Thrust reverser provided with at least one swing door and constructed to permit a bearing surface of reduced thickness of the trailing edge, for a jet engine, notably that of an aircraft, and a jet engine equipped with this thrust reverser
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United States of America Patent
Stats
-
Nov 17, 1998
Issued Date -
N/A
app pub date -
May 27, 1997
filing date -
Mar 28, 1994
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
The invention concerns a thrust reverser for a jet engine, of the type having swing doors (6) pivoting about fixed transverse pivots (7) secured to the rear end of flanges extending in line with pipe of the engine. According to the invention, each door (6) is borne by a connecting piece (10) offset towards the front with respect to a transverse plane passing through the pivot axis and orthogonal to the longitudinal axis of the door. Furthermore, the fairing (4a, 4b) extends as far as the rear end of the flanges, the said fairing and each door (6) being arranged, on the one hand, so as to cover completely the flanges in the folded position of the said door, and, on the other hand, to enable each door (6) to be brought into its deployed position without any interference between the said fairing and door.
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