Ducted fan gas turbine engine mounting

Details Ducted fan gas turbine engine mounting Ducted fan gas turbine engine mounting

1997-03-11

1999-01-19

Casaregola, Louis J.

Power plants

Reaction motor

Interrelated reaction motors

60 3931, F02C 720

Patent

active

058602763

ABSTRACT:
A ducted fan gas turbine engine is mountable on an aircraft structure via a pylon which includes a yoke. The yoke straddles the compressor module of the engine and is connected thereto at points diametrically opposite each other, thus obviating thrust links and the need for radial struts in the plane of the yoke.

REFERENCES:
patent: 4147029 (1979-04-01), Sargisson
patent: 4785625 (1988-11-01), Stryker et al.
patent: 5174525 (1992-12-01), Schilling
patent: 5205513 (1993-04-01), Schilling
patent: 5452575 (1995-09-01), Freid
patent: 5524847 (1996-06-01), Brodell et al.

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