Patent · US Active

Graduated chute delay six mode ejection system

US12325525B2 · kind B2 · utility

0Cited by
5References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 21, 2023
Grant dateJun 10, 2025
Priority date
Expiry dateJul 24, 2043

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D17/74
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A method is disclosed herein. The method includes receiving, by a processor, an ejection command for ejecting an ejection seat from an aircraft; determining, by the processor, an airspeed and an altitude of the ejection seat; responsive to the altitude of the ejection seat indicating a second mode of operation, determining, by the processor, whether the airspeed of the ejection seat is at or above a first threshold and below a second threshold; and responsive to the airspeed of the ejection seat being at or above the first threshold and below the second threshold: sending, by the processor, a command to deploy a drogue parachute; and, responsive to a first predetermined time period expiring, sending, by the processor, a command to deploy a main parachute and sever the drogue parachute based on a variable drogue severance delay.

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