Invention Application
- Patent Title: GEARED TURBINE ENGINE WITH O-DUCT AND THRUST REVERSER
- Patent Title (中): 具有O型和T型扭矩的齿轮式涡轮发动机
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Application No.: US14786439Application Date: 2014-04-24
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Publication No.: US20160069297A1Publication Date: 2016-03-10
- Inventor: Nigel D. Sawyers-Abbott
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Hartford
- Assignee: United Technoligies Corporation
- Current Assignee: United Technoligies Corporation
- Current Assignee Address: US CT Hartford
- International Application: PCT/US14/35300 WO 20140424
- Main IPC: F02K1/72
- IPC: F02K1/72 ; F02C3/107 ; F02C7/36

Abstract:
A geared turbofan engine is provided that includes a first rotor, a second rotor and a gear train that are arranged along an axis within a casing. The first rotor is connected to and driven by the second rotor through the gear train. The casing includes a nozzle, a bifurcation, a thrust reverser and a flowpath. The flowpath extends axially to the nozzle and circumferentially between opposing surfaces of the bifurcation.
Information query
IPC分类: