Patent · US Active

Ejection seat active roll correction

US12043394B2 · kind B2 · utility

0Cited by
6References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 2, 2022
Grant dateJul 23, 2024
Priority date
Expiry dateNov 1, 2042

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05D1/46
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A roll stabilization system for an aircraft ejection seat may be provided. An integral seat sequencer may activate an ejection sequence causing an aircraft ejection seat to be ejected from an aircraft. In various instances, particularly with lighter occupants of the aircraft ejection seat, the aircraft ejection seat may begin a rotational movement. To ameliorate this rotational movement, a roll correction rocket motor is installed on the aircraft ejection seat and selectively activated by the integral seat sequencer in the event that an undesired rotational movement is detected.

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