Gas turbine combustor structure
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Feb 6, 2024
Grant Date -
N/A
app pub date -
Dec 27, 2021
filing date -
Nov 8, 2019
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A combustor structure of an embodiment is disposed to penetrate, from a direction perpendicular to an axial direction of a turbine rotor in a supercritical CO2 gas turbine which uses supercritical CO2 for a working fluid, a casing of the supercritical CO2 gas turbine. The combustor structure includes a plurality of combustors. Each of the combustors includes: a combustor liner in a cylindrical shape, which combusts fuel and an oxidant; a fuel supply part which is provided at an upstream end of the combustor liner and supplies the fuel into the combustor liner; and an oxidant supply part which is provided at the upstream end of the combustor liner and supplies the oxidant into the combustor liner.
First Claim
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International Classification(s)
- 2021 Application Filing Year
- F23R Class
- 254 Applications Filed
- 181 Patents Issued To-Date
- 71.26 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 1 Citation Count
- F23R Class
- 97.22 % this patent is cited more than
- 1 Age
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