| TF39 | |
|---|---|
 | |
| A TF39 on a C-5 Galaxy at ILA (Internationale LuftfahrtAusstellung) in Berlin, 2008 | |
| Type | High-bypass turbofan |
| National origin | United States |
| Manufacturer | GE Aviation |
| First run | 1964 |
| Major applications | Lockheed C-5 Galaxy |
| Number built | 463 |
| Developed into | General Electric CF6 General Electric LM2500 |
The General Electric TF39 is a high-bypass turbofan engine that was developed to power the Lockheed C-5 Galaxy. It was the first high-bypass jet engine developed.
The United States Air Force opened the "CX-X Program" in 1964, intending to produce a next-generation strategic airlifter. Of the several airframe and engine proposals returned for consideration, Lockheed's aircraft and General Electric's engine were selected for the new design in 1965.
The high-bypass ratio of 8:1 for the TF-39 had its origins in the lift-fan technology demonstrated by GE in the XV-5 Vertifan aircraft. [1] This aircraft had two X353-5 engines, each consisting of a 62.5-inch-diameter [2] lift-fan driven by a gas generator (J85). The bpr in VTOL operation was 12.3. [3] This tip-turbine driven lift-fan concept was turned 90 degrees and developed as an 80-inch-diameter "cruise fan" demonstrator, driven by a J79 gas generator. [1] For the CX-X program GE demonstrated a half-scale engine, the GE1/6, with 15,830 lb thrust and an sfc of 0.336. [4] This was developed into the TF39 with a 97 in diameter fan.
The high-bypass substantially improved the thrust and fuel consumption compared to the previous GE jetliner turbofan, the CJ805-21. [1] It had two and a half times the thrust, while improving fuel efficiency by about 25%. [5] The first engine went for testing in 1965. Between 1968 and 1971, 463 TF39-1 and -1A engines were produced and delivered to power the C-5A fleet.
The TF39 core was used for the CF6 series of engines, and the LM2500 and LM6000 marine and industrial gas turbines.
The TF39 produced 41,000 to 43,000 lb (191 to 205 kN) of thrust. It had an 8:1 bypass ratio, a 25:1 compressor pressure ratio, and a 2,500 °F (1,370 °C) turbine temperature made possible by the latest cooling technology.
The engine included features developed from previous GE engines:
By modern standards the Low Pressure Compressor on the TF-39 is fairly unique as a single T-stage is mounted upstream of the fan rotor, rather than behind it. Although this T-stage supercharges the inner section of the fan rotor, not all of this airstream enters the High Pressure Compressor as a fair proportion also enters the bypass duct to supplement the air discharging from the outer section of the fan. In other words there are three streams leaving the fan, two of which enter the bypass duct. [7]
On September 7, 2017, the last C-5A powered with TF39 engines made its final flight to Davis-Monthan Air Force Base for retirement. [8] [9] The only application for the TF39, the Galaxy military transport, was re-engined with the more modern F138-GE-102, a military version of the General Electric CF6-80C2. Re-engining for the whole fleet took place from 2008 to 2018.
Data from [10]
Related development
Comparable engines
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