发明名称 Compressor
摘要 A compressor is disclosed, which has an inflow channel for guiding a compression medium into a compressor housing, a pressure chamber formed within the compressor housing, and a liner segment with nozzles that transport the compression medium from the pressure chamber to a rotor. The nozzles are formed in the liner segment as a plurality of nozzles arranged in a group in fan-like manner.
申请公布号 US9175690(B2) 申请公布日期 2015.11.03
申请号 US200913123951 申请日期 2009.10.16
申请人 MTU AERO ENGINES GmbH 发明人 Schütz Gottfried;Hiller Sven-J.;Burgold Yves
分类号 F04D27/02 主分类号 F04D27/02
代理机构 Barlow, Josephs & Holmes, Ltd. 代理人 Barlow, Josephs & Holmes, Ltd.
主权项 1. A compressor having an inflow channel (110), which guides a compression medium into a pressure chamber (112) formed inside a compressor housing (111), and a liner segment (120) with a plurality of groups of nozzles, each group of nozzles comprising a plurality of nozzles, and each nozzle (123) transports the compression medium from pressure chamber (112) to a rotor, the plurality of nozzles within each respective group of nozzles being aligned adjacent to one another in a circumferential direction of the liner segment, and the groups of nozzles being circumferentially spaced apart along the liner segment, is hereby characterized in that the pressure chamber (112) is positioned between the liner segment (120) and the compressor housing (111), each nozzle (123) has an entrance section (124) and an exit section (125), the entrance section extending linearly along an entrance axis, the exit section extending linearly along an exit axis, and the entrance axis and exit axis being at an angle to one another; each nozzle (123) includes a deflection region located where the entrance section (124) and exit section (125) meet; wherein each nozzle extends from a first side of the liner segment to a second side of the liner segment, so that the entrance section (124) is in facing relation with the compressor housing (111), and the exit section (125) is in facing relation with the rotor; and wherein each nozzle directs the compression medium in a downstream direction.
地址 Munich DE