Patent · US Active

Leading-edge component for an aircraft

US11230365B2 · kind B2 · utility

0Cited by
1References
12Claims
0Family size

Assignee

Inventor

Key dates

Filing dateApr 20, 2020
Grant dateJan 25, 2022
Priority date
Expiry dateApr 20, 2040

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/30
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A leading-edge component for an aircraft includes at least a part of a flow body having a front skin and at least one rib, wherein the front skin includes a top section, a bottom section and a leading edge arranged therebetween, wherein the rib extends from the bottom section to the top section, wherein the rib includes at least one kink separating the rib into a first section and at least one second section, and wherein main extension planes of the first section and the at least one second section enclose an angle of at least 10°.

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