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The RR500 is a larger derivative of the Rolls-Royce RR300 turboshaft, with the engine core scaled-up for increased power. [1] The basic weight of the engine with accessories is 250 lb (113 kg). The model produces around 500 shp (373 kW) for takeoff and can produce 380 shp (280 kW) in continuous use.
The engine was expected to fly first in mid-2013 on a Van's Aircraft RV-10 testbed, [1] but development ended before the engine was flown. By 2022 PBS Velká Bíteš was offering the TP 100 for sale as the non-certified PBS TP100 Turboprop Engine "for small aircraft and unmanned aerial vehicles".
The engine ran about 60 °F (33 °C) hotter than the TPE331-14 in the core. [3] It was Garrett's first free-turbine turboshaft, avoiding the high reduction gear of a single spool turboprop and allowing an easier starting since the gas generator is disengaged from the power turbine. The HP spool turns at 31,500 rpm while the LP spool turns at ...
In July 1990, Industri Pesawat Terbang Nusantara (IPTN) of Indonesia picked the GMA 2100 as the engine for the twin-engine N-250 regional airliner. [3] Flight testing with a 13 ft 6 in diameter (4.11 m) Dowty R373 propeller on a Lockheed P-3 Orion testbed aircraft began on August 23, 1990, and finished after over 50 hours of flight and ground ...
It will compete with the Pratt & Whitney Canada PT6, produced at 51,000 units and leading the small turboprop market for 50 years, adding to the sub 850 horsepower (630 kW) General Electric H80. It has been selected to power the new Beechcraft Denali single engine turboprop aircraft, seating up to 12 passengers at over 280 knots (520 km/h) for ...
The Klimov VK-800 is a turboshaft engine of the fifth generation. It is designed to equip the Mi-54, Ansat and Ka-226 "Sergei" type helicopters. The VK-800V derivative was developed for the power units of helicopters of small and large load-carrying capacity, both in twin- and single-engine configuration.
The GE38 became the T407 military turboprop in partnership with Lycoming Engines for the Lockheed P-7A, with a maximum takeoff power of 6,000 shp (4,475 kW). First run on December 26, 1989, [ 7 ] the T407 engine was scheduled to undergo flight testing on a Lockheed P-3 Orion testbed aircraft in the summer of 1990, [ 8 ] but the US Navy canceled ...
2000s turboprop engines (3 P) 2010s turboprop engines (3 P) This page was last edited on 13 July 2014, at 11:51 (UTC). Text is available under the Creative ...