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公开(公告)号：US11885579B2
公开(公告)日：2024-01-30
申请号：US17242204
申请日：2021-04-27
申请人： The Boeing Company
发明人： Richard W. Aston , Matthew Joseph Herrmann , Michael John Langmack , Nicole M. Hastings , Sumit K. Purohit
摘要： An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.
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公开(公告)号：US20210356015A1
公开(公告)日：2021-11-18
申请号：US16877480
申请日：2020-05-18
申请人： The Boeing Company
摘要： A vibration isolation system is disclosed, including a rigid retaining device having an internal space, a first external side, and a second external side. A rigid anchoring device is retained in the internal space of the rigid retaining device. The anchoring device has a linkage member that extends from the internal space to the first external side of the retaining device and is configured for rigid connection to a first apparatus. The second side of the retaining device is configured for attachment to a second apparatus. A damping material is sandwiched between the retaining device and the anchoring device, and is configured to limit transfer of vibration between the retaining device and the anchoring device.
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公开(公告)号：US20200003497A1
公开(公告)日：2020-01-02
申请号：US16024582
申请日：2018-06-29
申请人： The Boeing Company
发明人： Richard W. Aston , Matthew Joseph Herrmann , Michael John Langmack , Nicole M. Hastings , Sumit K. Purohit
IPC分类号： F28D7/00
摘要： An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.
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公开(公告)号：US11802606B2
公开(公告)日：2023-10-31
申请号：US16877480
申请日：2020-05-18
申请人： The Boeing Company
CPC分类号： F16F15/08 , B64G1/641 , B64G1/645 , F16M13/02 , B64G2001/228
摘要： A vibration isolation system is disclosed, including a rigid retaining device having an internal space, a first external side, and a second external side. A rigid anchoring device is retained in the internal space of the rigid retaining device. The anchoring device has a linkage member that extends from the internal space to the first external side of the retaining device and is configured for rigid connection to a first apparatus. The second side of the retaining device is configured for attachment to a second apparatus. A damping material is sandwiched between the retaining device and the anchoring device, and is configured to limit transfer of vibration between the retaining device and the anchoring device.
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公开(公告)号：US20210247140A1
公开(公告)日：2021-08-12
申请号：US17242204
申请日：2021-04-27
申请人： The Boeing Company
发明人： Richard W. Aston , Matthew Joseph Herrmann , Michael John Langmack , Nicole M. Hastings , Sumit K. Purohit
IPC分类号： F28D7/00
摘要： An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.
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公开(公告)号：US11015872B2
公开(公告)日：2021-05-25
申请号：US16024582
申请日：2018-06-29
申请人： The Boeing Company
发明人： Richard W. Aston , Matthew Joseph Herrmann , Michael John Langmack , Nicole M. Hastings , Sumit K. Purohit
摘要： An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.
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