Invention Grant
- Patent Title: Mini-disk for gas turbine engine
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Application No.: US15190398Application Date: 2016-06-23
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Publication No.: US10400603B2Publication Date: 2019-09-03
- Inventor: Raymond S. Hummel , Julian Partyka
- 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: Cantor Colburn LLP
- Main IPC: F01D5/06
- IPC: F01D5/06 ; F01D11/00 ; F01D5/08 ; F01D5/02 ; F01D25/08 ; F04D29/32

Abstract:
Mini-disks of gas turbine engines are provided having an axially extending portion extending axially with respect to an axis of the engine, the axially extending portion configured to engage with a hub arm of a compressor of the engine, a radially extending portion extends radially with respect to the axis, the radially extending portion configured to engage with an attachment of a turbine disk of the gas turbine engine, an intermediate portion extending between the axially extending portion and the radially extending portion, and at least one mini-disk connector configured to engage with a portion of the turbine disk of the gas turbine engine to prevent radial movement of the mini-disk during operation.
Public/Granted literature
- US20170370226A1 MINI-DISK FOR GAS TURBINE ENGINE Public/Granted day:2017-12-28
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