发明名称 |
AIRCRAFT ANTI-ICING SYSTEMS HAVING DEFLECTOR VANES |
摘要 |
Apparatus and methods to lower peak temperatures and improve performance of aircraft anti-icing systems are described herein. One described example apparatus includes a skin on an inlet side of a nacelle of an aircraft defining an annular chamber, a gas delivery system disposed within the annular chamber to provide a first gas to mix with and entrain a second gas in the annular chamber to define a flow through the annular chamber, and a deflector vane disposed within the annular chamber to redirect the flow through the annular chamber. The second gas is at a different temperature from the first gas. |
申请公布号 |
CA2865853(A1) |
申请公布日期 |
2015.07.14 |
申请号 |
CA20142865853 |
申请日期 |
2014.10.02 |
申请人 |
THE BOEING COMPANY |
发明人 |
JOHNSON, RICK A.;PHAM, VICTOR D.;GALLY, DANIEL H.;SEYDEL, JOSEPH JAMES;NATSUI, EDWARD CHARLES |
分类号 |
B64D33/02;B64D15/04;B64D29/00;F01D25/02;F02C7/047 |
主分类号 |
B64D33/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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