Multi-chamber airbag systems for use in aircraft and other vehicles are described herein. In some embodiments, an occupant restraint system includes a multi-chamber airbag that deploys from an occupant restraint (e.g., a lap seat belt) in an aircraft. The multi-chamber airbag can include a first portion that inflates generally upward in front of the occupant's torso, and a second portion that inflates in front of the first portion. The first portion and/or the second portion can include multiple chambers (e.g., generally cylindrical-shaped chambers) that, when inflated, provide the airbag with a shape and/or contact surfaces which can help to maintain the position of the airbag between the occupant and a strike object or hazard. In other embodiments, multi-chamber airbags configured in accordance with the present disclosure can me mounted to a structure (e.g., a monument, console, seat back, etc.) positioned generally in front of the occupant. The structure-mounted airbag can deploy generally toward the occupant in the event of a vehicle impact or other potentially harmful event to protect the occupant from impact injury.

Methods and apparatus for determining seatbelt status are disclosed. An example system includes a plurality of seats including seatbelts. Each of the seatbelts includes a sensor to detect a position of a respective seatbelt, the position including at least one of a fastened position or an unfastened position, and a transceiver to wirelessly communicate the position of the respective seatbelt. The system includes a remote monitoring unit to receive the positions of the seatbelts. The remote monitoring unit is to determine if one or more seats are occupied and, in response to determining that one or more seats are occupied, the remote monitoring unit is to display an overview the seats and the respective positions of the seatbelts for the one or more occupied seats.

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.

PORTABLE PERSONAL AIRBAG FOR AIRCRAFTS for the use in an air transport vehicle, such as airplanes, helicopters and others, seeking to solve the problem regarding user protection, considering its position in the chair, the space between chairs, the main protection area for the user, activation readiness, weight of the object, etc. Considering also that in cases of collision in aircrafts, the danger to life is much higher when compared to land accidents, therefore, we present the safety devices. The object of this application is an inflatable bag housed in a case manufactured with a compatible material, the format of the inflatable bag must be specific to fill the space between the passenger and the front seat, seeking to protect the head, abdomen and legs and the air bag can be empty out later by the user to be reused, only by installing another air supply unit. The airbag can provide an electronic information transmission device, via satellite, for example, with flash or compatible memory, and it can be a geolocator, for example, which is activated due to a condition established and predetermined, which can serve as a locator in searches, in case of accidents in remote places, such as the sea.

Various embodiments of vehicle occupant safety systems having extendable restraints for use with, for example, airbags are described herein. In one embodiment, for example, the disclosed technology includes a 2-point occupant restraint that secures an occupant in an aircraft seat. In this embodiment, the aircraft seat is positioned in a seating area that includes a forward monument housing a stowed airbag. In the event of a crash or other significant dynamic event that causes, for example, a rapid deceleration of the aircraft above a preset magnitude, the airbag deploys between the occupant and the monument as the dynamic forces cause the occupant to pitch forward. The forward momentum of the occupant's body creates a significant tension load in the 2-point restraint, which causes the restraint to extend by a preset amount, thereby allowing the occupant to move forward in the seat more than the occupant would have moved had the occupant been wearing a conventional, non-extending 2-point restraint. Although the occupant is allowed to move forward, the occupant remains secured to the extended restraint by means of non-extending webbing that is secured around the waist of the occupant. Allowing the occupant to move forward in this manner enables the occupant's upper torso to impact the airbag at a reduced or otherwise more favorable angle. This can reduce both the speed and the angle at which the occupant's head impacts the airbag, thereby reducing the likelihood of injury.

Methods and apparatus for determining seatbelt status are disclosed. An example seatbelt system for a mass transit vehicle includes a first seatbelt of a first seat that includes a first buckle and a first magnetically-responsive switch to detect a first tongue when the first seatbelt is in a fastened position. The example apparatus includes a second seatbelt of a second seat that includes a second buckle and a second magnetically-responsive switch to detect a second tongue when the second seatbelt is in the fastened position. The example apparatus includes a remote monitoring unit to indicate, when the first seat is occupied, if the first seatbelt is in the fastened positioned or an unfastened position. The remote monitoring unit is to indicate, when the second seat is occupied, if the second seatbelt is in the fastened positioned or the unfastened position.

Vehicle occupant restraint systems that include a compact, web-mounted airbag that can be deployed during a crash event are described herein. In some embodiments, the web (e.g., a shoulder belt) passes through the stowed airbag during normal use and, when the airbag inflates and deploys, the airbag extends along the length of the web (for example, along the entire length, or at least most of the length, of the web) to protect the occupant. In some embodiments, the restraint systems include shoulder belts having first and second overlapping web portions, and when the airbag inflates and deploys, the airbag extends along the length of the first web portion between the first web portion and the second web portion.

An energy absorbing system that is adapted for absorbing energy of an object in a vehicle in a crash situation by decreasing acceleration and force acting on the object in the crash situation, the energy absorbing system comprising at least one plastically deformable energy absorber that is plastically deformable in the crash situation. A mass-dependent self-adjusting mechanism is provided, the mass-dependent self-adjusting mechanism being adapted for adjusting, on the basis of an underlying mass of the object, a required compensation force that is to be provided by the energy absorbing system in the crash situation for plastically deforming the at least one plastically deformable energy absorber in order to decrease the acceleration and force acting on the object.

Structure mounted airbag assemblies and associated systems and methods are described herein. An airbag system configured in accordance with an embodiment of the present disclosure can include, for example, a housing having a cavity and an opening in communication with the cavity, an airbag assembly within the cavity, and an inflator operably coupled to the airbag assembly. The airbag assembly can include an airbag configured to deploy through the opening of the housing during a crash event. The airbag system can further include a door removably positioned across the opening and configured to move away from the opening during airbag deployment. The housing can be affixed to an interior portion of an aircraft, forward of and offset from an aircraft seat.

A system for deploying an airbag when an unmanned aerial vehicle (UAV) has failed or is no longer able to sustain flight, comprising a triggering means which releases compressed air into a bag or bags which are configured to expand around the UAV for the purpose of reducing the deceleration forces of the UAV on impact. UAV's are provided that are configured with a system that includes a triggering mechanism that deploys one or more bags when there is a failure or when flight is no longer sustainable.