Case deflection control in aircraft gas turbine engines

Details Case deflection control in aircraft gas turbine engines Case deflection control in aircraft gas turbine engines

B - Operations, Transporting

64

D

244/48

B64D 27/18 (2006.01) F02C 7/20 (2006.01)

Patent

CA 1153743

Case Deflection Control in Aircraft Gas Turbine Engines Abstract A gas turbine engine and structure for mounting the gas turbine engine on an aircraft is disclosed. Tech- niques for controlling the magnitude of engine case deflection from the axis of the engine are developed. The transfer of a portion of the gust and thrust loads externally of the engine case to a location downstream of the rearward engine mount generates a reverse moment which counteracts deflection in the engine case.

371028

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