发明名称 |
COMPRESSED-AIR SYSTEM AND COMPRESSED-AIR UNIT |
摘要 |
PROBLEM TO BE SOLVED: To provide a de-icing and surge control device capable of controlling surge by efficiently and rapidly de-icing an inlet in a compressor of an airplane. SOLUTION: A housing 40 comprises a diffuser shroud 68 and a heating plenum 72 formed by a heating housing part 46. The diffuser shroud 68 provides a curved annular wall 70 gradually widening to the radial outer side as it axially extends from the end of an impeller. A relatively short duct 30 connects an outlet 22 to the inlet of the heating plenum to flow a fluid therein. Consequently, the de-icing and surge control can be quickly performed. COPYRIGHT: (C)2007,JPO&INPIT
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申请公布号 |
JP2007132344(A) |
申请公布日期 |
2007.05.31 |
申请号 |
JP20060297277 |
申请日期 |
2006.11.01 |
申请人 |
HAMILTON SUNDSTRAND CORP |
发明人 |
MCAULIFFE CHRISTOPHER;BEERS CRAIG M |
分类号 |
F04D27/00;F04D27/02;F04D29/46;F04D29/58 |
主分类号 |
F04D27/00 |
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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