-
公开(公告)号:USD859471S1
公开(公告)日:2019-09-10
申请号:US29644877
申请日:2018-04-20
-
公开(公告)号:US20150322850A1
公开(公告)日:2015-11-12
申请号:US14274054
申请日:2014-05-09
发明人: Harsha Vardhana , Daniel Edward Loringer , Suresha Kumar Panambur , Paulraj Ramasamy , Raghav Shrikant Kulkarni , Krishna Lakshminarasimhan , Amol Muralidhar Petakar
CPC分类号: F02C6/12 , F01D15/02 , F01D21/045 , F01D25/005 , F01D25/166 , F01D25/26 , F02B37/00 , F02B39/005 , F02B39/08 , F05D2220/40 , F05D2230/53 , F05D2240/14 , F05D2240/24 , F05D2260/232 , F05D2300/10 , F05D2300/518
摘要: Various methods and systems are provided for a turbocharger comprising a turbine disc rotatable about a rotational axis of the turbocharger, a compressor wheel mechanically coupled to the turbine disc via a shaft, a compressor casing including an air inlet and a blower casing formed as one piece, the air inlet configured to admit air to the compressor wheel, and a turbine casing housing the turbine disc, the turbine casing including a shroud surrounding the turbine disc.
摘要翻译: 提供了用于涡轮增压器的各种方法和系统,所述涡轮增压器包括可围绕涡轮增压器的旋转轴线旋转的涡轮盘,通过轴机械联接到涡轮盘的压缩机叶轮,包括空气入口的压缩机壳体和形成为一体式的鼓风机壳体 ,空气入口构造成允许空气进入压缩机叶轮,以及容纳涡轮盘的涡轮机壳体,涡轮壳体包括围绕涡轮盘的护罩。
-
公开(公告)号:US08469657B2
公开(公告)日:2013-06-25
申请号:US13671636
申请日:2012-11-08
发明人: Anthony Holmes Furman , Kendall Roger Swenson , Daniel Edward Loringer , Suresha Kumar Panambur
IPC分类号: F01D11/11
CPC分类号: F02B37/00 , F01D1/06 , F01D25/16 , F02C6/12 , F05D2220/40 , F05D2240/53 , F16C17/10 , F16C2360/24
摘要: A turbocharger system, in certain embodiments, includes a compressor, a turbine, a shaft of common diameter coupling the compressor to the turbine, and a first fluid film bearing disposed about the shaft at a compressor end portion of the shaft. The system also includes a second fluid film fixed pad bearing disposed about the shaft at a turbine end portion of the shaft, wherein the first and second fluid film fixed pad bearings have different clearance ratios, effective lengths, or both, relative to one another. The system, in some embodiments, includes a compressor fluid film fixed pad bearing and a turbine fluid film fixed pad bearing, wherein the compressor and turbine fluid film fixed pad bearings have different clearance ratios and effective lengths, relative to one another.
摘要翻译: 在某些实施例中,涡轮增压器系统包括压缩机,涡轮机,将压缩机联接到涡轮机的共同直径的轴,以及在轴的压缩机端部处围绕轴布置的第一流体膜轴承。 该系统还包括在轴的涡轮机端部处围绕轴布置的第二流体膜固定垫轴承,其中第一和第二流体膜固定垫轴承具有彼此不同的间隙比,有效长度或两者。 在一些实施例中,该系统包括压缩机流体膜固定垫轴承和涡轮流体膜固定垫轴承,其中压缩机和涡轮流体膜固定垫轴承相对于彼此具有不同的间隙比和有效长度。
-
公开(公告)号:USD818502S1
公开(公告)日:2018-05-22
申请号:US29548899
申请日:2015-12-17
-
-
-