Device for mounting an air-flow dividing wall in a turbojet...

Details Device for mounting an air-flow dividing wall in a turbojet... Device for mounting an air-flow dividing wall in a turbojet...

2011-03-22

2011-03-22

Kim, Ted (Department: 3741)

Power plants

Reaction motor

Having afterburner

C060S765000

Reexamination Certificate

active

07908868

ABSTRACT:
A device for mounting a dividing wall for separating the main air stream and the bypass air in a bypass turbojet engine afterburner is disclosed. The device includes an attachment unit which attaches the upstream end of the wall to a guide vane casing and a supporting unit which supports the downstream end of the wall provided on flame holder arms of the afterburner radially on the inside of the dividing wall.

REFERENCES:
patent: 3826088 (1974-07-01), Nash et al.
patent: 4718230 (1988-01-01), Honeycutt et al.
patent: 4901527 (1990-02-01), Nash et al.
patent: 5396763 (1995-03-01), Mayer et al.
patent: 5400589 (1995-03-01), Mahias et al.
patent: 5813221 (1998-09-01), Geiser et al.
patent: 6976361 (2005-12-01), Cortes et al.
patent: 2005/0252216 (2005-11-01), Roche et al.
patent: 2006/0016193 (2006-01-01), Roche et al.
patent: 2006/0016194 (2006-01-01), Roche et al.
patent: 0 328 813 (1989-08-01), None
patent: 0 550 126 (1993-07-01), None
patent: 1 491 752 (2004-12-01), None

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