发明名称 |
ENHANCED TEMPERATURE CONTROL ANTI-ICE NOZZLE |
摘要 |
Systems, methods, and apparatus are disclosed for preventing formation of ice on an engine. Apparatus may include a nozzle housing coupled to a compression stage of the engine and further coupled to a leading edge housing of the engine. The nozzle housing may receive gases from the compression stage of the engine. The nozzle housing may include a first nozzle that may be configured to generate a first flow pattern and may be further configured to generate a first flow of a first portion of the gases into the leading edge housing based on the first flow pattern. The nozzle housing may also include a second nozzle that includes a concentric nozzle configured to generate a second flow pattern. The second nozzle may be configured to generate a second flow of a second portion of the gases into the leading edge housing based on the second flow pattern. |
申请公布号 |
US2015260099(A1) |
申请公布日期 |
2015.09.17 |
申请号 |
US201414209434 |
申请日期 |
2014.03.13 |
申请人 |
The Boeing Company |
发明人 |
Gally Daniel H.;Seydel Joseph J.;Nyi Nyi;Wit Tristan;Davidson Joseph G. |
分类号 |
F02C7/047;B05B1/00 |
主分类号 |
F02C7/047 |
代理机构 |
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代理人 |
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主权项 |
1. An apparatus for preventing formation of ice on an engine, the apparatus comprising:
a nozzle housing having an internal cavity defining an internal volume of the nozzle housing, wherein the nozzle housing is configured to receive gases from a compression stage of the engine, and wherein the nozzle housing is further configured to provide at least some of the gases to a leading edge housing of the engine; a first nozzle included in a first portion of the nozzle housing, wherein the first nozzle is configured to generate a first flow pattern, and is further configured to generate a first flow of a first portion of the gases into an internal volume of the leading edge housing based on the first flow pattern; and a second nozzle included in a second portion of the nozzle housing, wherein the second nozzle includes a concentric nozzle configured to generate a second flow pattern, wherein the second nozzle is configured to generate a second flow of a second portion of the gases into the internal volume of the leading edge housing based on the second flow pattern. |
地址 |
Chicago IL US |