- 专利标题: Multi-mode engine system with gas turbine engine and turbo-compressor
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申请号: US17535128申请日: 2021-11-24
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公开(公告)号: US11965458B2公开(公告)日: 2024-04-23
- 发明人: Andre M. Ajami , Ryan W. Hunter , Javier A. Cue
- 申请人: Raytheon Technologies Corporation
- 申请人地址: US CT Farmington
- 专利权人: RTX CORPORATION
- 当前专利权人: RTX CORPORATION
- 当前专利权人地址: US CT Farmington
- 代理机构: GETZ BALICH LLC
- 主分类号: F02C3/13
- IPC分类号: F02C3/13 ; F02C3/04 ; F02C5/02 ; F02C7/32
摘要:
An engine system is provided that includes a compressor section, a combustor section, a turbine section, a flowpath and a flow regulator. The combustor section includes a combustion chamber. The flowpath extends sequentially through the compressor section, the combustor section and the turbine section. The flow regulator is configured to open the flowpath between the compressor section and the combustion chamber during a first mode of operation. The flow regulator is configured to at least substantially close the flowpath between the compressor section and the combustion chamber during a second mode of operation.
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