Patent · US Active

Composite leg structure for a lightweight aircraft seat assembly

US8393574B2 · kind B2 · utility

7Cited by
5References
15Claims
0Family size

Assignee

Inventor

Key dates

Filing dateAug 28, 2008
Grant dateMar 12, 2013
Priority date—
Expiry dateJan 10, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49616
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A lightweight leg assembly for an aircraft seat assembly includes a leg frame comprising at least one leg attachment bracket and a main frame member carried by the at least one leg attachment bracket and comprising a thermoplastic material. At least one track fitting may be carried by the leg frame. A method of fabricating a leg assembly for an aircraft seat assembly is also disclosed.

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