- 专利标题: Transition section for accommodating mismatch between other sections of a cooling aperture in a turbine engine component
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申请号: US17401927申请日: 2021-08-13
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公开(公告)号: US11732590B2公开(公告)日: 2023-08-22
- 发明人: Brian Craig , James M. Koonankeil , Brian T. Hazel , Paul E. Denney , Dominic J. Mongillo
- 申请人: Raytheon Technologies Corporation
- 申请人地址: US CT Farmington
- 专利权人: Raytheon Technologies Corporation
- 当前专利权人: Raytheon Technologies Corporation
- 当前专利权人地址: US CT Farmington
- 代理机构: Getz Balich LLC
- 主分类号: F01D5/18
- IPC分类号: F01D5/18 ; F01D25/12
摘要:
An apparatus is provided for a turbine engine. This turbine engine apparatus includes a turbine engine component that includes a sidewall and a cooling aperture. The cooling aperture includes an inlet, an outlet, a meter section, a diffuser section and a transition section between and fluidly coupled with the meter section and the diffuser section. The cooling aperture extends through the sidewall from the inlet to the outlet. The meter section is at the inlet. The diffuser section is at the outlet. The transition section is configured to accommodate lateral misalignment between the meter section and the diffuser section.
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