Thrust reverser for jet engines

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

23926537, 60230, F02K 162

Patent

active

054195152

ABSTRACT:
A thrust reverser for use with a jet engine comprising a pair of symmetrical thrust reverser door, each of the doors being pivotally attached to the jet engine so as to be pivotally movable between reversing and non-reversing positions, each of the doors having a scarfed trailing edge portion so that in the reversing position, the trailing edge portions of the doors are in abutting contact, the thrust reverser doors comprising an inner skin and an outer skin, with the inner skins forming a portion of the jet flow boundary extending from said jet engine pipe to the trailing edge of the door, a pair of half-shells, one being associated with and surrounding the trailing edge portion of each of the doors, the half-shells each comprising inner and outer skins and the inner skin of the half-shells forming the jet flow boundary from the trailing edge of the doors to the exhaust outlet.

REFERENCES:
patent: 2735264 (1956-02-01), Sewett
patent: 3601992 (1970-08-01), Maison
patent: 3612399 (1971-10-01), Rodgers et al.
patent: 3837579 (1974-09-01), Camboulives et al.
patent: 4030687 (1977-06-01), Hapke
patent: 4182501 (1980-01-01), Fage
patent: 4618094 (1986-10-01), Palmer

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

Thrust reverser for jet engines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Thrust reverser for jet engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Thrust reverser for jet engines will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-357217

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