发明名称 AIRCRAFT LANDING GEAR MONITORING APPARATUS
摘要 <p>An apparatus is disclosed for monitoring the load on at least one part of an aircraft landing gear during landing of the aircraft. The apparatus (100) comprises a housing containing a sensor (110, 170) which senses a parameter indicative of the load in the part of the landing gear, a processor (120) which receives signals fromthe sensor and processes the signals to produce data representative of the parameter measured by the sensor, a battery (130) which provides electrical power to the processor, a memory (140) for storing measurement data from the processor, and a wireless transmitter (150, 160) which is controlled by the processor. The wireless transmitter is arranged to transmit at least some of the measurement data from the processor to a remote device (200) located outside of the housing.</p>
申请公布号 WO2008110836(A1) 申请公布日期 2008.09.18
申请号 WO2008GB50154 申请日期 2008.03.05
申请人 AIRBUS UK LIMITED;JONES, IAN, JAMES;VAN-GRIENSVEN, BASTIAAN;LIGHT, DAVID;HAZELDEN, ROGER, JOHN;STARK, DAVID, MATTHEW, JAMES;THOMPSON, MARTIN, JOHN, 发明人 JONES, IAN, JAMES;VAN-GRIENSVEN, BASTIAAN;LIGHT, DAVID;HAZELDEN, ROGER, JOHN;STARK, DAVID, MATTHEW, JAMES;THOMPSON, MARTIN, JOHN,
分类号 B64D45/00 主分类号 B64D45/00
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