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公开(公告)号：US20250027721A1
公开(公告)日：2025-01-23
申请号：US18349415
申请日：2023-07-10
Applicant: General Electric Company
Inventor： Michael Simonetti , Michael Vadnais , Nishita Deshmukh , Ramana Reddy Kollam , James Fitzgerald Bonar , Mehmet Kilic , Prerna Mandal
IPC: F28D7/16
Abstract: A gas turbine engine is provided. The gas turbine engine includes: a thermal management system having a thermal fluid member having a flow of thermal fluid therethrough during operation of the gas turbine engine and a heat exchanger assembly, the heat exchanger assembly including: a core section comprising a plurality of heat exchange members; and a heat exchange manifold including a first direction pressure vessel in fluid communication with the thermal fluid member and a second direction pressure vessel extending from the first direction pressure vessel, the first and second direction pressure vessels each extending in a reference plane, the second direction pressure vessel in fluid communication with the first direction pressure vessel and with at least one of the plurality of heat exchange members.
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公开(公告)号：US20250035382A1
公开(公告)日：2025-01-30
申请号：US18349395
申请日：2023-07-10
Applicant: General Electric Company
Inventor： Michael Simonetti , Michael Vadnais , Nishita Deshmukh , Ramana Reddy Kollam , James Fitzgerald Bonar , Mehmet Kilic , Prerna Mandal
Abstract: A gas turbine engine is provided. The gas turbine engine includes: a thermal management system having a thermal fluid member having a flow of thermal fluid therethrough during operation of the gas turbine engine and a heat exchanger assembly, the heat exchanger assembly including: a core section comprising a plurality of heat exchange members; and a heat exchange manifold including a first direction pressure vessel in fluid communication with the thermal fluid member and a second direction pressure vessel extending from the first direction pressure vessel, the first and second direction pressure vessels each extending in a reference plane, the second direction pressure vessel in fluid communication with the first direction pressure vessel and with at least one of the plurality of heat exchange members.
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公开(公告)号：US12259194B2
公开(公告)日：2025-03-25
申请号：US18349415
申请日：2023-07-10
Applicant: General Electric Company
Inventor： Michael Simonetti , Michael Vadnais , Nishita Deshmukh , Ramana Reddy Kollam , James Fitzgerald Bonar , Mehmet Kilic , Prerna Mandal
Abstract: A gas turbine engine is provided. The gas turbine engine includes: a thermal management system having a thermal fluid member having a flow of thermal fluid therethrough during operation of the gas turbine engine and a heat exchanger assembly, the heat exchanger assembly including: a core section comprising a plurality of heat exchange members; and a heat exchange manifold including a first direction pressure vessel in fluid communication with the thermal fluid member and a second direction pressure vessel extending from the first direction pressure vessel, the first and second direction pressure vessels each extending in a reference plane, the second direction pressure vessel in fluid communication with the first direction pressure vessel and with at least one of the plurality of heat exchange members.
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