Airfoil with adjustable tail flap
US9469354B1 · kind B1 · utility
Assignee
Inventor
Key dates
| Filing date | Jun 29, 2015 |
| Grant date | Oct 18, 2016 |
| Priority date | — |
| Expiry date | Jun 29, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T10/82
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An adjustable airfoil assembly attached to a front fascia of a vehicle. The airfoil assembly includes an airfoil wing and a flap pivotally connected to the airfoil wing. An actuator is operatively attached to the flap to selectively pivot the flap upwardly and downwardly to adjust downforce applied by the airfoil assembly to the front end of the vehicle. The wing is a fiber reinforced polymeric member fixedly attached to the front fascia by a plurality of posts connected to the front fascia. The flap has a top surface extending from the flat top surface of the wing to a rear edge of the flap and a base surface extending from the convex bottom surface to the rear edge of the flap.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.