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  2. 2si 460 - Wikipedia

    en.wikipedia.org/wiki/2si_460

    The 2si 460 is a family of in-line twin-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by ILO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.

  3. Garrett TFE731 - Wikipedia

    en.wikipedia.org/wiki/Garrett_TFE731

    The first test run of the TFE731 occurred in 1970 at Garrett's plant in Torrance, California. [2] The first production model, the TFE731-2, began rolling off the assembly line in August, 1972, and was used on the Learjet 35/36 and Dassault Falcon 10 , both of which entered production in 1973.

  4. Pratt & Whitney J58 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_J58

    The Pratt & Whitney J58 (company designation JT11D-20) is an American jet engine that powered the Lockheed A-12, and subsequently the YF-12 and the SR-71 aircraft. It was an afterburning turbojet engine with a unique compressor bleed to the afterburner that gave increased thrust at high speeds.

  5. Vacuum ejector - Wikipedia

    en.wikipedia.org/wiki/Vacuum_Ejector

    A vacuum ejector, or simply ejector, is a type of vacuum pump, which produces vacuum by means of the Venturi effect.. In an ejector, a working fluid (liquid or gaseous) flows through a jet nozzle into a tube that first narrows and then expands in cross-sectional area.

  6. Injector - Wikipedia

    en.wikipedia.org/wiki/Injector

    It is a fluid-dynamic pump with no moving parts except a valve to control inlet flow. Depending on the application, an injector can also take the form of an eductor-jet pump, a water eductor or an aspirator. An ejector operates on similar principles to create a vacuum feed connection for braking systems etc.

  7. Mitsubishi Astron engine - Wikipedia

    en.wikipedia.org/wiki/Mitsubishi_Astron_engine

    Power - 99 hp (74 kW) at 4300 rpm; Torque - 177 lb⋅ft (240 N⋅m) at 2000 rpm; Engine type - Inline 4-cylinder SOHC; Rocker arm - Roller Follower type [14] Fuel system - Distribution type jet pump (indirect injection) Combustion chamber - Swirl type; Bore x Stroke - 91.1 mm × 95 mm (3.59 in × 3.74 in) Compression ratio - 21.0:1

  8. Pratt & Whitney JT8D - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_JT8D

    The Pratt & Whitney JT8D is a low-bypass (0.96 to 1) turbofan engine introduced by Pratt & Whitney in February 1963 with the inaugural flight of the Boeing 727.It was a modification of the Pratt & Whitney J52 turbojet engine which powered the US Navy A-6 Intruder and A-4 Skyhawk attack aircraft.

  9. RD-170 - Wikipedia

    en.wikipedia.org/wiki/RD-170

    The RD-170 (Russian: Ракетный Двигатель-170 (РД-170), romanized: Raketnyy Dvigatel-170, lit. 'Rocket Engine-170') is the world's most powerful and heaviest liquid-fuel rocket engine.