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2. Air-blast injection - Wikipedia

   en.wikipedia.org/wiki/Air-blast_injection

   Unlike modern designs, air-blast injected Diesel engines do not have an injection pump. A simple low-pressure fuel-feed-pump is used instead to supply the injection nozzle with fuel. At injection, a blast of compressed air presses the fuel into the combustion chamber, hence the name air-blast injection. The compressed air comes from compressed ...

3. Gasoline pump - Wikipedia

   en.wikipedia.org/wiki/Gasoline_pump

   A gasoline pump or fuel dispenser is a machine at a filling station that is used to pump gasoline (petrol), diesel, or other types of liquid fuel into vehicles. Gasoline pumps are also known as bowsers or petrol bowsers (in Australia and South Africa ), [ 2 ] [ 3 ] petrol pumps (in Commonwealth countries), or gas pumps (in North America ).

4. Pintle injector - Wikipedia

   en.wikipedia.org/wiki/Pintle_injector

   This radiatively-cooled engine weighed 0.3 lb (135 grams) and was successfully tested in August 1993, delivering over 300 seconds I sp with a 150:1 nozzle expansion ratio. The pintle diameter was (1.6764 mm) and scanning electron microscopy was needed to verify the dimensions on the ± (0.0762 mm ±0.00762 mm) radial metering orifices. [2]

5. List of Isuzu engines - Wikipedia

   en.wikipedia.org/wiki/List_of_Isuzu_engines

   The early version used 5-hole injector nozzles, the latest has 7-hole injector nozzles for better emissions and fuel economy. 79 mm (3.1 in) 86 mm (3.4 in) 1,686 cc (102.9 cu in) 74 kW (101 PS) 16 Valve DOHC A17DTL A17DTN After the ISUZU Polska factory went under full GM ownership, the engine marking changed to A17.

6. Spray (liquid drop) - Wikipedia

   en.wikipedia.org/wiki/Spray_(liquid_drop)

   Examples include fuel injectors for gasoline and diesel engines, atomizers for jet engines (gas turbines), [12] atomizers for injecting heavy fuel oil into combustion air in steam boiler injectors, and rocket engine injectors. Drop size is critical because the large surface area of a finely atomized spray enhances fuel evaporation rate.

7. Propelling nozzle - Wikipedia

   en.wikipedia.org/wiki/Propelling_nozzle

   Beyond this point the nozzle diameter becomes the biggest diameter and starts to incur increasing drag. Nozzles are thus limited to the installation size and the loss in thrust incurred is a trade off with other considerations such as lower drag, less weight. Examples are the F-16 at Mach 2.0 [21] and the XB-70 at Mach 3.0. [22]