Invention Grant
- Patent Title: Gas turbine engine rotor disk-seal arrangement
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Application No.: US14775388Application Date: 2014-03-14
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Publication No.: US10024183B2Publication Date: 2018-07-17
- Inventor: Julian Partyka , Jonathan P. Sandoval
- 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: O'Shea Getz P.C.
- International Application: PCT/US2014/027316 WO 20140314
- International Announcement: WO2014/152414 WO 20140925
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D5/30 ; F02C7/28 ; F01D5/02

Abstract:
A disk-seal arrangement for a gas turbine engine rotor includes a blade retention disk having a longitudinally opening slot therein and a seal disk juxtaposed to said blade retention disk and a single anti-rotation tab received within the blade retention disk slot. The seal disk also includes a pair of balance slots disposed immediately adjacent the antirotation tab to offset the weight thereof for preserving rotor balance. A split ring is disposed longitudinally between the blade retention and seal disks for reacting longitudinal loading therebetween. The ends of the split ring seat against side surfaces of the antirotation between the split ring and the blade retention and seal disks.
Public/Granted literature
- US20160017737A1 GAS TURBINE ENGINE ROTOR DISK-SEAL ARRANGEMENT Public/Granted day:2016-01-21
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