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Source: The Open Library

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1Exoskeletal engine concept

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“Exoskeletal engine concept” Metadata:

  • Title: Exoskeletal engine concept
  • Author:
  • Language: English
  • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
  • Publish Date:
  • Publish Location: ➤  [Cleveland, Ohio] - Hanover, MD

“Exoskeletal engine concept” Subjects and Themes:

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Access and General Info:

  • First Year Published: 2001
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    Bypass ratio

    The bypass ratio (BPR) of a turbofan engine is the ratio between the mass flow rate of the bypass stream to the mass flow rate entering the core. A 10:1

    Turbofan

    The ratio of the mass-flow of air bypassing the engine core to the mass-flow of air passing through the core is referred to as the bypass ratio. The

    Pratt & Whitney JT9D

    The Pratt & Whitney JT9D engine was the first high bypass ratio jet engine to power a wide-body airliner. Its initial application was the Boeing 747-100

    Thrust reversal

    reversing devices are used to block the blast and redirect it forward. High bypass ratio engines usually reverse thrust by changing the direction of only the

    Bypass

    colour film Bypass capacitor, used to bypass a power supply or other high impedance component Bypass ratio in turbofan aircraft engines Bypass duct, whose

    Afterburner

    it pays to select an engine cycle with a high specific thrust (i.e. high fan pressure ratio/low bypass ratio). The resulting engine is relatively fuel

    Rolls-Royce Trent 700

    (247 cm) fan for a 5:1 bypass ratio, it produces 300.3–316.3 kN (67,500–71,100 lbf) of thrust and reaches an overall pressure ratio of 36:1. It competes

    General Electric CF6

    F138, is a family of high-bypass turbofan engines produced by GE Aviation. Based on the TF39, the first high-thrust, high-bypass jet engine, the CF6 has

    Progress D-27

    was proposed for the Tupolev Tu-334. D-527 an engine with an ultra-high bypass ratio of 18 that was considered for the Tupolev Tu-334. Nicknamed "super

    General Electric Passport

    CFM LEAP, it is a twin-spool axial engine with a 5.6:1 bypass ratio, a 45:1 overall pressure ratio and one-piece 52 in (130 cm) titanium fan blisk with


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