrowest point (i.e. the nozzle throat). In this situation, the nozzle is said to be choked. Increasing the nozzle pressure ratio further will not increase the throat Mach number above one.

  5. Fuel injection - Wikipedia

    en.wikipedia.org/wiki/Fuel_injection

    The accumulator has a high-pressure relief valve to maintain pressure and return the excess fuel to the fuel tank. The fuel is sprayed with the help of a nozzle that is opened and closed with a solenoid-operated needle valve. [5]

  6. Rotary atomizers - Wikipedia

    en.wikipedia.org/wiki/Rotary_atomizers

    The devices using this method to achieve atomization are called as airblast, air-assist, or popularly twin-fluid atomizers. In a Rotary Atomizer, the rotating cup or disc forces the liquid to come out at a very high speed through its rim. [1] [2] The Rotary, Pressure-swirl [3] or Twin-fluid Atomizers [4] are the most common methods for spray ...

  7. Components of jet engines - Wikipedia

    en.wikipedia.org/wiki/Components_of_jet_engines

    Supersonic nozzle — For high nozzle pressure ratios (Nozzle Entry Pressure/Ambient Pressure) a convergent-divergent (de Laval) nozzle is used. The expansion to atmospheric pressure and supersonic gas velocity continues downstream of the throat and produces more thrust.