Sealing assembly between an aircraft fuselage and the outer nozz

Details Sealing assembly between an aircraft fuselage and the outer nozz Sealing assembly between an aircraft fuselage and the outer nozz

1991-11-29

1993-06-29

Barefoot, Galen

Aeronautics and astronautics

Aircraft power plants

2441291, 244131, B64D 2904

Patent

active

052226921

ABSTRACT:
An aircraft having a turbojet engine disposed within its fuselage wherein towards the rear end thereof it is provided with a sealing assembly between the rear end of the fuselage and the outer flaps of the nozzle of the turbojet engine, the sealing assembly including a central carrier ring, preferably made of a carbon-epoxy material, secured to the turbojet engine by supporting legs, a hollow front seal at the front end of the carrier ring engaging the inner surface of the fuselage, and a hollow rear seal at the rear end of the carrier ring engaging each of the outer flaps, the carrier ring also engaging the inner surface of the fuselage at a position spaced rearwardly from the front seal.

REFERENCES:
patent: 3098352 (1963-07-01), Taub et al.
patent: 3243126 (1966-03-01), Kurti et al.
patent: 3441221 (1969-04-01), Naud et al.
patent: 3658253 (1972-04-01), Steffen
patent: 4022948 (1977-05-01), Smith et al.
patent: 4114248 (1978-09-01), Smith et al.
patent: 4203286 (1980-05-01), Warburton

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