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公开(公告)号:US11326519B2
公开(公告)日:2022-05-10
申请号:US16800375
申请日:2020-02-25
Applicant: General Electric Company
Inventor: Matti Veikko Kalevi Makela , Emilio Eramo , Christopher Lloyd McKenzie , Apostolos Pavlos Karafillis
Abstract: A frame for a heat engine, the frame including an inner wall extended from an inlet end to an outlet end, the inner wall forming at least in part a core flowpath, the inner wall comprising a plenum formed between an outer portion of the inner wall and an inner portion of the inner wall, wherein a cavity is formed inward of the inner portion of the inner wall, and wherein the inner wall includes a first plenum opening providing fluid communication between the cavity and the plenum, and wherein the inner wall comprises a second plenum opening providing fluid communication between the plenum and the core flowpath.
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公开(公告)号:US11255264B2
公开(公告)日:2022-02-22
申请号:US16800326
申请日:2020-02-25
Applicant: General Electric Company
Inventor: Matti Veikko Kalevi Makela , Emilio Eramo , Christopher Lloyd McKenzie
Abstract: A thermal management system for a heat engine, the system including an forming at least in part a core flowpath and a cavity, wherein the core flowpath and the cavity are separated by a double wall structure formed by at least a portion of inner wall, and wherein the double wall structure includes a plenum. A first opening provides fluid communication between the cavity and the plenum, and a second opening provides fluid communication between the plenum and the core flowpath. The inner wall is configured to receive a first flow of fluid. An outer wall forms a passage extended at least partially around the core flowpath. The outer wall is configured to receive a second flow of fluid fluidly separated from the core flowpath.
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公开(公告)号:US11560843B2
公开(公告)日:2023-01-24
申请号:US16800410
申请日:2020-02-25
Applicant: General Electric Company
Inventor: Matti Veikko Kalevi Makela , Emilio Eramo , Christopher Lloyd McKenzie , Apostolos Pavlos Karafillis , John Alan Manteiga
Abstract: A turbo machine including a plenum is formed within a double wall structure including an opening configured to provide fluid communication of a first flow of fluid between the plenum through the double wall structure, and an outer wall forming a passage configured to receive a second flow of fluid separate from the first flow of fluid, wherein a flowpath structure is formed at least in part within an inner wall, the flowpath structure configured to receive a third flow of fluid therethrough, the third flow of fluid separate from the first flow of fluid, the flowpath structure comprising an exit opening configured to provide fluid communication from the flowpath structure to the flowpath.
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公开(公告)号:US20210262386A1
公开(公告)日:2021-08-26
申请号:US16800375
申请日:2020-02-25
Applicant: General Electric Company
Inventor: Matti Veikko Kalevi Makela , Emilio Eramo , Christopher Lloyd McKenzie , Apostolos Pavlos Karafillis
Abstract: A frame for a heat engine, the frame including an inner wall extended from an inlet end to an outlet end, the inner wall forming at least in part a core flowpath, the inner wall comprising a plenum formed between an outer portion of the inner wall and an inner portion of the inner wall, wherein a cavity is formed inward of the inner portion of the inner wall, and wherein the inner wall includes a first plenum opening providing fluid communication between the cavity and the plenum, and wherein the inner wall comprises a second plenum opening providing fluid communication between the plenum and the core flowpath.
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公开(公告)号:US20170002664A1
公开(公告)日:2017-01-05
申请号:US14790243
申请日:2015-07-02
Applicant: GENERAL ELECTRIC COMPANY
IPC: F01D5/18
CPC classification number: F01D5/187 , F01D5/188 , F01D5/20 , F05D2220/323 , F05D2240/307 , F05D2250/185 , F05D2260/202 , Y02T50/676
Abstract: A turbine blade includes an airfoil having an internal cooling circuit. The cooling circuit includes a body cooling passage with at least one turn, and a tip cooling channel that forms a cooling barrier to thermally isolate the turn from at least a portion of the exterior surface of the airfoil.
Abstract translation: 涡轮叶片包括具有内部冷却回路的翼型件。 冷却回路包括具有至少一匝的主体冷却通道和形成冷却障碍物的顶部冷却通道,以将匝与翼型件的外表面的至少一部分热隔离。
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公开(公告)号:US20210262389A1
公开(公告)日:2021-08-26
申请号:US16800326
申请日:2020-02-25
Applicant: General Electric Company
Inventor: Matti Veikko Kalevi Makela , Emilio Eramo , Christopher Lloyd McKenzie
IPC: F02C7/14
Abstract: A thermal management system for a heat engine, the system including an forming at least in part a core flowpath and a cavity, wherein the core flowpath and the cavity are separated by a double wall structure formed by at least a portion of inner wall, and wherein the double wall structure includes a plenum. A first opening provides fluid communication between the cavity and the plenum, and a second opening provides fluid communication between the plenum and the core flowpath. The inner wall is configured to receive a first flow of fluid. An outer wall forms a passage extended at least partially around the core flowpath. The outer wall is configured to receive a second flow of fluid fluidly separated from the core flowpath.
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公开(公告)号:US20210262385A1
公开(公告)日:2021-08-26
申请号:US16800410
申请日:2020-02-25
Applicant: General Electric Company
Inventor: Matti Veikko Kalevi Makela , Emilio Eramo , Christopher Lloyd McKenzie , Apostolos Pavlos Karafillis , John Alan Manteiga
Abstract: A turbo machine including a plenum is formed within a double wall structure including an opening configured to provide fluid communication of a first flow of fluid between the plenum through the double wall structure, and an outer wall forming a passage configured to receive a second flow of fluid separate from the first flow of fluid, wherein a flowpath structure is formed at least in part within an inner wall, the flowpath structure configured to receive a third flow of fluid therethrough, the third flow of fluid separate from the first flow of fluid, the flowpath structure comprising an exit opening configured to provide fluid communication from the flowpath structure to the flowpath.
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公开(公告)号:US09976424B2
公开(公告)日:2018-05-22
申请号:US14790243
申请日:2015-07-02
Applicant: General Electric Company
IPC: F01D5/18
CPC classification number: F01D5/187 , F01D5/188 , F01D5/20 , F05D2220/323 , F05D2240/307 , F05D2250/185 , F05D2260/202 , Y02T50/676
Abstract: A turbine blade includes an airfoil having an internal cooling circuit. The cooling circuit includes a body cooling passage with at least one turn, and a tip cooling channel that forms a cooling barrier to thermally isolate the turn from at least a portion of the exterior surface of the airfoil.
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