Jet engine provided with a thrust reverser
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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-
May 10, 1994
Issued Date -
N/A
app pub date -
Feb 5, 1993
filing date -
Oct 27, 1988
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A jet engine for an aircraft has a thrust reverser including one or more doors which define at least a part of the throat of the engine's nozzle. The engine further includes a latch mechanism for retaining the doors in a stowed position. The doors may be deployed for reversal of engine thrust, but are also capable while stowed of being pivoted in a limited way to change the cross-section area of the throat of the nozzle.
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