Invention Grant
US08545183B2 Seal coating between rotor blade and rotor disk slot in gas turbine engine
有权
燃气轮机发动机转子叶片与转子盘槽之间的密封涂层
- Patent Title: Seal coating between rotor blade and rotor disk slot in gas turbine engine
- Patent Title (中): 燃气轮机发动机转子叶片与转子盘槽之间的密封涂层
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Application No.: US12676222Application Date: 2008-08-26
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Publication No.: US08545183B2Publication Date: 2013-10-01
- Inventor: Rene James Webb
- Applicant: Rene James Webb
- Applicant Address: DE Munich
- Assignee: Siemens Aktiengesellschaft
- Current Assignee: Siemens Aktiengesellschaft
- Current Assignee Address: DE Munich
- Priority: GB0717291.9 20070906
- International Application: PCT/EP2008/061116 WO 20080826
- International Announcement: WO2009/030606 WO 20090312
- Main IPC: F01D5/30
- IPC: F01D5/30

Abstract:
A gas turbine rotor blade and rotor disk arrangement is provided. The rotor blade and the rotor disk includes a coating in order to seal the gap which normally exists between the bottom part of the blade root and the bottom part of the disk slot. The coating may be applied to the blade root or to the disk itself on the bottom part of the disk slot. The coating is preferably an abradable nickel-alloy Bentonite coating. The coating may also be applied to only a portion of the areas being sealed, omitting a portion at the start of the slot or at the start of one of the lobes of the blade root, so that a lead-in is formed, whereby the blade can more easily be inserted into the slot.
Public/Granted literature
- US20100178169A1 Seal Coating Between Rotor Blade and Rotor Disk Slot in Gas Turbine Engine Public/Granted day:2010-07-15
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