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RT300 Jet-A1 Model that runs on Jet A-1 fuel, with a compression ratio of 8.5:1 and produces 31 hp (23 kW) at 7500 rpm. [2]RT300 LCR Model that runs on petroleum or avgas, with a compression ratio of 9.6:1 and produces 32 hp (24 kW) at 7500 rpm.
The PW 300 series has been developed in partnership with MTU who are responsible for the low pressure turbine. The first variant, the PW305A, has the following configuration and was designed with a core flexible enough for engines with take-off thrusts from 20 kN to 31 kN (4,500 to 7,000 lb): a single-stage fan driven by a three-stage low pressure turbine, supercharging a four-stage axial ...
The R-15-300 was designed at the OKB-300 design bureau led by Sergei Tumansky in the late 1950s. The engine was originally intended for the Tupolev Tu-121 high-altitude high-speed cruise missile. Due to a lack of Soviet resources and funding, the engine casing was mainly steel, and in areas exposed to high temperatures, 30-micrometre silver ...
Honeywell HTF7500E turbofans were selected along a Rockwell Collins Pro Line Fusion avionics suite integrated cockpit and a Parker Hannifin fly-by-wire flight control system. [2] At the May 2008 European Business Aviation Convention and Exhibition, the larger was named Legacy 500 priced at $18.4 million and the smaller Legacy 450, priced at $15 ...
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 ...
Rotax is one of the world's principal suppliers of aircraft engines for ultralight aircraft, light aircraft and unmanned aerial vehicles. [2] Between 1985 and 1995, 60,000 Rotax engines were sold for aircraft propulsion. [2] In the light aircraft class, in 1998 Rotax outsold all other aero engine manufacturers combined. [4]
It powers the Airbus A300-600 and Airbus A310-300, Boeing 747-400 and 767-200/300, and McDonnell Douglas MD-11 widebodies. [ 1 ] Development of the 64,000–68,000 lbf (280–300 kN), 100 in (2.5 m)-fan version began in December 1991 for the Airbus A330 , was FAA certified in August 1993, and made its first flight two months later.
The Tumansky R-29 is a Soviet turbojet aircraft engine that was developed in the early 1970s. [1] It is generally described as being in the "third generation" of Soviet gas turbine engines which are characterized by high thrust-to-weight ratios and the use of turbine air cooling.