发明名称 |
Shovel nose pneumatic vortex control |
摘要 |
A system for facilitating the enhanced aerodynamic control of an aircraft having a fuselage including a forebody defining a frontal portion adapted to create a primary vortex under certain flight conditions and a rear portion. The control system comprises a contour discontinuity which is formed between the frontal and rear portions of the forebody. The contour discontinuity is sized and configured to create a secondary vortex under certain flight conditions. In addition to the contour discontinuity, the control system comprises a pressurized fluid injecting device which is disposed within the forebody of the fuselage adjacent the contour discontinuity. The pressurized fluid injecting device is used to selectively manipulate the secondary vortex to control the flight performance characteristics of the aircraft.
|
申请公布号 |
US5927645(A) |
申请公布日期 |
1999.07.27 |
申请号 |
US19980007717 |
申请日期 |
1998.01.15 |
申请人 |
NORTHROP GRUMMAN CORPORATION |
发明人 |
LATZ, JOHN PAUL |
分类号 |
B64C23/06;(IPC1-7):B64C7/00 |
主分类号 |
B64C23/06 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|