Patent · US Active

Aircraft interior flooring systems

US10046847B2 · kind B2 · utility

3Cited by
41References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 11, 2018
Grant dateAug 14, 2018
Priority date
Expiry dateJan 11, 2038

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D9/003
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft flooring system for an aircraft fuselage adapted to secure a payload component may include first and second seat tracks extending longitudinally with respect to the aircraft fuselage, the first and second seat tracks being spaced from one another; and an intercostal assembly extending between the first and second seat tracks. The intercostal assembly can include a first intercostal having a center member having a first end and a second end and a top flange including a mounting region between the first and second ends; and at least first and second tab members. The first tab member can be coupled to the top flange toward the first end of the center member and the second tab member can be coupled to the top flange toward the second end of the center member. The first and second tab members can extend beyond the first and second ends of the center member, respectively, and be configured to be coupled to the first and second seat tracks.

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