Invention Grant
- Patent Title: Turbine abradable layer with inclined angle surface ridge or groove pattern
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Application No.: US15118996Application Date: 2015-02-18
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Publication No.: US10221716B2Publication Date: 2019-03-05
- Inventor: Kok-Mun Tham , Ching-Pang Lee
- Applicant: Siemens Aktiengesellschaft
- Applicant Address: DE München
- Assignee: SIEMENS AKTIENGESELLSCHAFT
- Current Assignee: SIEMENS AKTIENGESELLSCHAFT
- Current Assignee Address: DE München
- International Application: PCT/US2015/016302 WO 20150218
- International Announcement: WO2015/130522 WO 20150903
- Main IPC: F01D11/12
- IPC: F01D11/12 ; F01D11/14 ; F01D5/02 ; F01D5/12 ; F01D25/24

Abstract:
Turbine and compressor casing/housing abradable component embodiments for turbine engines, have abradable surfaces with ridges projecting from the abradable surface, separated by grooves. The ridges have one or both sidewalls inclined against the opposing turbine blade tip rotational direction for redirecting and/or dissipating blade tip gap leakage airflow energy. In some embodiments the ridge tip and/or groove base have inclined profiles for redirecting airflow leakage away from the blade tip gap. In some embodiments, the inclined ridge tip profile provides a progressive wear zone that increases abradable surface area as the inclined ridge is abraded by the rotating blade tip.
Public/Granted literature
- US20160362997A1 TURBINE ABRADABLE LAYER WITH INCLINED ANGLE SURFACE RIDGE OR GROOVE PATTERN Public/Granted day:2016-12-15
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