B64D25/06

Device for Propelling a Passenger
20190161188 · 2019-05-30 · ·

The invention relates to a device for propelling a passenger, comprising a body arranged to receive said passenger and cooperating with a fuel-fed thrust unit. The arrangement of such a device enables great freedom of movement in the air. More specifically, the thrust unit comprises at least one thrust sub-unit, each advantageously comprising at least two thrusters and secondary course-correction and/attitude-correction thrusters.

Inertia reel mounts and mounting arrangements

An inertia reel mount for a seat includes a slide, a carriage arranged to support a seatbelt inertia reel, and a damper. The carriage is movable between first and second positions relative to the slide. The damper is fixed to the slide, is arranged between the carriage and the slide to oppose movement of the carriage, and is arranged to absorb kinetic energy from the carriage from sudden acceleration of a seat occupant secured in the seat by the seatbelt as the carriage moves from the first position to the second position.

INERTIA REEL MOUNTS AND MOUNTING ARRANGEMENTS
20180339776 · 2018-11-29 ·

An inertia reel mount for a seat includes a slide, a carriage arranged to support a seatbelt inertia reel, and a damper. The carriage is movable between first and second positions relative to the slide. The damper is fixed to the slide, is arranged between the carriage and the slide to oppose movement of the carriage, and is arranged to absorb kinetic energy from the carriage from sudden acceleration of a seat occupant secured in the seat by the seatbelt as the carriage moves from the first position to the second position.

ELECTRONIC MODULE ASSEMBLY FOR CONTROLLING AIRCRAFT RESTRAINT SYSTEMS
20180244229 · 2018-08-30 ·

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
20180244229 · 2018-08-30 ·

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.

Aircraft having at least one control device for controlling inflation of an inflatable safety bag, and an associated method of controlling inflation of an inflatable safety bag
10040572 · 2018-08-07 · ·

A control device including at least one control member for measuring an acceleration of an aircraft, for generating an inflation order, and for transmitting the inflation order to an inflation member, the inflation member serving to inflate at least one inflatable safety bag, the control device, the inflation member and the inflatable bag being arranged together on a single seat of the aircraft. Such a control device includes at least one readying system connected to the at least one control member, the readying system comprising: at least a first sensor suitable for continuously measuring a first current acceleration of the aircraft relative to at least one axis; and at least one switch that is controllable as a function of the first current acceleration of the aircraft as measured by the first sensor.

Aircraft having at least one control device for controlling inflation of an inflatable safety bag, and an associated method of controlling inflation of an inflatable safety bag
10040572 · 2018-08-07 · ·

A control device including at least one control member for measuring an acceleration of an aircraft, for generating an inflation order, and for transmitting the inflation order to an inflation member, the inflation member serving to inflate at least one inflatable safety bag, the control device, the inflation member and the inflatable bag being arranged together on a single seat of the aircraft. Such a control device includes at least one readying system connected to the at least one control member, the readying system comprising: at least a first sensor suitable for continuously measuring a first current acceleration of the aircraft relative to at least one axis; and at least one switch that is controllable as a function of the first current acceleration of the aircraft as measured by the first sensor.

Aircraft bench organized to receive a variable number of passengers

An aircraft bench having passenger-receiving locations each defined by two seating plates for receiving a respective buttock of a passenger. Each of the seating plates is individually mounted to pivot on a front spar of the bench and each is individually supported in suspension via its rear edge by a respective energy absorber. The bench is fitted with a plurality of adjacent sets of straps that are lockable together in pairs by a buckle, with locking points that are selectively usable for belting in a passenger depending on the passenger-receiving location selected by the passenger.

Aircraft bench organized to receive a variable number of passengers

An aircraft bench having passenger-receiving locations each defined by two seating plates for receiving a respective buttock of a passenger. Each of the seating plates is individually mounted to pivot on a front spar of the bench and each is individually supported in suspension via its rear edge by a respective energy absorber. The bench is fitted with a plurality of adjacent sets of straps that are lockable together in pairs by a buckle, with locking points that are selectively usable for belting in a passenger depending on the passenger-receiving location selected by the passenger.

Mechanically Actuated Cargo Restraint System
20180111543 · 2018-04-26 ·

A mechanically actuated cargo restraint system for a vehicle includes a rotatable reel in a frame, a first flexible tether, a base and a pawl. The frame includes a cog having a single tooth. The first flexible tether has a first end coupled to the rotatable reel and a second end capable of being coupled to one of a vehicle and a cargo item. The first flexible tether is windable around the rotatable reel. The base rotate with the reel. The pawl is pivotally connected to the base, and is biased in a first position that allows rotation of the pawl with respect to the cog. The pawl moves to a second position responsive to centrifugal force associated with a velocity of rotation of the rotatable reel exceeding a threshold. The pawl engages the cog in the second position to inhibit relative movement of the pawl with respect to the cog.