发明名称 |
Aircraft pitot and static pressure sensing device and aircraft having the sensing device |
摘要 |
An aircraft pitot and static pressure sensing device and an aircraft having the sensing device, more particularly a fighter aircraft, include a plurality of pressure sensors disposed in a radome of the aircraft. In addition, a plurality of air intake ports is provided in the radome. The air intake ports are connected through connecting passages to the pressure sensors.
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申请公布号 |
US6038932(A) |
申请公布日期 |
2000.03.21 |
申请号 |
US19970942224 |
申请日期 |
1997.10.01 |
申请人 |
NORD-MICRO ELEKTRONIK FEINMECHANIK AG;DAIMLER CHRYSLER AG |
发明人 |
WANDEL, HERMANN;JOST, MICHAEL;SOMMER, HELMUT;FISCHER-WILK, ROBERT |
分类号 |
G01P5/14;G01L19/00;G01P5/165;G01P13/02;(IPC1-7):G01F1/46;G01C21/00 |
主分类号 |
G01P5/14 |
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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