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As the RPM of the engine increases, the throttle plate in the carburetor is gradually closed, reducing the amount of fuel and air admitted to the engine, until the engine RPM is stable. If RPM drops below the desired value, the throttle plate will automatically open, admitting more fuel/air mix to the engine.
Data from QuickieBuilders and Western Canada Aviation Museum General characteristics Crew: one pilot Capacity: one passenger and 510 lb (231 kg) useful load Length: 19 ft 10 in (6.05 m) Wingspan: 16 ft 8 in (5.08 m) Height: 4 ft 5 in (1.35 m) Wing area: 67 sq ft (6.22 m 2) Empty weight: 490 lb (222 kg) Max takeoff weight: 1,000 lb (454 kg) Powerplant: 1 × Revmaster 2100-DQ converted auto ...
The M970 Semi-Trailer Refueler is a 5,000-U.S.-gallon (19,000 L; 4,200 imp gal) fuel dispensing tanker designed for under/overwing refueling of aircraft. It is equipped with a filter/separator, recirculation system and two refueling systems, one for underwing and one for overwing servicing.
The turbocharger has a compression ratio of 3.5:1 and the engine will have a critical altitude of 15,000 ft (4,572 m). It employs dual electronically controlled fuel injection, using dual channel Rockwell Collins ECUs, with dual ignition and produces 141 hp (105 kW) for take-off and 135 hp (101 kW) continuous. The engine can produce rated power ...
The LV7 is the multi-point fuel injection 1.4 L naturally-aspirated variant of the SGE, with a 74 mm × 81.3 mm (2.91 in × 3.20 in) bore and stroke for a total capacity of 1,399 cc (1.4 L). Compression ratio is 10.6:1 and the engine can run on regular unleaded grade gasoline.
A gasoline engine burns a mix of gasoline and air, consisting of a range of about twelve to eighteen parts (by weight) of air to one part of fuel (by weight). A mixture with a 14.7:1 air/fuel ratio is stoichiometric, that is when burned, 100% of the fuel and the oxygen are consumed.