Gas turbine vectoring exhaust nozzle

Details Gas turbine vectoring exhaust nozzle Gas turbine vectoring exhaust nozzle

1993-07-09

1994-08-09

Casaregola, Louis J.

Power plants

Reaction motor

With thrust direction modifying means

60266, 23926517, 23926537, F02K 112

Patent

active

053354893

ABSTRACT:
An exhaust nozzle has variable convergent flaps, ejector flaps, and short divergent flaps spaced inwardly from the ejector flaps, cooling air is introduced through the opening between the divergent and ejector flaps. When the nozzle is vectored, the size of the opening is increased in the region of the nozzle experiencing higher static pressure.

REFERENCES:
patent: 2846844 (1958-08-01), O'Rourke
patent: 3004385 (1961-10-01), Spears, Jr. et al.
patent: 4037405 (1977-07-01), Huenninger et al.
patent: 4043509 (1977-08-01), McHugh et al.
patent: 4502636 (1985-03-01), Nightingale et al.
patent: 4778109 (1988-10-01), Jourdain et al.
patent: 4819876 (1989-04-01), Thayer
patent: 4994660 (1991-02-01), Hauer
patent: 5050803 (1991-09-01), Wakeman et al.
patent: 5082182 (1992-01-01), Bruchez, Jr. et al.

Affiliated with

Also associated with

Rating

Gas turbine vectoring 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 Gas turbine vectoring exhaust nozzle, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine vectoring exhaust nozzle will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-208400