Patent · US Active

Space saver fitting for ejection seat catapult

US11370553B2 · kind B2 · utility

0Cited by
10References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 28, 2020
Grant dateJun 28, 2022
Priority date
Expiry dateDec 31, 2040

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D11/0616
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A fitting for use with an ejection seat system of an aircraft includes a fitting bar configured to extend across a top of a catapult of the ejection seat system and defining an angled slot configured to receive a portion of a gas port of the ejection seat system. The fitting further includes a first leg and a second leg coupled to and extending away from the fitting bar and configured to be pivotally coupled to a smokestack structure of the ejection seat system.

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