Combustor and gas turbine including the combustor

The upstream-side wall portion 54 includes, in the circumferential direction thereof, a first region 31 where air inlets 30 are formed at a lower density, and a second region 32 which is disposed at a position offset from the first region 31 in the circumferential direction, and in which the air inl...

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Hauptverfasser: Taniguchi, Kenta, Abe, Naoki, Matsumura, Yoshikazu, Akamatsu, Shinji, Sato, Kenji, Takiguchi, Satoshi
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creator Taniguchi, Kenta
Abe, Naoki
Matsumura, Yoshikazu
Akamatsu, Shinji
Sato, Kenji
Takiguchi, Satoshi
description The upstream-side wall portion 54 includes, in the circumferential direction thereof, a first region 31 where air inlets 30 are formed at a lower density, and a second region 32 which is disposed at a position offset from the first region 31 in the circumferential direction, and in which the air inlets 30 are formed at a higher density than in the first region 31.
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subjects BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title Combustor and gas turbine including the combustor
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