Thrust reverser
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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-
Nov 8, 2011
Grant Date -
May 21, 2009
app pub date -
Nov 16, 2007
filing date -
Nov 16, 2007
priority date (Note) -
In Force
status (Latency Note)
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Abstract
The thrust reverser is used with an aircraft gas turbine engine and includes upper and lower doors pivotable between a stowed position and a deployed position. When deployed, the doors redirect a portion of the efflux to generate a nose-down pitching moment on an aircraft to improve handling during thrust reversing on a runway.
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