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  2. Pratt & Whitney Canada PT6 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PT6

    It is common to bleed air from a compressor to make it work properly at low engine speeds. The PT6 has a bleed arrangement which reuses the bleed air by returning it in a tangential direction at the entry to the compressor, an idea patented by Schaum et al. and titled "Turbine Engine With Induced Pre-Swirl at Compressor Inlet". [19]

  3. Pratt & Whitney Canada PT6T - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PT6T

    Congress only approved the purchase when it was assured that a U.S. source would be found for the PT6T engines. This source was Pratt & Whitney Engine Services in Bridgeport, West Virginia, which was established in 1971 to assemble and test new T400-WV-402 engines. As a result, the U.S. military ordered 294 Bell 212s under the designation UH-1N ...

  4. Pratt & Whitney Canada JT15D - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_JT15D

    The engine was first run in August 1967 before being test flown on an Avro Canada CF-100 Canuck in an underslung external test pod. [3] In 1975 a unique over-wing installation in place of Pratt & Whitney Canada PT6 turboprops was fitted to a Beechcraft Super King Air and flown for 93 hours to investigate the use of turbofan engines on that ...

  5. Pilatus PC-6 Porter - Wikipedia

    en.wikipedia.org/wiki/Pilatus_PC-6_Porter

    PC-6 cabin interior, circa 1960s. The Pilatus PC-6 Porter is a Short Takeoff and Landing (STOL) utility aircraft.The majority of aircraft are powered by a single Pratt & Whitney Canada PT6A turboprop engine, which drives a fully reversible, constant-speed, three-bladed HC-B3TN-3D (or an alternative four-bladed HC-D4N-3P) Hartzell aluminium propeller via a reduction gearbox.

  6. Pratt & Whitney Canada PW600 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW600

    The 2,500 lbf (11 kN) thrust PW625F demonstrator engine was first run on 31 October 2001. [1] It flew in late 2002. [2] In 2002, the PW610F was selected for the Eclipse 500 twinjet, replacing the EJ22 as Williams was unable to reach sufficient reliability. The 950 lbf (4.2 kN) thrust engine was certified by Transport Canada on 27 July 2006. [3]

  7. Components of jet engines - Wikipedia

    en.wikipedia.org/wiki/Components_of_jet_engines

    Diagram of a typical gas turbine jet engine. Air is compressed by the compressor blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor blades. 1. Intake 2. Low pressure compression 3. High pressure compression ...

  8. Free-turbine turboshaft - Wikipedia

    en.wikipedia.org/wiki/Free-turbine_turboshaft

    The compressor spool, turbine and compressor, is in green. The free power turbine is in purple. A free-turbine turboshaft is a form of turboshaft or turboprop gas turbine engine where the power is extracted from the exhaust stream of a gas turbine by an independent turbine, downstream of the gas turbine. The power turbine is not mechanically ...

  9. Beechcraft 1900 - Wikipedia

    en.wikipedia.org/wiki/Beechcraft_1900

    The Beechcraft 1900 is a U.S made twin-engine turboprop regional airliner manufactured by Beechcraft. It is also used as a freight aircraft and corporate transport, and by several governmental and military organizations. With customers favoring larger regional jets, then-owner Raytheon ended production in October 2002. [3]

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