In-flight reverser
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Nov 10, 1992
Issued Date -
N/A
app pub date -
Dec 13, 1991
filing date -
Jan 11, 1991
priority date (Note) -
In Force
status (Latency Note)
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Abstract
Increased aircraft control is achieved by combining reverse thruster operation with splay capability. Each of the four door sets has a pair of vanes controllable to various parallel positions. Maximum opening at 26.degree. from the vertical decreases in each direction from the maximum position. The vanes may be controlled to effect yaw and pitch control while maintaining a constant total effective flow area. Back pressure on the turbine is thereby unaffected.
First Claim
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