Turbojet engine exhaust casing with integral suspension lugs

Details Turbojet engine exhaust casing with integral suspension lugs Turbojet engine exhaust casing with integral suspension lugs

1992-06-17

1993-03-02

Barefoot, Galen

Aeronautics and astronautics

Aircraft power plants

Mounting

60 3931, 248554, B64D 2700

Patent

active

051902451

ABSTRACT:
The exhaust casing of a turbojet engine has a cross-sectional shape in the form of a regular polygon and carries at least three external hanging lugs provided with holes for receiving fixing axles of a rear suspension structure for the engine. The lugs are carried by non-consecutive sides of the casing in ), manner that the geometrical axis of the hole of each lug is situated at the intersection of the median planes of the two sides of the casing adjacent the side carrying the lug.

REFERENCES:
patent: 3848832 (1974-11-01), Stanley et al.
patent: 4742975 (1988-05-01), Pachomoff et al.
Joubert, European Pub. App. 0028970, May 1981.

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