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公开(公告)号:US20180128123A1
公开(公告)日:2018-05-10
申请号:US15344185
申请日:2016-11-04
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Thomas Bruce Avis , Michael Dreher , Erik R. Granstrand
Abstract: Disclosed is a lubricant supply system, for a bearing damper in a bearing housing, the bearing housing in an engine bearing compartment of a gas turbine engine, the bearing compartment rotatably supporting an engine component, including a first interface, a second interface, a bearing supply conduit fluidly coupled to the second interface and extending from the first interface to the second interface, the bearing supply conduit supplying lubricant to the bearing housing, a damper supply conduit located within the bearing supply conduit, extending between the interfaces, the damper supply conduit supplying lubricant to the bearing damper, and fluid in the bearing supply conduit is capable of insulting fluid in the damper supply conduit 108 from heat transferred through the interfaces.
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公开(公告)号:US20170350274A1
公开(公告)日:2017-12-07
申请号:US15170221
申请日:2016-06-01
Applicant: United Technologies Corporation
Inventor: Ryan K. Snyder , Thomas Bruce Avis , Francis Parnin
CPC classification number: F01D25/18 , F01D25/183 , F01D25/24 , F01M11/02 , F02C3/04 , F05D2220/32 , F05D2240/55 , F05D2240/60 , F05D2260/98
Abstract: A gas turbine engine includes a bearing compartment with a bottom disposed opposite a top. An outlet is formed in the bottom of the bearing compartment. A seal is positioned between the bottom of the bearing compartment and the top of the bearing compartment. A scavenge line is connected to the outlet. The scavenge line forms a fluid trap that extends in a first direction from the outlet and the bottom of the bearing compartment and then extends in a second direction to a position disposed vertically between the bottom of the bearing compartment and the seal.
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公开(公告)号:US20160258360A1
公开(公告)日:2016-09-08
申请号:US15031558
申请日:2014-05-23
Applicant: United Technologies Corporation
Inventor: Robert F. Sheil , Thomas Bruce Avis , Peter Tu
CPC classification number: F02C7/222 , F02C3/04 , F02C7/06 , F02C7/22 , F05D2220/32 , F05D2240/35 , F05D2240/54 , F05D2240/90 , F16C35/06 , F23R3/10 , F23R3/28
Abstract: A fuel supply manifold of a gas turbine engine, a method for assembling a fuel supply manifold for a gas turbine engine, and a gas turbine engine are disclosed. The fuel supply manifold for the gas turbine engine man include a plurality of fuel supply tubes, a fitting connecting at least two members of the plurality of fuel supply tubes, a bracket attached to the fitting, a bearing housing having a ball bearing, a bushing attached to a diffuser case of the gas turbine engine, wherein the bushing is surrounded by the ball bearing, and a removable fastener to connect the bearing housing to the bracket.
Abstract translation: 公开了一种燃气涡轮发动机的燃料供给歧管,用于组装燃气涡轮发动机的燃料供给歧管的方法和燃气涡轮发动机。 用于燃气涡轮发动机人的燃料供应歧管包括多个燃料供应管,连接多个燃料供应管中的至少两个构件的配件,附接到配件的支架,具有球轴承的轴承壳体,衬套 附接到燃气涡轮发动机的扩散器壳体,其中衬套被球轴承包围,以及可拆卸的紧固件以将轴承壳体连接到支架。
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公开(公告)号:US20160010773A1
公开(公告)日:2016-01-14
申请号:US14759879
申请日:2014-01-20
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Thomas Bruce Avis , Michael Dreher
CPC classification number: F16L23/02 , F01D25/00 , F01D25/24 , F01D25/28 , F05D2260/30
Abstract: A component mount is disclosed which may comprise a tube fitting having first and second ends, a bracket extending from the tube fitting, and a mount extending from the tube fitting. The component mount may be used to mount a line replaceable unit to a casing of a gas turbine engine.
Abstract translation: 公开了一种组件安装件,其可以包括具有第一和第二端的管接头,从管接头延伸的托架和从管接头延伸的安装件。 组件安装件可用于将线路可更换单元安装到燃气涡轮发动机的壳体。
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