Invention Grant
- Patent Title: Aerofoil blade
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Application No.: US14451690Application Date: 2014-08-05
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Publication No.: US09695698B2Publication Date: 2017-07-04
- Inventor: Mark John Knight
- Applicant: ROLLS-ROYCE PLC
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE plc
- Current Assignee: ROLLS-ROYCE plc
- Current Assignee Address: GB London
- Agency: Oliff PLC
- Priority: GB1314296.3 20130809
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/14 ; F01D11/16

Abstract:
A turbomachine aerofoil blade has an aerofoil body portion and a dovetail root fixing at the base of the aerofoil body portion which slides, in use, into a correspondingly shaped slot of a rotor of the turbomachine. The dovetail root fixing has a neck portion, and support flanks engage with matching angled surfaces of the slot under centrifugal loading of the aerofoil blade to support the aerofoil blade on the rotor. The neck portion is shaped such that a rotational adjustment of the aerofoil blade relative to its angular position when supported under centrifugal loading is needed to provide adequate clearance at the neck portion to allow the dovetail root fixing to slide into the slot. On centrifugal loading the engagement of the support flanks with the matching angled surfaces of the slot forces a reversal of the rotational adjustment and reduces the clearance at the neck portion.
Public/Granted literature
- US20150300181A1 AEROFOIL BLADE Public/Granted day:2015-10-22
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