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

1993-11-09

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

244 54, 248554, F02C 720

Patent

active

052591832

ABSTRACT:
The exhaust casing of a turbojet engine has a polygonal cross-section and carries at least three hanging lugs provided with holes designed to receive fixing axles of a rear suspension structure for the engine. The axes of these holes are situated at vertices of the polygon defined by the cross-section of the casing, and this polygon is regular except at the position of each of the hanging lugs, where it is deformed to displace the respective vertex radially outward.

REFERENCES:
patent: 3806607 (1974-04-01), Kutney
patent: 4492078 (1985-01-01), Williamson
patent: 4520974 (1985-06-01), Debeneix
patent: 5078342 (1992-01-01), Langley et al.

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