Invention Grant
- Patent Title: Gas turbine combustor having a plurality of angled vanes circumferentially spaced within the combustor
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Application No.: US16295542Application Date: 2019-03-07
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Publication No.: US11434831B2Publication Date: 2022-09-06
- Inventor: Peter Daniel Silkowski
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Venable LLP
- Agent Elizabeth C. G. Gitlin; Michele V. Frank
- Main IPC: F02C9/22
- IPC: F02C9/22 ; F02C3/14 ; F23R3/02 ; F02C6/00 ; F02C3/04
Abstract:
A gas turbine engine includes: a compressor section including a compressor mean radius; a combustor section fluidly coupled downstream of the compressor section and include a combustor mean radius; and a turbine section fluidly coupled downstream of the combustor section and a turbine mid-span radius. The combustor mean radius is greater than each of the compressor mean radius and the turbine mid-span radius.
Public/Granted literature
- US20200025110A1 GAS TURBINE ENGINE Public/Granted day:2020-01-23
Information query
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