Patent · US Active

Attenuators for aircraft cable and ejection seat arm restraint assemblies

US11597525B2 · kind B2 · utility

1Cited by
13References
6Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 30, 2021
Grant dateMar 7, 2023
Priority date
Expiry dateMar 30, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D25/06
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An arm restraint assembly for an ejection seat may comprise a primary arm configured to pivot about a primary arm pivot joint, a first cable portion coupled to the primary arm, and an attenuator coupled to the first cable portion. The first cable portion may be configured to pivot the primary arm about the primary arm pivot joint. The attenuator may include a housing and a plunger having a head located in the housing. The head of the plunger may be biased toward a first end of the housing.

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