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
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
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