Abstract: A pretensioner for tightening an occupant restraint, such as a seatbelt, against an occupant on a vehicle. The pretensioner has a locking reel which is activated when a signal is sent by a crash sensing device. When such signal is sent, the pretensioner causes a rack to turn a pinion, which is attached to a reel which tightens the occupant restraint. The pinion is allowed to turn freely by holding the rack out of its sphere of movement until the piston, which controls the position of the rack, is caused to extend. The pinion turns a shaft which is connected to a locking reel through a connector which is movable between a connected configuration and a disconnected configuration.

Abstract: An aircraft crash sensor activates an aircrew safety device upon sensing an aircraft impact in any direction to minimize the aircrew flail envelope and reduce the possibility of injury caused by the crash. The crash sensor is useful in a plurality of different aircraft all having different characteristics and mounting orientations for the crash sensor. It includes accelerometers which sense accelerations along three orthogonal axes. The memory contains algorithms for each of a plurality of different aircraft. The memory also contains a program which converts the acceleration data measured along the sensor's axes to acceleration data on the aircraft's orthogonal X, Y and Z axes. These converted acceleration signals are input to a microcontroller which evaluates them, by analyzing them with an algorithm contained in non-volatile programmable memory, to determine when a crash has occurred.

Abstract: An aircraft crash sensor activates an aircrew safety device upon sensing an aircraft impact in any direction to minimize the aircrew flail envelope and reduce the possibility of injury caused by the crash. The crash sensor is useful in a plurality of different aircraft all having different characteristics and mounting orientations for the crash sensor. It includes accelerometers which sense accelerations along three orthogonal axes. The memory contains algorithms for each of a plurality of different aircraft. The memory also contains a program which converts the acceleration data measured along the sensor's axes to acceleration data on the aircraft's orthogonal X, Y and Z axes. These converted acceleration signals are input to a microcontroller which evaluates them, by analyzing them with an algorithm contained in non-volatile programmable memory, to determine when a crash has occurred.