Pivoting door thrust reverser with actuating mechanism
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United States of America Patent
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-
Oct 19, 1999
Grant Date -
N/A
app pub date -
Oct 2, 1997
filing date -
Oct 3, 1996
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
An actuating mechanism is disclosed for a thrust reverser of a turbojet engine having an engine cowling with a reverse thrust opening, a thrust reverser door pivotally connected to the engine cowling so as to pivot between forward and reverse thrust positions, and a linear actuator having a casing with an extendable and retractable piston rod. The piston rod is connected to the thrust reverser by a first connection forming a first connection point. An interface bracket is fixedly attached to the turbojet engine structure and engages a mounting flange in a connector affixed to the actuator casing at a second connection point, the mounting flange being in contact with the interface bracket at a third connection point, the first, second and third connection points lying in a straight line.
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