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公开(公告)号:US08201389B2
公开(公告)日:2012-06-19
申请号:US11543793
申请日:2006-10-06
IPC分类号: F02C7/06
CPC分类号: F01D25/18
摘要: A single oil nozzle unit is mounted in a bearing compartment of a gas turbine engine for providing multiple individual jets for the individual bearing components in the bearing compartment.
摘要翻译: 单个油嘴单元安装在燃气涡轮发动机的轴承室中,用于为轴承室中的各个轴承部件提供多个单独的喷嘴。
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公开(公告)号:US07797922B2
公开(公告)日:2010-09-21
申请号:US11757648
申请日:2007-06-04
申请人: Andreas Eleftheriou , David Denis , Denis Leclair , Yves Roussel
发明人: Andreas Eleftheriou , David Denis , Denis Leclair , Yves Roussel
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 an aircraft turbine bypass engine comprises a splitter having slots to receive and be welded to a plurality of struts extending between an outer ring and an inner hub of the casing.
摘要翻译: 用于飞机涡轮机旁路引擎的壳体包括具有狭槽的分离器,其具有接收并焊接到在壳体的外环和内毂之间延伸的多个支柱。
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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:US20080086882A1
公开(公告)日:2008-04-17
申请号:US11537903
申请日:2006-10-02
申请人: Andreas Eleftheriou , Stevan Bokan , Jason Fish , Steven Hunt
发明人: Andreas Eleftheriou , Stevan Bokan , Jason Fish , Steven Hunt
IPC分类号: B23P15/04
CPC分类号: F01D25/24 , F05D2230/232 , F05D2230/26 , F05D2240/14 , F05D2250/231 , F05D2250/232 , Y02T50/671 , Y10T29/4932
摘要: The method comprises flowforming at least one section of the preform and then welding at least one additional element to the at least one flowformed section.
摘要翻译: 该方法包括流动成形预制件的至少一个部分,然后将至少一个附加元件焊接到至少一个流动部分。
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