A device for controlling a balance of an urban air mobility, may include a receiver configured to receive occupant information related to the urban air mobility from a cloud server; and a controller configured to control the balance of the urban air mobility according to the received occupant information.

A device for controlling a balance of an urban air mobility, may include a receiver configured to receive occupant information related to the urban air mobility from a cloud server; and a controller configured to control the balance of the urban air mobility according to the received occupant information.

A method and apparatus for protecting a passenger during a crash comprises a moveable seat with an energy absorber (EA) that allows the seat to stroke a finite distance to decelerate the passenger in a controlled manner. The seat is designed so that one of a plurality of fixed profile EA's can be selectively engaged to provide a tailored EA composite profile adapted to the occupant's weight and anticipated crash environment. The tailored EA composite profile applies a frequency matched, low onset force to the seat, which substantially eliminates problems associated with dynamic overshoot of the passenger's spine.

A pilot's seat offering an evacuation device. The seat comprises a ladder fixed to the rear of the back and covered by a detachable cover associated with the seat and deployable between a storage position retracted inside the cover and a deployed evacuation position, in which case the cover is detached. Thus, the evacuation device is incorporated harmoniously into the seat which offers a solid base for the evacuation ladder.

Described is an extendable joint (10,100) for attaching a passenger seat to a cabin floor or support structure. The extendable joint (10,100) exhibits behavior of a rigid mounting during normal usage, such as when carrying or securing passengers or luggage. However, if a force threshold is exceeded, such as with an emergency situation, the extendable joint (10,100) may lengthen to absorb energy applied from the cabin floor through the passenger seat and vice versa. Additional force damping mechanisms may also be incorporated into the joint to further absorb, distribute, or reduce loadings that may otherwise separate the passenger seat from the floor or support structure.

Described is an extendable joint (10,100) for attaching a passenger seat to a cabin floor or support structure. The extendable joint (10,100) exhibits behavior of a rigid mounting during normal usage, such as when carrying or securing passengers or luggage. However, if a force threshold is exceeded, such as with an emergency situation, the extendable joint (10,100) may lengthen to absorb energy applied from the cabin floor through the passenger seat and vice versa. Additional force damping mechanisms may also be incorporated into the joint to further absorb, distribute, or reduce loadings that may otherwise separate the passenger seat from the floor or support structure.

An innovative capsule type flying vehicle with vertical takeoff and landing, which belongs to the field of devices for air transportation, preferably used for individual transportation, but optionally can be configured for the transportation of two people, where the great inconvenience of products of the same purpose found in the state of technology is the fact that they leave the user exposed and unprotected; differently, the object of this present request consists of a propelled flying vehicle having an aerodynamic envelope and structure, shaped as an ogive capsule, manufactured using light, reliable, safe and easily controllable material, capable of taking off and landing vertically and hovering, flying and maneuvering over great distances and altitudes; consisting of a pod-shaped capsule (1) formed by a base (2), head (3), entry door (4) with a windshield (4A) and a support to fix the propulsion engine.

A method and apparatus for protecting a passenger during a crash comprises a moveable seat with an energy absorber (EA) that allows the seat to stroke a finite distance to decelerate the passenger in a controlled manner. The seat is designed so that one of a plurality of fixed profile EA's can be selectively engaged to provide a tailored EA composite profile adapted to the occupant's weight and anticipated crash environment. The tailored EA composite profile applies a frequency matched, low onset force to the seat, which substantially eliminates problems associated with dynamic overshoot of the passenger's spine.

The present disclosure discloses a landing aid for a parachutist, in particular for a tandem jump or landing with heavy equipment, having an air bag, which protects the parachutist during landing, wherein the air bag has an inflow opening through which air can flow into the air bag in order to fill it by means of the airstream. It is provided that the landing aid comprises a spring element, by means of which the inflow opening is held in the correct position with respect to the air flow and/or an unpacking process of the air bag is supported.

The present disclosure discloses a landing aid for a parachutist, in particular for a tandem jump or landing with heavy equipment, having an air bag, which protects the parachutist during landing, wherein the air bag has an inflow opening through which air can flow into the air bag in order to fill it by means of the airstream. It is provided that the landing aid comprises a spring element, by means of which the inflow opening is held in the correct position with respect to the air flow and/or an unpacking process of the air bag is supported.