Invention Grant
- Patent Title: Transition duct for a gas turbine engine
-
Application No.: US15491067Application Date: 2017-04-19
-
Publication No.: US10746032B2Publication Date: 2020-08-18
- Inventor: Keith J. Kucinskas
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F01D25/16 ; F01D5/02
Abstract:
A compressor section for a gas turbine engine includes an upstream portion that includes at least one upstream rotor stage. A downstream portion includes at least one downstream rotor stage configured to rotate with the upstream rotor stage. A transition duct separates the upstream portion from the downstream portion.
Public/Granted literature
- US20180306040A1 TRANSITION DUCT FOR A GAS TURBINE ENGINE Public/Granted day:2018-10-25
Information query
