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Pratt & Whitney JT9D

Aircraft Engines

The Pratt & Whitney JT9D was the first high bypass ratio jet engine to power a wide-body airliner and Pratt & Whitney's first high-bypass-ratio turbofan. The program was launched in September 1965 and the first engine was tested in December 1966. After FAA certification in May 1969 it entered service in January 1970 on the Boeing 747-100, the first jumbo jet, and it later powered the Boeing 767, the Airbus A300 and A310 and the McDonnell Douglas DC-10. It has a single-stage fan, a three-stage low-pressure compressor and an eleven-stage high-pressure compressor, and it used titanium and nickel alloys to improve fuel efficiency over the earlier JT3D. During the 747 flight tests the casing ovalized under takeoff stress and rubbed the turbine blade tips, so thirty aircraft waited outside the factory with concrete blocks hanging from their pylons until the casing was strengthened. Production ceased in 1990 and the PW4000 replaced it.

Facts
Year
1966 1
Displacement or Thrust
43,500 lbf (193 kN) for the JT9D-3 1
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Source Pratt & Whitney JT9D (Wikipedia)
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Source Pratt & Whitney JT9D (Wikipedia)Lead
Quote, Lead
It was Pratt & Whitney's first high-bypass-ratio turbofan.
Sources
1. Pratt & Whitney JT9D (Wikipedia)
  • Development
    The JT9D program was launched in September 1965 and the first engine was tested in December 1966.
  • Design
    The JT9D-3, the earliest certified version of the engine, weighed 8,470 lb (3,840 kg) and produced 43,500 lbf (193 kN) thrust.
  • Lead
    It was Pratt & Whitney's first high-bypass-ratio turbofan.
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