B64D25/06

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
20170008641 · 2017-01-12 ·

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
20170008641 · 2017-01-12 ·

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.

SEAT RESTRAINT SYSTEM

A seat restraint system holds a user to a seating rig using multiple restraints. These restraints can be released simultaneously using a release actuation system, thereby quickly freeing the user from the seating rig. Certain types of restraints are extendable relative to the seating rig between retracted and extended positions to facilitate freedom of movement of the user. The release actuation system allows the restraints to extend without unintentional actuation of the release mechanism. The release actuation system allows the restraints to be released regardless of the position (e.g., retracted, extended, therebetween) of the extendable restraints.

SEAT RESTRAINT SYSTEM

A seat restraint system holds a user to a seating rig using multiple restraints. These restraints can be released simultaneously using a release actuation system, thereby quickly freeing the user from the seating rig. Certain types of restraints are extendable relative to the seating rig between retracted and extended positions to facilitate freedom of movement of the user. The release actuation system allows the restraints to extend without unintentional actuation of the release mechanism. The release actuation system allows the restraints to be released regardless of the position (e.g., retracted, extended, therebetween) of the extendable restraints.

Drone Taxi System for Ground-Level Personal Transportation
20260103288 · 2026-04-16 ·

Systems and methods for a drone taxi system for ground-level transportation are disclosed. The system includes a multi-rotor drone apparatus capable of carrying individuals at low altitudes, approximately 1-2 feet off the ground. The system includes advanced stabilization and obstacle detection capabilities, a secure harness with a quick-release mechanism, and an inflatable safety vest that activates during emergencies. Controlled via a smartphone application, the system enables users to request drone rides, map routes, and view trip status in real-time. The drone ensures safe and efficient transit over short distances, combining the functionality of ride-sharing platforms with the experience of low-altitude travel. This system addresses urban mobility challenges, offering a safe, efficient, and eco-friendly alternative to traditional ground-based transportation methods while minimizing risks and maximizing convenience for users.

Drone Taxi System for Ground-Level Personal Transportation
20260103288 · 2026-04-16 ·

Systems and methods for a drone taxi system for ground-level transportation are disclosed. The system includes a multi-rotor drone apparatus capable of carrying individuals at low altitudes, approximately 1-2 feet off the ground. The system includes advanced stabilization and obstacle detection capabilities, a secure harness with a quick-release mechanism, and an inflatable safety vest that activates during emergencies. Controlled via a smartphone application, the system enables users to request drone rides, map routes, and view trip status in real-time. The drone ensures safe and efficient transit over short distances, combining the functionality of ride-sharing platforms with the experience of low-altitude travel. This system addresses urban mobility challenges, offering a safe, efficient, and eco-friendly alternative to traditional ground-based transportation methods while minimizing risks and maximizing convenience for users.

IMPACT- AND BLAST-RESISTANT AIRCRAFT SEAT
20260116549 · 2026-04-30 ·

This invention provides, in some embodiments, an impact- and blast-resistance improved aircraft pilot chair, which is able to provide improved protection to a pilot, from exposure to significant G forces and/or exposure to projectiles including projectiles penetrating the aircraft and/or effects of pilot chair ejection and/or effects of aircraft crash

IMPACT- AND BLAST-RESISTANT AIRCRAFT SEAT
20260116549 · 2026-04-30 ·

This invention provides, in some embodiments, an impact- and blast-resistance improved aircraft pilot chair, which is able to provide improved protection to a pilot, from exposure to significant G forces and/or exposure to projectiles including projectiles penetrating the aircraft and/or effects of pilot chair ejection and/or effects of aircraft crash