Combustor including a flow guide introduction portion connected to a flow guide main body portion, and a gas turbine

Patent metadata

Field	Value
Publication number	US-10584879-B2
Application number	US-201515510313-A
Country	US
Kind code	B2
Filing date	Sep 18, 2015
Priority date	Sep 25, 2014
Publication date	Mar 10, 2020
Grant date	Mar 10, 2020

Abstract

A combustor including a combustor main body having a transition piece that defines a flow channel therein, and a combustor basket inserted in the transition piece from an upstream side of the flow channel that defines a gap through which a film air is sent with an inner peripheral surface of the transition piece; a connecting pipe disposed upstream of an outlet of the gap that connects to the combustor main body from an outer peripheral side and communicates with the flow channel via a connection hole; and a flow guide disposed at an identical position to the outlet of the gap on a downstream side of a connecting portion of the connecting pipe and the combustor main body that guides a compressed air introduced from outside the connecting pipe so that a flow rate distribution is made uniform in a circumferential direction of the combustor main body.

First claim

The invention claimed is:

1. A combustor comprising:
a combustor main body comprising
a transition piece that defines a flow channel therein, and
a combustor basket inserted in the transition piece from an upstream side of the flow channel that sends a combustion gas through the flow channel and defines a gap through which a film air is sent with an inner peripheral surface of the transition piece;
a connecting pipe disposed upstream of an outlet of the gap that connects to the combustor main body from an outer peripheral side, the connecting pipe being provided with a communication hole formed inside the connecting pipe, wherein the communication hole communicates with the flow channel; and
a flow guide disposed in the flow channel on a downstream side of a connecting portion of the connecting pipe and the combustor main body that guides a compressed air introduced from outside the connecting pipe so that a flow rate distribution is made uniform in a circumferential direction of the combustor main body,
wherein the connecting portion includes an intake hole that connects an inside and an outside of the connecting portion,
wherein the flow guide includes:
an introduction portion disposed proximal to the connecting pipe that extends from the intake hole toward the flow channel; and
a flow guide main body portion connected to the introduction portion that extends toward a downstream side of the flow channel, and

wherein the flow guide main body portion includes an outer edge dimensioned to be concentric with an arcuate cross section of the introduction portion and a pair of free side edges that join together opposite ends of the outer edge and the introduction portion.

2. The combustor according to claim 1 , wherein the flow guide main body portion gradually increases in dimension in the circumferential direction toward the downstream side of the flow channel.

3. A gas turbine comprising:
an air compressor;
the combustor according to claim 1 ; and
a turbine driven by the combustion gas generated by the combustor.

4. A gas turbine comprising:
an air compressor;
the combustor according to claim 2 ; and
a turbine driven by the combustion gas generated by the combustor.

Assignees

• Mitsubishi Hitachi Power Sys

Inventors

• Tsunoda Naoki
• Takiguchi Satoshi
• Akamatsu Shinji
• Nishida Koichi
• Tanaka Katsunori

Classifications

• F01D25/12

  Cooling · CPC title

• F05D2260/202

  by film cooling · CPC title

• F02C3/04

  having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title

• F23R3/16 Primary

  with devices inside the flame tube or the combustion chamber to influence the air or gas flow · CPC title

• F23R3/42

  characterised by the arrangement or form of the flame tubes or combustion chambers · CPC title