Patent · US Active

Control device and method for an aircraft

US12370984B2 · kind B2 · utility

0Cited by
10References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 27, 2023
Grant dateJul 29, 2025
Priority date
Expiry dateFeb 6, 2044

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05G2505/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A control device for an aircraft is disclosed including a push-button switch that is configured to be held in a depressed position by a pilot during taxiing of the aircraft. The push-button switch is configured to return automatically to a released position if it is not held in the depressed position by the pilot. The control device is configured to output a command for braking to a braking system of the aircraft, if the push-button switch moves to the released position during taxiing of the aircraft and does not return to the depressed position within a set time. The button may be provided on a tiller. A method of detecting on-board pilot incapacitation during an aircraft taxi phase is also disclosed.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.