Patent · US Active

Aircraft airflow modification device and vortex generator arrangement for an aircraft

US10737771B2 · kind B2 · utility

0Cited by
10References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 21, 2017
Grant dateAug 11, 2020
Priority date
Expiry dateAug 29, 2038

Classification

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

Abstract

An aircraft airflow modification device, comprising: at least one resiliently deformable base member; and at least one resiliently deformable flap member that extends from the resiliently deformable base member. Deformation of the resiliently deformable base member from a first state to a second state results in corresponding deformation of the resiliently deformable flap member from a first state to a second state.

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