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Thermal switches on microprocessors often stop only the fetching of instructions to execute, reducing the clock rate to zero until a lower temperature is reached, while maintaining power to the cache to prevent data loss (although a second switch, with a higher triggering temperature, usually turns off even the cache and forces the computer to ...
The GE F110 turbofan fighter jet engine is a derivative of the F101, designed using data from the F101-powered variant of the F-16 Fighting Falcon tested in the early 1980s. [ 2 ] [ 3 ] The F101 also became the basis for the highly successful CFM56 series of civil turbofans.
The General Electric F110 is an afterburning turbofan jet engine produced by GE Aerospace (formerly GE Aviation). It was derived from the General Electric F101 as an alternative engine to the Pratt & Whitney F100 for powering tactical fighter aircraft, with the F-16C Fighting Falcon and F-14A+/B Tomcat being the initial platforms; the F110 would eventually power new F-15 Eagle variants as well.
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F414-GE-39E (GE RM16) New version of the F414G for the Saab JAS-39E/F Gripen. [38] [39] [40] F414-GE-400K Variant of the F414-GE-400 co-developed by General Electric and Hanwha Aerospace for the South Korean KAI KF-21 Boramae, to be manufactured jointly and assembled locally in South Korea by Hanwha Aerospace. [41] [42] F414-GE-100
Lean-burn refers to the burning of fuel with an excess of air in an internal combustion engine.In lean-burn engines the air–fuel ratio may be as lean as 65:1 (by mass). ). The air:fuel ratio needed to stoichiometrically combust gasoline, by contrast, is 14.
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In February 2012, GE announced studies on a more efficient derivative of the GE90, calling it the GE9X, to power both the -8 and -9 variants of the new Boeing 777X. It was to feature the same 128 in (325 cm) fan diameter as the GE90-115B with thrust decreased by 15,800 lbf (70 kN) to a new rating of 99,500 lbf (443 kN) per engine. [ 1 ]
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