发明名称 |
Catapult restraint/release system |
摘要 |
Apparatus for restraining an aircraft against the combined forces of a catapult launching shuttle and aircraft takeoff power during a catapult assisted takeoff until a predetermined combined force level has been reached. Release of the aircraft is triggered by the relative movement of a central piston within a housing which causes disengagement of gripping lugs from a tensile bar attached to the aircraft. The relative movement is enabled by the compressibility of hydraulic oil confined within the apparatus and loaded by the combined forces.
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申请公布号 |
US4103849(A) |
申请公布日期 |
1978.08.01 |
申请号 |
US19770833415 |
申请日期 |
1977.09.15 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY |
发明人 |
HOLT, LLOYD J.;PANLAQUI, CLAYTON E. |
分类号 |
B64F1/04;(IPC1-7):B64F1/04;B64F1/16 |
主分类号 |
B64F1/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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