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2. Genteq - Wikipedia

   en.wikipedia.org/wiki/Genteq

   Genteq is the rebranding of Regal's GE ECM, GE Capacitors and GE Commercial Motors divisions, which occurred in 2009. [ 1 ] Genteq develops and manufactures electronically commutated motors (ECM) and capacitors for residential and light commercial heating and air conditioning ( HVAC ) systems.

3. General Electric TF39 - Wikipedia

   en.wikipedia.org/wiki/General_Electric_TF39

   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. [4] 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. [8] This was developed into the TF39 with a 97 in diameter fan.

4. List of GE reciprocating engines - Wikipedia

   en.wikipedia.org/wiki/List_of_GE_reciprocating...

   GE GEVO-16, 16-cylinder engine used in locomotives, such as the GE ES59ACi, [6] GE ES58ACi, [6] GE ES57ACi Diesel Locomotives. HDL series [1] GE 7HDL-16, 16-cylinder engine used in only the GE AC6000CW [7] L250. GE L250 Series, 6- and 8-cylinder marine engines for propulsion and electric generator usage [8] PowerHaul series

5. General Electric CF34 - Wikipedia

   en.wikipedia.org/wiki/General_Electric_CF34

   The LP spool has 3 core booster stages behind the fan. Static thrust is 82 kilonewtons (18,500 lbf) for the -10E variant. On wing times can reach 14,000 hours, an overhaul costs over $1.5 million and a set of LLPs $2.1 million for a 25,000 cycle life. [ 4 ]

6. GE Aerospace - Wikipedia

   en.wikipedia.org/wiki/GE_Aerospace

   General Electric Company, doing business as GE Aerospace, [5] is an American aircraft engine supplier that is headquartered in Evendale, Ohio, outside Cincinnati.It is the legal successor to the original General Electric Company founded in 1892, which split into three separate companies between November 2021 and April 2024, adopting the trade name GE Aerospace after divesting its healthcare ...

7. CFE CFE738 - Wikipedia

   en.wikipedia.org/wiki/CFE_CFE738

   Other cycle parameters are a bypass ratio of 5.3 and airflow of 240 lb/s (108.9 kg/s). The take-off thrust is 5,600 lbf (24.9 kN), flat-rated to ISA +15°C (30°C, 86°F). Chosen to power the Falcon 2000 in 1990, the engine was also first run in May 1990, [ 1 ] and it was first flown on a Boeing 727 testbed on 31 August 1992. [ 2 ]