An electronic module assembly for controlling the deployment of one or more airbags in an aircraft includes a power source, a crash sensor configured to produce a signal in response to a crash event and an accelerometer that is configured to produce a signal in response to a crash event. A processor starts a timer upon detection of the signal from the crash sensor. When the processor receives a signal from the crash sensor, the processor is configured to determine if a signal has also been received from the accelerometer and if signals from both the crash sensor and the accelerometer indicate a crash event then the processor reads a memory associated with an inflator. The processor reads a timing value selected for the inflator and fires the inflator when the timer has a value equal to the timing value selected for the inflator.
ELECTRONIC MODULE ASSEMBLY FOR CONTROLLING AIRCRAFT RESTRAINT SYSTEMS
26.09.2019
Patent
Elektronische Ressource
Englisch
Electronic module assembly for controlling aircraft restraint systems
Europäisches Patentamt | 2021
|ELECTRONIC MODULE ASSEMBLY FOR CONTROLLING AIRCRAFT RESTRAINT SYSTEMS
Europäisches Patentamt | 2018
|ELECTRONIC MODULE ASSEMBLY FOR CONTROLLING AIRCRAFT RESTRAINT SYSTEMS
Europäisches Patentamt | 2018
|Electronic module assembly for controlling aircraft restraint systems
Europäisches Patentamt | 2019
|ELECTRONIC MODULE ASSEMBLY FOR CONTROLLING AIRCRAFT RESTRAINT SYSTEMS
Europäisches Patentamt | 2018
|