发明名称 |
Aircraft load factor overload warning system |
摘要 |
An overload warning system for fighter type aircraft combines analytical techniques of computing structural loads with flight conditions and aircraft control inputs to calculate the allowable load factor/control input on a real time basis. The flight conditions and aircraft control inputs are monitored by a microprocessor, which continuously monitors actual load factor, compares the answers with a computed allowable value and generates an output signal whenever a prescribed value is exceeded. This signal is available for transmission to aural or visual warning devices and for permanent recording.
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申请公布号 |
US4302745(A) |
申请公布日期 |
1981.11.24 |
申请号 |
US19800110957 |
申请日期 |
1980.01.10 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE |
发明人 |
JOHNSTON, JOHN T.;VENORSKY, GEORGE W. |
分类号 |
G05D1/00;(IPC1-7):G08B21/00 |
主分类号 |
G05D1/00 |
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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