Thrust orienting nozzle

Details Thrust orienting nozzle Thrust orienting nozzle

2006-06-29

2009-12-15

Casaregola, Louis J (Department: 3741)

Power plants

Reaction motor

With thrust direction modifying means

C060S231000, C239S265230

Reexamination Certificate

active

07631486

ABSTRACT:
The present invention relates to a thrust orienting nozzle, shaped in such a way as to divide a principal propulsion gas flow coming from at least one gas generator into a first flow and a second flow for an ejection in a first half-nozzle and in a second half-nozzle and comprising at least one of following two piloting means: a means of dividing the principal flow into each of the two half-nozzles, and a means of orienting the thrust vector produced by each of the two half-nozzles.The invention applies in particular to the yaw control of an aircraft without a vertical tail unit.

REFERENCES:
patent: 3285262 (1966-11-01), Ernst et al.
patent: 5170964 (1992-12-01), Enderle et al.
patent: 5706650 (1998-01-01), Thayer
patent: 6112513 (2000-09-01), Catt et al.
patent: 6679048 (2004-01-01), Lee et al.
patent: 2002/0189232 (2002-12-01), Weiland et al.
patent: 1 158 156 (2001-11-01), None

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