Aerodynamic profile with a reversibly deformable contour for aircraft, in particular for rotary wing aircraft
US8770523B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | May 27, 2009 |
| Grant date | Jul 8, 2014 |
| Priority date | — |
| Expiry date | Mar 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.