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  2. PBS TS100 - Wikipedia

    en.wikipedia.org/wiki/PBS_TS100

    The PBS TS100 is a small turboshaft engine produced by a Czech turbine engine manufacturer PBS Velká Bíteš.The engine with a maximum power of 241 hp (180 kW) has been developed for light helicopters weighing up to 2,204 lb (1,000 kg).

  3. Rolls-Royce RR500 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_RR500

    The Rolls-Royce RR500 is a family of small gas turbine engines developed by Rolls-Royce Corporation. The RR500TP turboprop variant was intended for use in small aircraft. The RR500TS was the turboshaft variant designed for light helicopters. Development of the RR500 was abandoned in 2012.

  4. Solar T62 - Wikipedia

    en.wikipedia.org/wiki/Solar_T62

    The Solar T62 Titan is an American gas turbine engine used mainly as a aircraft auxiliary power unit (APU), conventional power generator, turboprop engine for fixed-wing aircraft or turboshaft engine for helicopters. A new turbine version was developed as the Solar T66.

  5. Pratt & Whitney Canada PW100 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW100

    The PW150 engine was introduced on 24 April 1995, when Bombardier selected the engine for the launch of its de Havilland Dash 8-400 regional turboprop. The PW150 was a higher-power version of the PW100 series, with the low-pressure compressor changed from a single-stage centrifugal compressor to a three-stage axial compressor , and the turbine ...

  6. Boeing T50 - Wikipedia

    en.wikipedia.org/wiki/Boeing_T50

    The Boeing T50 (company designation Model 502) was a small turboshaft engine produced by Boeing. It was the first turboshaft engine to ever power a helicopter: a modified Kaman K-225 in 1951. [ 1 ] Based on Boeing's earlier Model 500 gas generator, the T50's main application was in the QH-50 DASH helicopter drone of the 1950s.

  7. LHTEC T800 - Wikipedia

    en.wikipedia.org/wiki/LHTEC_T800

    Data from General characteristics Type: turboshaft Length: 31.5 inches (0.80 m) Diameter: Dry weight: 315 pounds (143 kg) Components Compressor: low-pressure centrifugal, high-pressure centrifugal Turbine: low-pressure, high pressure, 2 power turbine Performance Maximum power output: 1,563 shp (1,166 kW) Specific fuel consumption: ~0.459 lb/(hp⋅h) (279 g/kWh) See also Comparable engines Avco ...

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