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公开(公告)号:US09909448B2
公开(公告)日:2018-03-06
申请号:US14686799
申请日:2015-04-15
Applicant: General Electric Company
Inventor: William Dwight Gerstler , James Michael Kostka , Jeffrey Douglas Rambo , John William Moores
CPC classification number: F01D25/12 , F01D5/181 , F01D9/04 , F01D9/041 , F01D25/18 , F02C7/14 , F05D2220/32 , F05D2240/12 , F05D2260/208 , F05D2260/232 , F28D15/046
Abstract: A heat transfer apparatus for a gas turbine engine includes: a component having a wall structure defining a flow bounding surface; a chamber formed in the component, the chamber including a wicking structure, a vapor channel, and a working fluid.
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公开(公告)号:US20200254520A1
公开(公告)日:2020-08-13
申请号:US16273513
申请日:2019-02-12
Applicant: General Electric Company
Inventor: Johnnattan Tennessee Ugarte , John Eric Bloomberg , Xuefeng Zhang , John William Moores , Justin Michael Stekli , Sameer Surendra Parasnis , Jun Zheng Hu
Abstract: A method for additively manufacturing a component includes receiving, via an additive manufacturing system, a geometry of the component and melting and fusing, via an energy beam of the additive manufacturing system, material layer by layer atop a build platform according to the geometry so as to build up a plurality of layers that form the component. The method also includes determining a surface area change from one of the plurality of layers to the next based on the geometry. Further, the method includes temporarily discontinuing melting and fusing of the material by the energy beam between building of one or more of the plurality of layers so as to provide a delay after building one or more of the plurality of layers when the surface area change is above a predetermined threshold. As such, the delay allows for one or more previously built layers to at least partially cool so as to eliminate and/or reduce build failures from occurring in the final component.
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公开(公告)号:US20160281532A1
公开(公告)日:2016-09-29
申请号:US14666389
申请日:2015-03-24
Applicant: General Electric Company
Inventor: Jeffrey Douglas Rambo , William Dwight Gerstler , James Michael Kostka , John William Moores
IPC: F01D25/12
CPC classification number: F01D25/12 , F02C7/14 , F02C7/18 , F05D2250/71 , F05D2260/213 , F28D1/0477 , F28D2021/0021 , F28D2021/0026 , F28F1/26
Abstract: A heat exchanger apparatus for a gas turbine engine includes: a plurality of heat exchanger pipes, each pipe having first and second ends; wherein the heat exchanger pipes are disposed in a repeating pattern such that each heat exchanger pipe is joined to at least one other heat exchanger pipe.
Abstract translation: 一种用于燃气涡轮发动机的热交换器装置包括:多个热交换器管,每个管具有第一和第二端; 其中所述热交换器管以重复图案设置,使得每个热交换器管连接到至少一个其它热交换管。
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公开(公告)号:US11173668B2
公开(公告)日:2021-11-16
申请号:US16734485
申请日:2020-01-06
Applicant: General Electric Company
Inventor: Christian Xavier Stevenson , Patrick Michael Kenney , John William Moores , David Corsmeier
IPC: B29C64/40 , B33Y10/00 , B29C64/10 , B29C64/153 , B29C64/135 , B23K26/354
Abstract: The present disclosure generally relates to methods for additive manufacturing (AM) that utilize rail support structures in the process of building objects, as well as novel rail support structures to be used within these AM processes. The rail support structures include a plurality of substantially parallel vertical walls, each wall extending substantially parallel to a direction from the first side to the second side. Adjacent walls of the plurality of substantially parallel vertical walls are separated by a portion of unfused powder. An object is formed above the plurality of substantially parallel vertical walls.
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公开(公告)号:US10556383B2
公开(公告)日:2020-02-11
申请号:US15153445
申请日:2016-05-12
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Christian Xavier Stevenson , Patrick Michael Kenney , John William Moores , David Corsmeier
IPC: B29C64/40 , B33Y10/00 , B29C64/10 , B29C64/153 , B29C64/135 , B23K26/354
Abstract: The present disclosure generally relates to methods for additive manufacturing (AM) that utilize rail support structures in the process of building objects, as well as novel rail support structures to be used within these AM processes. The rail support structures include a plurality of substantially parallel vertical walls, each wall extending substantially parallel to a direction from the first side to the second side. Adjacent walls of the plurality of substantially parallel vertical walls are separated by a portion of unfused powder. An object is formed above the plurality of substantially parallel vertical walls.
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