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公开(公告)号:US20050109013A1
公开(公告)日:2005-05-26
申请号:US10883987
申请日:2004-07-06
申请人: Andreas Eleftheriou , Kevin Lobo , Maurice Weinberg , Quantal Liu
发明人: Andreas Eleftheriou , Kevin Lobo , Maurice Weinberg , Quantal Liu
CPC分类号: F01D5/22 , F01D25/24 , F02K3/06 , Y02T50/671 , Y02T50/673
摘要: A casing for a gas turbine includes a construction providing improved structural efficiency. Improved load paths and means for transmitting loads in the engine case are disclosed.
摘要翻译: 用于燃气轮机的壳体包括提供改进的结构效率的结构。 公开了用于在发动机壳体中传递负载的改进的负载路径和装置。
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公开(公告)号:US20050022501A1
公开(公告)日:2005-02-03
申请号:US10628556
申请日:2003-07-29
申请人: Andreas Eleftheriou , Kevin Lobo , Maurice Weinberg , Quantai Liu
发明人: Andreas Eleftheriou , Kevin Lobo , Maurice Weinberg , Quantai Liu
CPC分类号: F01D5/22 , F01D25/24 , F02K3/06 , Y02T50/671 , Y02T50/673
摘要: A casing for a gas turbine includes a fan case, an intermediate case and a gas generator case integrated with one another.
摘要翻译: 用于燃气轮机的壳体包括彼此集成的风扇壳体,中间壳体和气体发生器壳体。
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公开(公告)号:US07370467B2
公开(公告)日:2008-05-13
申请号:US10628556
申请日:2003-07-29
CPC分类号: F01D5/22 , F01D25/24 , F02K3/06 , Y02T50/671 , Y02T50/673
摘要: A casing for a gas turbine includes a fan case, an intermediate case and a gas generator case integrated with one another.
摘要翻译: 用于燃气轮机的壳体包括彼此集成的风扇壳体,中间壳体和气体发生器壳体。
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公开(公告)号:US07765787B2
公开(公告)日:2010-08-03
申请号:US11780609
申请日:2007-07-20
IPC分类号: F02K3/02
CPC分类号: F02K3/06 , F01D25/162 , F01D25/24 , F02C7/20 , F05D2230/60 , F05D2240/122 , F05D2240/304 , Y02T50/671
摘要: A casing for a gas turbine includes a construction providing improved structural efficiency. Improved load paths and means for transmitting loads in the engine case are disclosed.
摘要翻译: 用于燃气轮机的壳体包括提供改进的结构效率的结构。 公开了用于在发动机壳体中传递负载的改进的负载路径和装置。
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公开(公告)号:US07266941B2
公开(公告)日:2007-09-11
申请号:US10883987
申请日:2004-07-06
CPC分类号: F01D5/22 , F01D25/24 , F02K3/06 , Y02T50/671 , Y02T50/673
摘要: A casing for a gas turbine includes a construction providing improved structural efficiency. Improved load paths and means for transmitting loads in the engine case are disclosed.
摘要翻译: 用于燃气轮机的壳体包括提供改进的结构效率的结构。 公开了用于在发动机壳体中传递负载的改进的负载路径和装置。
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公开(公告)号:US07770378B2
公开(公告)日:2010-08-10
申请号:US11780575
申请日:2007-07-20
CPC分类号: F02K3/06 , F01D25/162 , F01D25/24 , F02C7/20 , F05D2230/60 , F05D2240/122 , F05D2240/304 , Y02T50/671
摘要: A casing for a gas turbine includes a construction providing improved structural efficiency. Improved load paths and means for transmitting loads in the engine case are disclosed.
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公开(公告)号:US07793488B2
公开(公告)日:2010-09-14
申请号:US11780597
申请日:2007-07-20
IPC分类号: F02K3/06
CPC分类号: F01D5/22 , F01D25/24 , F02K3/06 , Y02T50/671 , Y02T50/673
摘要: A casing for a gas turbine includes a construction providing improved structural efficiency. Improved load paths and means for transmitting loads in the engine case are disclosed.
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公开(公告)号:US07739866B2
公开(公告)日:2010-06-22
申请号:US11780852
申请日:2007-07-20
CPC分类号: F02K3/06 , F01D25/162 , F01D25/24 , F02C7/20 , F05D2230/60 , F05D2240/122 , F05D2240/304 , Y02T50/671
摘要: A casing for a gas turbine includes a construction providing improved structural efficiency. Improved load paths and means for transmitting loads in the engine case are disclosed.
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公开(公告)号:US07565796B2
公开(公告)日:2009-07-28
申请号:US11780908
申请日:2007-07-20
IPC分类号: F02K3/06
CPC分类号: F02K3/06 , F01D25/162 , F01D25/24 , F02C7/20 , F05D2230/60 , F05D2240/122 , F05D2240/304 , Y02T50/671
摘要: A casing for a gas turbine includes a construction providing improved structural efficiency. Improved load paths and means for transmitting loads in the engine case are disclosed.
摘要翻译: 用于燃气轮机的壳体包括提供改进的结构效率的结构。 公开了用于在发动机壳体中传递负载的改进的负载路径和装置。
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公开(公告)号:US09394828B2
公开(公告)日:2016-07-19
申请号:US13036407
申请日:2011-02-28
CPC分类号: F02C7/08 , F05D2220/323 , F05D2230/60 , F05D2230/642 , F28D9/0018 , F28D21/001 , F28F9/0236 , F28F9/26 , F28F21/087 , F28F2230/00 , F28F2265/26 , Y10T29/49716
摘要: A gas turbine engine recuperator including a plurality of independent arcuate segments, each segment having an inlet connection member designed to sealingly engage a plenum in fluid flow communication with the compressor discharge, and an outlet connection member designed to sealingly engage a plenum containing the combustor. One of the inlet and outlet connection members is a rigid member forming a rigid connection to the respective plenum, and the other of the inlet and outlet connection members includes a flexible member and forms a floating connection to the respective plenum, the floating connection allowing relative movement between the segment and a remainder of the gas turbine engine.
摘要翻译: 一种燃气涡轮发动机换热器,包括多个独立的弧形段,每个段具有入口连接构件,其设计成密封地接合与压缩机排放流体流动连通的气室;以及出口连接构件,设计成密封地接合包含燃烧器的气室。 入口和出口连接构件中的一个是刚性构件,其形成与相应的气室的刚性连接,并且入口和出口连接构件中的另一个包括柔性构件并且形成到相应气室的浮动连接,所述浮动连接允许相对 该段与燃气涡轮发动机的其余部分之间的运动。
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