Invention Grant
- Patent Title: Turbine disk and blade arrangement
- Patent Title (中): 涡轮盘和叶片装置
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Application No.: US13022034Application Date: 2011-02-07
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Publication No.: US08696304B2Publication Date: 2014-04-15
- Inventor: Robert Elliott , Benjamin J. Meyer
- Applicant: Robert Elliott , Benjamin J. Meyer
- Applicant Address: GB London
- Assignee: Rolls-Royce PLC
- Current Assignee: Rolls-Royce PLC
- Current Assignee Address: GB London
- Agency: Oliff PLC
- Priority: GB1002679.7 20100217
- Main IPC: F01D5/30
- IPC: F01D5/30

Abstract:
A turbine disk and blade arrangement having a plurality of turbine blades mounted circumferentially around a disk. Each blade has a fir tree root which provides a series of fore-to-aft-extending projections and grooves. The disk has a plurality of radially extending posts which define fir tree recesses therebetween. Each fir tree recess also provides a series of fore-to-aft-extending projections and grooves allowing each fir tree root to engage with a respective fir tree recess. On each pair of facing sides of the fir tree root and the fir tree recess, one or more projections of the fir tree roots and/or the fir tree recesses are truncated to form fore-to-aft-extending cooling passages. The arrangement has lock plates which cover forward and/or rearward surfaces of the posts and of the fir tree roots and define feed channels therebetween which feed cooling air to the respective cooling passage.
Public/Granted literature
- US20110200448A1 TURBINE DISK AND BLADE ARRANGEMENT Public/Granted day:2011-08-18
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