Invention Grant
- Patent Title: Gas turbine rotors
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Application No.: US14813284Application Date: 2015-07-30
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Publication No.: US10006364B2Publication Date: 2018-06-26
- Inventor: Gabriel L. Suciu , Brian D. Merry , James D. Hill
- 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 ; F02C7/12 ; F01D5/08 ; F01D25/24 ; F02C3/04 ; F02C7/20 ; F01D11/00 ; F01D25/12 ; F04D29/32 ; F04D29/16 ; F04D29/54 ; F04D29/58

Abstract:
A rotor for a gas turbine engine includes a cold shell, a hot shell, and a spoke. The spoke is connected to and extends radially outward from the cold shell. The hot shell is connected to the cold shell by the spoke and includes an axially extending outboard segment and an axially extending inboard segment. The outboard segment is connected to the inboard segment and the inboard segment is disposed radially inboard of the outboard segment for sealably engaging a stator blade shroud.
Public/Granted literature
- US20160053688A1 GAS TURBINE ROTORS Public/Granted day:2016-02-25
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