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  2. Williams FJ33 - Wikipedia

    en.wikipedia.org/wiki/Williams_FJ33

    Engine configuration is a single stage fan, with booster stage, driven by a two-stage LP turbine, supercharging a centrifugal HP compressor, driven by a single stage HP turbine. [3] An annular combustor is featured.

  3. General Electric CF34 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_CF34

    Later higher thrust versions of the CF34 feature an advanced technology core, with only 10 HP compressor stages. Latest variants, the -10A and -10E, were derived from the CFM56 engine family, [citation needed] and have a radically different HP spool, containing a 9-stage compressor driven by a single stage turbine. The LP spool has 3 core ...

  4. CFM International LEAP - Wikipedia

    en.wikipedia.org/wiki/CFM_International_LEAP

    [24] [25] Southwest Airlines is the launch customer of the 737 MAX with a firm order of 150 aircraft. [26] The list price is US$14.5 million [27] for a LEAP-1A, and US$14.5 million for a LEAP-1B. [28] CFM International offers rate-per-flight-hour support agreements (also known as "power by the hour" agreements) for the engine.

  5. Kaeser Compressors - Wikipedia

    en.wikipedia.org/wiki/Kaeser_Compressors

    Fredericksburg is near to several transport centers, and remains home to the US headquarters. The 22.5-acre (91,000 m 2 ) site includes a 155,176-square-foot (14,416.3 m 2 ) facility. Reiner Mueller retired in December 2008, and his son Frank assumed leadership in January 2009.

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    Get AOL Mail for FREE! Manage your email like never before with travel, photo & document views. Personalize your inbox with themes & tabs. You've Got Mail!

  7. General Electric CF6 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_CF6

    Two booster stages were added to the LP (low pressure) compressor and the last two stages of the HP compressor were removed [6] which increased the overall pressure ratio to 29.3. Although the 86.4 in (2.19 m) diameter fan was retained, the airflow was raised to 1,450 lb/s (660 kg/s), yielding a static thrust of 51,000 lb f (227 kN).

  8. Gas turbine engine compressors - Wikipedia

    en.wikipedia.org/wiki/Gas_turbine_engine_compressors

    On civil turbofans, the first stage of the LP compressor is often a single-stage fan. If the HP compressor pressure ratio exceeds about 4.5:1, then the unit will probably have variable geometry (i.e. variable stators) on the first few stages, to make the surge line on the compressor map more shallow, to accommodate the shallow working line.

  9. Compressor map - Wikipedia

    en.wikipedia.org/wiki/Compressor_map

    A compressor map is a chart which shows the performance of a turbomachinery compressor. This type of compressor is used in gas turbine engines, for supercharging reciprocating engines and for industrial processes, where it is known as a dynamic compressor. A map is created from compressor rig test results or predicted by a special computer program.

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