Ventilation system for a convergent divergent exhaust nozzle

Details Ventilation system for a convergent divergent exhaust nozzle Ventilation system for a convergent divergent exhaust nozzle

2007-11-20

2007-11-20

Kim, Ted (Department: 3746)

Power plants

Reaction motor

With thrust direction modifying means

C060S262000, C060S266000, C239S265350, C239S265170, C239S265390

Reexamination Certificate

active

10945917

ABSTRACT:
The invention relates to a ventilation system for a convergent divergent exhaust nozzle in a bypass turbojet comprising an afterburn chamber surrounded by an annular passage through which circulates a stream of cooling air, a convergent divergent axisymmetric nozzle arranged downstream of said afterburn chamber, each circle of flaps comprising alternately a plurality of controlled flaps, and a plurality of follower flaps, a circle of cold flaps arranged radially outside said nozzle and hinged at their upstream end to a conical shell linked to the downstream part of the casing. The means of cooling the divergent flaps comprise an annular plenum chamber delimited downstream by said conical shell and fed with cooling air through drillings made in a boundary wall between said plenum chamber and the downstream end of said annular passage, a plurality of distribution cells surrounding the plenum chamber and linked to the latter, said cells being delimited downstream by said conical shell and being arranged around the X axis in the planes of symmetry of the follower flaps and telescopic pipelines each linking a cell to the follower divergent flap situated in the same plane of symmetry as said cell.

REFERENCES:
patent: 4000612 (1977-01-01), Wakeman et al.
patent: 5255849 (1993-10-01), Mayer et al.
patent: 5435127 (1995-07-01), Luffy et al.
patent: 5586431 (1996-12-01), Thonebe et al.
patent: 5593112 (1997-01-01), Maier et al.
patent: 5603531 (1997-02-01), Maier
patent: 5775589 (1998-07-01), Vdoviak et al.
patent: 5799874 (1998-09-01), Eigenbrode et al.
patent: 5996936 (1999-12-01), Mueller
patent: 6021637 (2000-02-01), Scavo
patent: 6301877 (2001-10-01), Liang et al.
patent: 7213393 (2007-05-01), Lapergue et al.
patent: 2003/0182929 (2003-10-01), de Verduzan et al.
patent: 0 541 346 (1993-05-01), None
patent: 1 333 172 (2003-08-01), None

Affiliated with

Also associated with

Rating

Ventilation system for a convergent divergent exhaust nozzle does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Ventilation system for a convergent divergent exhaust nozzle, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Ventilation system for a convergent divergent exhaust nozzle will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-3806247