Gas turbine engine augmentor

Power plants – Reaction motor – Liquid oxidizer

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60749, F02C 100

Patent

active

047651369

ABSTRACT:
The pilot section of a flameholder of an augmentor for a gas turbine engine is modified to improve the ignition and stability characteristics by judiciously locating aperture(s) or slot(s) in the pilot section wherein their orientation is critical so as to create a vortical flow field.

REFERENCES:
patent: 2368179 (1945-01-01), Turpin
patent: 2517015 (1950-08-01), Mock et al.
patent: 2529506 (1950-11-01), Lloyd et al.
patent: 2918794 (1959-12-01), Hurd
patent: 2920445 (1960-01-01), Bailey
patent: 2925716 (1960-02-01), Regan et al.
patent: 3030773 (1962-04-01), Johnson
patent: 3151453 (1964-10-01), Lefebvre et al.
patent: 3366373 (1968-01-01), Reed
patent: 3540216 (1970-10-01), Quillevere et al.
patent: 3587232 (1971-06-01), Bryce
patent: 3618318 (1971-11-01), Bryce
patent: 3701255 (1972-10-01), Markowski
patent: 3732059 (1973-05-01), Goodnight et al.
patent: 3800530 (1974-04-01), Nash
patent: 3869864 (1975-03-01), Bunn
patent: 3946553 (1976-03-01), Roberts et al.
patent: 3999378 (1976-12-01), Tatem, Jr. et al.
patent: 4062182 (1977-12-01), Fehler et al.

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

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

Rate now

     

Profile ID: LFUS-PAI-O-829248

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