Gas exhaust nozzle for a bypass turbomachine having an...

Power plants – Reaction motor – Particular exhaust nozzle feature

Reexamination Certificate

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Details

C060S771000, C060S226100, C239S265390, C181S213000

Reexamination Certificate

active

07600384

ABSTRACT:
The invention relates to an exhaust nozzle for a bypass turbomachine, the nozzle comprising a central body, a primary cowl surrounding the central body to define a primary channel, and a secondary cowl surrounding the primary cowl to define a secondary annular channel, the secondary cowl comprising a stationary portion and a movable portion disposed to extend the stationary portion and capable of moving longitudinally upstream and downstream relative to the stationary portion and relative to the primary cowl so as to vary the exhaust section and/or the throat section of the nozzle, the stationary portion of the secondary cowl presenting a plurality of spaced-apart repetitive patterns disposed extending its trailing edge, and the movable portion of the secondary cowl including in its outside surface a plurality of indentations of shapes complementary to the patterns of the stationary portion.

REFERENCES:
patent: 2794319 (1957-06-01), Stockdale
patent: 2796731 (1957-06-01), Rubbra et al.
patent: 3262270 (1966-07-01), Beavers
patent: 3581841 (1971-06-01), Raynes
patent: 3642209 (1972-02-01), Stahl
patent: 3797785 (1974-03-01), Baerresen et al.
patent: 3829020 (1974-08-01), Stearns
patent: 4162040 (1979-07-01), Carey
patent: 4383407 (1983-05-01), Inman
patent: 4525999 (1985-07-01), Inman
patent: 4922713 (1990-05-01), Barbarin et al.
patent: 4994660 (1991-02-01), Hauer
patent: 5039014 (1991-08-01), Lippmeier
patent: 5054285 (1991-10-01), Geidel et al.
patent: 5655360 (1997-08-01), Butler
patent: 5778659 (1998-07-01), Duesler et al.
patent: 5806302 (1998-09-01), Cariola et al.
patent: 5996937 (1999-12-01), Gonidec et al.
patent: 6318070 (2001-11-01), Rey et al.
patent: 6360528 (2002-03-01), Brausch et al.
patent: 6895742 (2005-05-01), Lair et al.
patent: 6966175 (2005-11-01), Lair
patent: 6968675 (2005-11-01), Ramlaoui et al.
patent: 6983602 (2006-01-01), Senile
patent: 7000378 (2006-02-01), Birch et al.
patent: 7010905 (2006-03-01), Lair
patent: 7174704 (2007-02-01), Renggli
patent: 2001/0010148 (2001-08-01), Michel et al.
patent: 2006/0016171 (2006-01-01), Renggli
patent: 0 780 562 (1997-06-01), None
patent: 2 372 779 (2002-09-01), None

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