发明名称 |
Inlet icing protection simulation system |
摘要 |
A method and apparatus for generating a flow of heated air (124) in an airfoil model of an inlet (104) of an aircraft (108) engine. Heated air (124) is sent into a duct system associated with the airfoil model (110) of the inlet (104) of the aircraft (108) engine. The heated air (124) is circulated within the airfoil model (110) of the inlet (104) of the aircraft (108) engine using the duct system in a manner that simulates air flowing in the inlet (104) of the aircraft (108) engine. |
申请公布号 |
EP2703291(A2) |
申请公布日期 |
2014.03.05 |
申请号 |
EP20130174077 |
申请日期 |
2013.06.27 |
申请人 |
THE BOEING COMPANY |
发明人 |
MEIS, CHARLES STEVEN;HASS, DAVID CHARLES |
分类号 |
B64D15/04 |
主分类号 |
B64D15/04 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|