Abstract:
An electronic module assembly (EMA) for use in controlling one or more personal restraint systems. A programmed processor within the EMA is configured to determine when a personal restraint system associated with each seat in a vehicle should be deployed. In addition, the programmed processor is configured to perform a diagnostic self-test to determine if the EMA and the personal restraint systems are operational. In one embodiment, results of the diagnostic self-test routine are displayed on a display included on the electronic module assembly. In an alternative embodiment, the results of the diagnostic self-test routine are transmitted via a wireless transceiver to a remote device. The remote device can include a wireless interrogator or can be a remote computer system such as a cabin management computer system.
Abstract:
An electronic module assembly (EMA) for use in controlling one or more personal restraint systems. A programmed processor within the EMA is configured to determine when a personal restraint system associated with each seat in a vehicle should be deployed. In addition, the programmed processor is configured to perform a diagnostic self-test to determine if the EMA and the personal restraint systems are operational. In one embodiment, results of the diagnostic self-test routine are displayed on a display included on the electronic module assembly. In an alternative embodiment, the results of the diagnostic self-test routine are transmitted via a wireless transceiver to a remote device. The remote device can include a wireless interrogator or can be a remote computer system such as a cabin management computer system.
Abstract:
Airbags for use in aircraft and other vehicles are described herein. In some embodiments, an airbag can deploy from a structure forward of a seated occupant at a generally upward angle relative to a longitudinal axis of the aircraft. The distal end portion of the airbag can include a recessed impact surface portion configured to receive the head and/or neck of the seat occupant.
Abstract:
An airbag assembly for leg flail protection and associated systems and methods are described herein. An airbag system configured in accordance with an embodiment of the present technology can include, for example, a housing having a cavity and an opening in communication with the cavity, an airbag stowed within the cavity, and an inflator operably coupled to the airbag. The airbag can be configured to deploy through the opening of the housing during a crash or other significant dynamic event. The airbag can deploy outwardly from the side-facing seat to reduce occupant leg rotation during the crash or other significant dynamic event. The airbag can be pushed out of the housing before it is fully inflated. The airbag can be stowed and include folded first and second opposing side portions such that when the airbag is deployed, the portion nearest the occupant unfurls toward the occupant prior to the other portion farthest from the occupant unfurling in a direction away from the occupant.
Abstract:
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.
Abstract:
A system for testing a number of electronic module assemblies (EMAs) that control one or more personal restraint systems. A programmed processor with a computer system transmits signals that instruct the EMAs to perform a diagnostic self-test. The results of the self-test are received by the computer system and stored in a computer readable memory. In one embodiment, the computer system is a cabin management computer system for use on an aircraft.
Abstract:
Buckle assemblies with dual release features and associated systems and methods are disclosed herein. In one embodiment, a buckle assembly is configured to detachably engage latch plates. The buckle assembly can include a top cover and a bottom housing collectively defining an operation space; a load plate having a plurality of apertures, an actuator configured to connect with the top cover, a plurality of pawls configured to operably enter the corresponding apertures so as to secure a plurality of latch plates, a release ring positioned adjacent to the pawls and connected with a release cord. The latch plates can be released by rotating the top cover or pulling the release cord.
Abstract:
Tensioning apparatuses for occupant restraint systems and associated systems and methods. In one embodiment, an occupant restraint system for a vehicle can include a flexible web configured to extend across at least a portion of an occupant seated in the vehicle and an electrically actuated web retractor operably coupled to a proximal end portion of the web. The web retractor is configured to automatically wind and unwind the web. The system also includes an acceleration sensor operably coupled to the electrically actuated web retractor. The acceleration sensor is configured to send an electrical signal to the web retractor in response to a vehicle acceleration above a preset magnitude. In response to the signal, the web retractor is configured to (a) retract the web, and/or (b) at least temporarily prevent the web from moving inwardly or outwardly.
Abstract:
A buckle assembly for a vehicle restraint system where the buckle assembly is adapted to receive a plurality of belt connectors, with the belt connectors being simultaneously released upon moving at least one handle to a release position.
Abstract:
Inflator connectors for inflatable personal restraints and associated systems and methods are described herein. An inflator connector configured in accordance with an embodiment of the present technology, for example, can include a body having an attachment portion and a sleeve portion and a coupling rotatably received in the sleeve portion. The attachment portion of the body can include a first bore having a first engagement feature positioned toward a first opening for operably engaging at least one of an inflator and a gas tube. The sleeve portion can include a second bore in fluid communication with the first bore. The coupling can include a second engagement feature positioned toward a second opening for operably engaging the other of the inflator and the gas tube.