Patent · US Active

Rotorcraft fuel system having enhanced crash resistance

US10196151B2 · kind B2 · utility

3Cited by
7References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 2, 2016
Grant dateFeb 5, 2019
Priority date
Expiry dateFeb 25, 2037

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C27/04
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A rotorcraft includes a fuselage having a fuel tank receiving assembly with a fuel tank positioned therein. The fuel tank including a plurality of interconnected fuel bags operable to contain liquid fuel. A network of straps is disposed about the fuel tank forming a restraint assembly. The network of straps includes at least one perimeter strap extending at least partially about at least two fuel bags and at least one surrounding strap extending at least partially about the at least two fuel bags. The at least one perimeter strap has at least two intersections with the at least one surrounding strap.

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