Exoskeleton arm aid in aircraft cockpit for high accelerations

Patent metadata

Field	Value
Publication number	US-2024253208-A1
Application number	US-202418425375-A
Country	US
Kind code	A1
Filing date	Jan 29, 2024
Priority date	Feb 1, 2023
Publication date	Aug 1, 2024
Grant date	—

Abstract

A system to assist an occupant of an aircraft during cockpit operation under high accelerations, wherein the system includes an exoskeleton arm including a plurality of joints, actuators, and bearing surfaces to support an arm of the occupant, an inertial measuring unit configured to detect kinematic data of the aircraft and transmit the kinematic data, a computing unit configured to receive the kinematic data transmitted from the inertial measuring unit, to determine an acceleration at the occupant's seat from the kinematic data, and to control the actuators of the exoskeleton arm to generate a counterforce directed against the acceleration at the occupant's seat in an amount that compensates for inertial forces of the occupant's arm due to the acceleration at the occupant's seat.

First claim

1 . A system to assist an occupant of an aircraft during cockpit operation under high accelerations, wherein the system comprises:
an exoskeleton arm comprising a plurality of joints, actuators, and bearing surfaces to support an arm of the occupant; an inertial measuring unit configured to detect kinematic data of the aircraft and to transmit the kinematic data; and a computing unit configured to:
receive the kinematic data transmitted from the inertial measuring unit;
determine an acceleration at the occupant's seat from the kinematic data; and
control the actuators of the exoskeleton arm to generate a counterforce directed against the acceleration at the occupant's seat in an amount that compensates for inertial forces of the occupant's arm due to the acceleration at the occupant's seat.

2 . The system according to claim 1 , wherein the system further comprises an inertial arm measuring unit arranged on the exoskeleton arm, the inertial arm measuring unit configured to determine kinematic data of the exoskeleton arm and transmit the kinematic data of the exoskeleton arm to the computing unit, the computing unit being further configured to determine the counterforce from the kinematic data of the aircraft detected by the inertial measuring unit and from the kinematic data of the exoskeleton arm determined by the inertial arm measuring unit, and to control the actuators of the exoskeleton arm in order to apply the counterforce as determined.

3 . The system according to claim 1 , wherein the exoskeleton arm comprises bio-sensors configured to determine action potentials of the occupant and transmit the action potentials to the computing unit, the computing unit being further configured to determine a movement of the exoskeleton arm desired by the occupant based on the action potentials determined by the bio-sensors, and to control the actuators superimposed on the counterforce in order to apply a force and/or a torque to carry out the movement of the exoskeleton arm desired by the occupant.

4 . The system according to claim 1 , wherein the computing unit is further configured to determine a spatial direction of the acceleration occurring at the occupants seat, to determine the counterforce along the spatial direction, and to control the actuators of the exoskeleton arm accordingly.

5 . The system according to claim 1 , wherein the system further comprises an optical tracking system configured to detect a current position and/or a current speed of the exoskeleton arm relative to the cockpit of the aircraft, and to transmit the current position and/or the current speed to the computing unit, the computing unit being further configured to readjust a movement of the exoskeleton arm and/or the counterforce based on the current position and/or the current speed of the exoskeleton arm.

6 . The system according to claim 1 , wherein the inertial measuring unit is intended to be arranged in the aircraft at a known distance from the occupant's seat along a longitudinal axis of the aircraft, the computing unit being further configured to calculate accelerations at the occupant's seat using the known distance and from the kinematic data of the inertial measuring unit.

7 . The system according to claim 1 , wherein the exoskeleton arm further comprises respective bearing surfaces for an upper arm and a forearm adjoining the upper arm.

8 . The system according to claim 7 , wherein the joints of the exoskeleton arm have degrees of freedom configured analogously to degrees of freedom of a human shoulder and a human elbow, such that the occupant's arm accommodated in the exoskeleton arm is capable of performing all movements possible due to its degrees of freedom in the shoulder and the elbow through the exoskeleton arm as well, and the actuators of the exoskeleton arm support all the movements by the counterforce against the acceleration as determined.

9 . An aircraft comprising a system according to claim 1 .

10 . The aircraft according to claim 9 , wherein the aircraft comprises a first exoskeleton arm and a second exoskeleton arm, wherein respective exoskeleton arms are mounted on structure of the aircraft structure at shoulder height behind the occupant's seat.

Assignees

• Deutsch Zentr Luft & Raumfahrt

Inventors

• Wolz Florian

Classifications

• B64D25/06

  Harnessing · CPC title

• B25J9/0006 Primary

  Exoskeletons, i.e. resembling a human figure · CPC title

• B64D11/00

  Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title