Invention Grant
- Patent Title: Tangential rotor blade slot spacer for a gas turbine engine
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Application No.: US16793307Application Date: 2020-02-18
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Publication No.: US11242761B2Publication Date: 2022-02-08
- Inventor: Weston Behling , Michael C. Weber , William B. McLean , William S. Pratt , Joon Ha
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Bachman & LaPointe, P.C.
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/32
Abstract:
A rotor disk assembly for a gas turbine engine includes a rotor disk that defines an axis, the rotor disk comprising a slot within a rim of the disk and a spacer within the slot, the spacer having a clearance feature sized to permit rotation of a rotor blade from an insertion position to an installed position.
Public/Granted literature
- US20210254480A1 Tangential Rotor Blade Slot Spacer for a Gas Turbine Engine Public/Granted day:2021-08-19
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