- 专利标题: FLUTTER INHIBITING INTAKE FOR GAS TURBINE PROPULSION SYSTEM
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申请号: US15452634申请日: 2017-03-07
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公开(公告)号: US20180258857A1公开(公告)日: 2018-09-13
- 发明人: Dilip Prasad , Bruce L. Morin
- 申请人: UNITED TECHNOLOGIES CORPORATION
- 主分类号: F02C7/045
- IPC分类号: F02C7/045 ; F01D25/06
摘要:
Disclosed is a flutter damper including a first plurality of chambers configured for peak acoustical energy absorption at a frequency range that is associated with a first fan flutter mode, the first plurality of chambers in fluid communication with a flow surface, and a second plurality of chambers configured for peak acoustical energy absorption at a frequency range that is associated with a second fan flutter mode, the second plurality of chambers in fluid communication with the flow surface, and wherein the first plurality of chambers and second plurality of chambers are disposed in a grid pattern.
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