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, |