Patent · US Active

Heated leading edge structure for an aircraft

US11807369B2 · kind B2 · utility

0Cited by
3References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 21, 2022
Grant dateNov 7, 2023
Priority date
Expiry dateMar 21, 2042

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C3/28
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A heated leading edge structure for an aircraft, including a leading edge panel having an outer surface configured to be contacted by an ambient flow, and an inner surface opposite the outer surface, and including a heater device mounted to the inner surface of the leading edge panel for heating of the leading edge panel. The heater device is mounted to the inner surface of the leading edge panel in a detachable manner to provide a simple, lightweight and cost-efficient leading edge structure that enables a simple, quick and efficient maintenance.

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