Force balancing actuator
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United States of America Patent
Stats
-
Nov 17, 2009
Grant Date -
N/A
app pub date -
Mar 6, 2006
filing date -
Mar 6, 2006
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
There is provided a force balancing actuator for mounting a pressure vessel, containing an engine, to aircraft structure. The force balancing actuator includes a cylinder and piston that is mechanically connected between the pressure vessel and aircraft structure. This piston and cylinder adjustably provides force there between in response to variations in differential pressure between the pressurized cabin and ambient pressure. The cylinder and piston thereby relieves excessive load on engine isolators allowing the isolators to absorb engine vibrations.
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