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公开(公告)号:US12130099B2
公开(公告)日:2024-10-29
申请号:US17959399
申请日:2022-10-04
Applicant: Hamilton Sundstrand Corporation
Inventor: Kathryn L. Kirsch , Robert H. Dold , Paul Attridge , Alexandru Cadar , Joseph Turney , Ram Ranjan
IPC: F28F9/02
CPC classification number: F28F9/0275 , F28F2009/0287
Abstract: A header for a high-pressure heat exchanger includes a first high-pressure transition section with inlets for multiple first high-pressure flow channels that are spaced from one another in a radial direction and collectively arranged in a substantially circular shape. The inlets for the multiple first high-pressure flow channels on a radially outer edge of the first high-pressure transition section are spaced further apart in a circumferential direction from adjacent inlets of the multiple first high-pressure flow channels than radially inward inlets are spaced from adjacent radially inward inlets of the multiple first high-pressure flow channels. The header also includes multiple first high-pressure flow channels extending from the first high-pressure transition section to a second-high pressure transition section that is configured to divide each of the multiple first high-pressure flow channels into at least two first high-pressure sub-flow channels.
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公开(公告)号:US20230116443A1
公开(公告)日:2023-04-13
申请号:US17959399
申请日:2022-10-04
Applicant: Hamilton Sundstrand Corporation
Inventor: Kathryn L. Kirsch , Robert H. Dold , Paul Attridge , Alexandru Cadar , Joseph Turney , Ram Ranjan
IPC: F28F9/02
Abstract: A header for a high-pressure heat exchanger includes a first high-pressure transition section with inlets for multiple first high-pressure flow channels that are spaced from one another in a radial direction and collectively arranged in a substantially circular shape. The inlets for the multiple first high-pressure flow channels on a radially outer edge of the first high-pressure transition section are spaced further apart in a circumferential direction from adjacent inlets of the multiple first high-pressure flow channels than radially inward inlets are spaced from adjacent radially inward inlets of the multiple first high-pressure flow channels. The header also includes multiple first high-pressure flow channels extending from the first high-pressure transition section to a second-high pressure transition section that is configured to divide each of the multiple first high-pressure flow channels into at least two first high-pressure sub-flow channels.
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公开(公告)号:US12209823B2
公开(公告)日:2025-01-28
申请号:US17581571
申请日:2022-01-21
Applicant: Hamilton Sundstrand Corporation
Inventor: Kathryn L. Kirsch , Robert H. Dold , Paul Attridge , Alexandru Cadar
Abstract: In accordance with at least one aspect of this disclosure, a transition structure for a heat exchanger can include a body defining a dome cavity. The dome cavity can be configured to transition flow between at least one first channel and a plurality of second channels having a different number than the at least one first channel.
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4.
公开(公告)号:US11097487B2
公开(公告)日:2021-08-24
申请号:US16230354
申请日:2018-12-21
Applicant: Hamilton Sundstrand Corporation
Inventor: Tahany Ibrahim El-Wardany , Joseph V. Mantese , Abhijit Chakraborty , Paul Attridge
IPC: B29C64/153 , G06F30/00 , B33Y30/00 , B29C64/393 , B29C64/371 , B22F10/20 , B22F10/30 , B33Y10/00 , B33Y40/00 , B33Y50/02 , B33Y70/00
Abstract: An additive manufacturing system includes an additive manufacturing (AM) device, a first sensor device, and a compute device. The AM device is configured to form a bulk component in a layer-by-layer manner, by at least iteratively depositing a first layer of raw material onto a working surface in a deposition chamber, consolidating the initial layer into an initial additive portion of the bulk component, then forming subsequent additive portions of the bulk component by depositing and consolidating a subsequent plurality of layers of the raw material onto the first additive portion. The first sensor device is configured to measure an actual composition of at least one first byproduct portion formed upon consolidation of one of the first or subsequent layers of raw material in the deposition chamber. The compute device includes a processor and a memory, and is communicatively coupled to the additive manufacturing device and first sensor device. The additive manufacturing device and compute device provide an in situ sensor analysis of the component while in a formation state during a build process by comparing an actual composition of the at least one first byproduct portion to an expected composition range stored in the memory.
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公开(公告)号:US11493286B1
公开(公告)日:2022-11-08
申请号:US17499352
申请日:2021-10-12
Applicant: Hamilton Sundstrand Corporation
Inventor: Kathryn L. Kirsch , Robert H. Dold , Paul Attridge , Alexandru Cadar , Joseph Turney , Ram Ranjan
IPC: F28F9/02
Abstract: A header for a high-pressure heat exchanger includes a first high-pressure transition section with inlets for multiple first high-pressure flow channels that are spaced from one another in a radial direction and collectively arranged in a substantially circular shape. The inlets for the multiple first high-pressure flow channels on a radially outer edge of the first high-pressure transition section are spaced further apart in a circumferential direction from adjacent inlets of the multiple first high-pressure flow channels than radially inward inlets are spaced from adjacent radially inward inlets of the multiple first high-pressure flow channels. The header also includes multiple first high-pressure flow channels extending from the first high-pressure transition section to a second-high pressure transition section that is configured to divide each of the multiple first high-pressure flow channels into at least two first high-pressure sub-flow channels. Each flow channel of the multiple first high-pressure flow channels and each sub-flow channel of the first high-pressure sub-flow channels have a round cross-sectional shape.
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