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

1980-04-02

1984-01-31

Croyle, Carlton R.

Power plants

Reaction motor

Interrelated reaction motors

244 54, 60 3931, F02C 720

Patent

active

044281897

ABSTRACT:
A gas turbine engine and structure for mounting the gas turbine engine on an aircraft is disclosed. Techniques 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.

REFERENCES:
patent: 3138920 (1964-06-01), Reichert
patent: 3675418 (1972-07-01), Lenkeit et al.
patent: 3844115 (1974-10-01), Freid
patent: 4022018 (1977-05-01), Tuten et al.
patent: 4266741 (1981-05-01), Murphy

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