Patent · US Active

System and method for lift augmentation of aircraft wings

US11787526B2 · kind B2 · utility

1Cited by
9References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 23, 2021
Grant dateOct 17, 2023
Priority date
Expiry dateDec 23, 2041

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/10
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A system and method for lift augmentation of an aircraft having a wing with a leading edge and a trailing edge extending along a wingspan, a plurality of thrust-producing devices connected to the bottom of said wing, at least one flap connected to an inboard portion of said wing proximate the trailing edge, and an aircraft roll control device connected to said wing, wherein the improvement comprises a plurality of slipstreams associated with a plurality of thrust producing devices and a flap adaptable to deflect from a chord of the inboard portion of the wing.

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