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General Electric T31

Aircraft Engines

The General Electric T31, which the company designated TG-100A, was the first turboprop engine designed and built in the United States. It benefited from the Anglo-American technology exchange, one of its designers, Glenn Warren, stating that the most important British contribution was the concept of multiple combustion cans, and its axial compressor design was directly influenced by the NACA eight-stage compressor. General Electric chose a single-shaft layout like the Rolls-Royce Dart, with a 14-stage all-axial compressor, a single stage turbine and a long epicyclic propeller reduction gearbox. The XT31 was first used in the experimental Consolidated Vultee XP-81, which first flew on 21 December 1945 as the first aircraft to combine turboprop and turbojet power, with an Allison J33 turbojet in the rear fuselage.

Facts
Classification
Fuel or Cycle
Jet Fuel / Turbine 1
Year
1945 1
Connections

Of Make

Source General Electric T31 (Wikipedia)
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Also in Business Atlas: the manufacturer of this subject.

Source General Electric T31 (Wikipedia)Lead, maker
Quote, Lead, maker
was the first turboprop engine designed and built in the United States
Sources
1. General Electric T31 (Wikipedia)
  • Lead, engine kind, cycle
    was the first turboprop engine designed and built in the United States
  • Design and development, first flight
    It made its initial flight in the Consolidated Vultee XP-81 on 21 December 1945
  • Lead, maker
    was the first turboprop engine designed and built in the United States
  • Part Of: Consolidated Vultee XP-81, Design and development, application
    The General Electric XT31 was first used in the experimental Consolidated Vultee XP-81
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