Invention Grant
- Patent Title: Balance ring for gas turbine engine
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Application No.: US13622652Application Date: 2012-09-19
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Publication No.: US09957799B2Publication Date: 2018-05-01
- Inventor: Jason Arnold
- 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: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D5/02
- IPC: F01D5/02 ; F16F15/32 ; F16F15/34

Abstract:
A ring has a ring body with a central portion surrounding an axis and extending to first and second opposing ends separated by a split. The central portion has a first axial thickness. At least one retaining feature is formed on the ring body, the at least one retaining feature having a second axial thickness greater than the first axial thickness. An assembly and a gas turbine engine are also disclosed.
Public/Granted literature
- US20140079537A1 Balance Ring for Gas Turbine Engine Public/Granted day:2014-03-20
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