Invention Grant
- Patent Title: Gas turbine blade and rotor wear-protection system
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Application No.: US17123355Application Date: 2020-12-16
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Publication No.: US11591919B2Publication Date: 2023-02-28
- Inventor: Gino Palumbo , Klaus Tomantschger , Jonathan McCrea , David Lionel Limoges
- Applicant: INTEGRAN TECHNOLOGIES INC.
- Applicant Address: CA Mississauga
- Assignee: INTEGRAN TECHNOLOGIES INC.
- Current Assignee: INTEGRAN TECHNOLOGIES INC.
- Current Assignee Address: CA Mississauga
- Agency: Rankin, Hill & Clark LLP
- Main IPC: F01D5/30
- IPC: F01D5/30

Abstract:
Sacrificial inserts for use in gas turbine engines to reduce friction and wear damage between compressor fan blades and the fan rotors are disclosed. The consumable metallic shims have low friction and reduce fretting and galling on fan blade roots and fan rotor dovetail slots thereby increasing their operating lives, as well as reduce engine noise and improve engine efficiency. The electroformed, compliant, multi-purpose shims may have variable thickness and, when positioned between the blade dovetail root and the rotor disk dovetail slot, prevent movement and slippage between air foil blades and the rotor.
Public/Granted literature
- US20220186621A1 GAS TURBINE BLADE AND ROTOR WEAR-PROTECTION SYSTEM Public/Granted day:2022-06-16
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