Fuselage tail jet engine thrust reverser

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

181 33HB, 23926529, 244 125, 244 23D, B64D 3304

Patent

active

039971341

ABSTRACT:
Production of a downwardly and forwardly directed reverse thrust discharged from a reverse-thrust duct is controlled by a door in the rearward-discharge duct having its rearward portion pivotally mounted for swinging of its forward portion between a position lodged in a recess in the side of the rearward-discharge duct and a position in which the forward edge of the door is spaced from the recess and the door is inclined to deflect jet exhaust from the rearward-discharge duct into the reverse-thrust duct branching from the rearward-discharge duct. The discharge end of the reverse-thrust duct can be closed by a second door and actuating means interconnecting the two doors can move them simultaneously through proportionate degrees of movement.

REFERENCES:
patent: 2853852 (1958-09-01), Bodine
patent: 2973921 (1961-03-01), Price
patent: 2988302 (1961-06-01), Smith
patent: 3614037 (1971-10-01), Vdolek
patent: 3655133 (1972-04-01), Medawar et al.
patent: 3791586 (1974-02-01), Moorehead

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

Fuselage tail jet engine thrust reverser does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-1340898

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