Aircraft engine ejector nozzle

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With retractable noise suppressing stream divider

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

23926519, 23926517, B64D 3304

Patent

active

057791503

ABSTRACT:
An aircraft ejector nozzle includes a plug assembly (26) located between upper and lower cowlings (18, 20) and upright sidewalls (22). The plug assembly (26) includes separable upper and lower diverters (28, 30). Each diverter includes multiple subsections pivotably attached end-to-end. In one embodiment, first, second, and third subsections (90, 92, 94) are provided. Stationary ejectors (40, 42) located in the cowlings (18, 20) input ambient airflow (44) into an exhaust stream (32). Preferably the ejectors (40, 42) include mixing components (46). Upper and lower aft flaps (48, 50) further tailor the exhaust path shape. An actuation assembly (52) moves the diverters (28, 30) and aft flaps (48, 50) between their various positions. One actuation assembly embodiment includes a number of rotatable disks (118, 120, 132, 134, 142) for guiding the upper and lower diverters (28, 30) and the aft flaps (48, 50). In a first plug assembly configuration the diverter forward ends (84) are positioned together and the diverter aft ends (86) are positioned together. The first configuration forces exhaust (32) around the diverters (28, 30). In a second plug assembly configuration the diverter forward ends (84) are positioned apart and the diverter aft ends (86) are positioned apart. The second configuration forces exhaust (32) between the diverters (28, 30) while simultaneously covering the ejectors (40, 42). Acoustic linings (100) are provided at various locations within the nozzle and are exposed to the exhaust flow only during noise suppression configurations, thus minimizing liner wear and contamination.

REFERENCES:
patent: 2803944 (1957-08-01), Kroon
patent: 2938335 (1960-05-01), Cook
patent: 2997845 (1961-08-01), Oulianoff
patent: 3237864 (1966-03-01), Taylor et al.
patent: 3263931 (1966-08-01), Bartek et al.
patent: 3333772 (1967-08-01), Bruner
patent: 3372876 (1968-03-01), Colville et al.
patent: 3409228 (1968-11-01), Mehr
patent: 3524588 (1970-08-01), Duval
patent: 3550721 (1970-12-01), Bruner
patent: 3613829 (1971-10-01), Cabassut
patent: 3637041 (1972-01-01), Hilbig
patent: 3647020 (1972-03-01), MacDonald
patent: 3664455 (1972-05-01), Duvvuri
patent: 3695387 (1972-10-01), Hilbig
patent: 3774868 (1973-11-01), Goetz
patent: 3897169 (1975-07-01), Fowler
patent: 4095417 (1978-06-01), Banthin
patent: 4165607 (1979-08-01), Rudolph
patent: 4175640 (1979-11-01), Birch et al.
patent: 4215536 (1980-08-01), Rudolph
patent: 4422524 (1983-12-01), Osborn
patent: 4537026 (1985-08-01), Nightingale
patent: 4690329 (1987-09-01), Madden
patent: 4819876 (1989-04-01), Thayer
patent: 4958489 (1990-09-01), Simmons
patent: 5044553 (1991-09-01), Degress
patent: 5044559 (1991-09-01), Russell et al.
patent: 5343697 (1994-09-01), Johnson et al.
"The Jet Engine," chapters 6, 14, 15 and 19, Rolls-Royce plc, 1992.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Aircraft engine ejector 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 Aircraft engine ejector nozzle, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft engine ejector nozzle will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1874493

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.