Title:
ELECTRONIC MODULE ASSEMBLY FOR CONTROLLING AIRCRAFT RESTRAINT SYSTEMS
Document Type and Number:
Japanese Patent JP2018140774
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a system for controlling airbags used in an aircraft.SOLUTION: 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 a 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.SELECTED DRAWING: Figure 1
More Like This:
| WO/2000/050261 | CAPACITIVE SENSORS FOR VEHICULAR ENVIRONMENTS |
| WO/2008/043616 | CRASH SENSOR AND METHOD FOR PROCESSING AT LEAST ONE MEASURED SIGNAL |
| WO/2005/098384 | DEVICE FOR DETECTING COLLISION WITH A VEHICLE |
Inventors:
PETER ANTHONY SETTLES
SCOTT FINK
GIUSEPPE GULLOTTO
SCOTT FINK
GIUSEPPE GULLOTTO
Application Number:
JP2018024110A
Publication Date:
September 13, 2018
Filing Date:
February 14, 2018
Export Citation:
Assignee:
AMSAFE INC
International Classes:
B60R21/0136; B60R22/48; B64D25/02
Attorney, Agent or Firm:
Shinichiro Tanaka
Disciple Maru Ken
▲吉▼田 和彦
Fumiaki Otsuka
Takaki Nishijima
Hiroyuki Suda
Hiroshi Uesugi
Naoki Kondo
Disciple Maru Ken
▲吉▼田 和彦
Fumiaki Otsuka
Takaki Nishijima
Hiroyuki Suda
Hiroshi Uesugi
Naoki Kondo