Invention Grant
- Patent Title: Method of assembling gas turbine engine section
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Application No.: US15059805Application Date: 2016-03-03
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Publication No.: US09909457B2Publication Date: 2018-03-06
- Inventor: Nelson DaCunha , Jesse R. Christophel
- 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: F01D25/24
- IPC: F01D25/24 ; F01D9/04 ; F01D17/16 ; F02C9/22 ; F01D5/06 ; B23K31/02 ; F01D17/14

Abstract:
A method for assembling a section of a gas turbine engine is disclosed. The method involves aligning a vane ring with a first rotor hub such that a row of vanes on the vane ring is adjacent a first row of blades of the first rotor hub, and aligning a second rotor hub with the vane ring such that a second row of blades of the second rotor hub is adjacent the row of vanes and the row of vanes is axially between the first row of blades and the second row of blades. The first hub and the second hub are then non-mechanically bonded together.
Public/Granted literature
- US20160215653A1 METHOD OF ASSEMBLING GAS TURBINE ENGINE SECTION Public/Granted day:2016-07-28
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