Invention Grant
- Patent Title: Hollow turbine blade
- Patent Title (中): 中空涡轮叶片
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Application No.: US12870115Application Date: 2010-08-27
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Publication No.: US08444390B2Publication Date: 2013-05-21
- Inventor: Simon Read
- Applicant: Simon Read
- Applicant Address: GB London
- Assignee: Rolls-Royce PLC
- Current Assignee: Rolls-Royce PLC
- Current Assignee Address: GB London
- Agency: Oliff & Berridge, PLC
- Priority: GB0917229.7 20091002
- Main IPC: F01D5/18
- IPC: F01D5/18

Abstract:
A blade for a turbine engine made by the diffusion-bonding/superplastic-forming (DB/SPF) process has a hollow skin made of front and back panels 1, 3 and internal reinforcement in the form of webs 5 extending between the two faces or panels at an angle to the plane of the blade. The cavities are filled with viscoelastic damping filler 7. In order to allow the blade to deform more easily so that the filler can take up the strain, the webs are pre-buckled so as to compress at least some of the webs. When the blade is deformed, the webs straighten or buckle further, applying a deformation to the filler as they do so and thus dissipating energy. The blade is thus well reinforced against impact but still capable of damping vibrations.
Public/Granted literature
- US20110081249A1 HOLLOW TURBINE BLADE Public/Granted day:2011-04-07
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