Patent · US Active

Aerodynamic profile with a reversibly deformable contour for aircraft, in particular for rotary wing aircraft

US8770523B2 · kind B2 · utility

1Cited by
8References
20Claims
0Family size

Assignee

Inventor

Key dates

Filing dateMay 27, 2009
Grant dateJul 8, 2014
Priority date
Expiry dateMar 1, 2030

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2027/4736
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aerodynamic profile (10) for aircraft, in particular for rotary wing aircraft, which profile (10) includes a cover skin (14, 15) on the pressure side and on the suction side, with a profile contour that is controllably formable in the rear profile region (13) by actuators (30), wherein each cover skin (14, 15) is designed as a non-shear-resistant sandwich that includes a film or foil (21, 22) which is connected to a non-shear-resistant core (20), wherein the cover skins (14, 15) are held in their profile shape by flexible webs (17).

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