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 代理人
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