Flow control device and method for aircraft and missile forebody
US9429400B1 · kind B1 · utility
10Cited by
14References
13Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 9, 2009 |
| Grant date | Aug 30, 2016 |
| Priority date | — |
| Expiry date | Dec 16, 2032 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/10
- WIPO fieldOther special machines
- WIPO sectorMechanical engineering
Abstract
A forebody flow control system and more particularly an aircraft or missile flow control system for enhanced maneuverability and stabilization utilizes various types of sensors and various types of activatable flow effectors to maneuver the aircraft or missile with the help of a control system. A method of operating the flow control system is also disclosed.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.