The General Electric F101 is an afterburning turbofan jet engine. It powers the Rockwell B-1 Lancer strategic bomber fleet of the USAF. In full afterburner it produces a thrust of more than 30,000 pounds-force (130 kN). The F101 was GE's first turbofan with an afterburner. [1]

The F101 engine was originally developed for the Advanced Manned Strategic Aircraft program, which became the B-1A strategic bomber, and powered four development aircraft from 1970 to 1981. Rated in the 30,000 pound thrust class, the F101 …

2011年7月7日 · The General Electric F101, a moderate bypass ratio turbofan engine, was originally developed for the Advanced Manned Strategic Aircraft program, which became the B-1 strategic bomber.

The General Electric F101 is an afterburning turbofan jet engine. It powers the Rockwell B-1 Lancer strategic bomber fleet of the USAF. In full afterburner it produces a thrust of more than 30,000 pounds-force (130 kN). The F101 was GE's first turbofan with an afterburner. [1]

The General Electric F101 is an afterburning turbofan jet engine. It powers the Rockwell B-1 Lancer strategic bomber fleet of the USAF. In full afterburner it produces a thrust of more than 30,000 pounds-force (130 kN).

2019年5月22日 · In 1970, the U.S. Air Force selected the GE F101 engine to power the B-1 bomber. The dual-shaft F101, GE’s first afterburning turbofan, built upon the GE1 and GE9 demonstrators, along with metallurgical advances from the X370 demonstrator.

2025年1月21日 · The bomber is powered by four General Electric F101-GE-102 turbofan engines, mounted in two-engine nacelles under the wing roots. These are rated at 17,390 pounds of thrust (23.578 kilonewtons) and produce 30,780 pounds (41.732 kilonewtons) with “augmentation.”

This is an axial-flow engine with a 2-stage fan section, 9-stage compressor and 3-stage turbine (1 high- and 2 low-pressure stages). It is rated at 16,150 pounds of thrust (71.839 kilonewtons), and 29,850 pounds (132.779 kilonewtons) with afterburner.

5 General Electric F101 Augmented Turbofan I'ngine. 25 6 FI01 Engine Combustor Assembly. 26 4 7 F101 Engine Combustor Flowpath. 27 8 F101 Combustor Dome Details, Aft Looking Forward. 28 9 F101 Combustor Liner Cooling Scheme. 30 10 F101 Engine Fuel Nozzle. 31 11 F101 Engine Fuel Nozzle Flow Characteristic. 32

The F101 turbofan engine with afterburner and variable geometric nozzle has been specially developed for the B-1 Lancer (USAF supersonic bomber). Originally, the F101 motor was developed for a project under the name Advanced Manned Strategic Aircraft program .