Invention Application
US20160069297A1 GEARED TURBINE ENGINE WITH O-DUCT AND THRUST REVERSER 审中-公开
具有O型和T型扭矩的齿轮式涡轮发动机

GEARED TURBINE ENGINE WITH O-DUCT AND THRUST REVERSER
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.
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