CN114777158A - Combustion chamber mixing structure based on blunt body group - Google Patents
Combustion chamber mixing structure based on blunt body group Download PDFInfo
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- CN114777158A CN114777158A CN202210523369.5A CN202210523369A CN114777158A CN 114777158 A CN114777158 A CN 114777158A CN 202210523369 A CN202210523369 A CN 202210523369A CN 114777158 A CN114777158 A CN 114777158A
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- wall
- bluff body
- combustion chamber
- body group
- bluff
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Abstract
本发明的目的在于提供一种基于钝体组的燃烧室掺混结构,包括燃烧室、钝体组,燃烧室包括前壁及其后方的管壁,前壁上安装喷嘴,所述钝体组包括前钝体和后钝体,所述前钝体包括外壁和内壁,内壁位于喷嘴外部,外壁位于内壁外部,外壁与内壁之间形成流道,流道连通管壁内部空间,管壁上设置进气孔,进气孔后方设置后钝体。本发明在传统燃烧室基础上加设数对钝体组,可以代替旋流器,提高油气掺混效果的同时起到稳焰的作用。
The object of the present invention is to provide a combustion chamber mixing structure based on a bluff body group, comprising a combustion chamber and a bluff body group, the combustion chamber includes a front wall and a pipe wall behind it, a nozzle is installed on the front wall, and the bluff body group Including a front bluff body and a rear bluff body, the front bluff body includes an outer wall and an inner wall, the inner wall is located outside the nozzle, the outer wall is located outside the inner wall, a flow channel is formed between the outer wall and the inner wall, the flow channel communicates with the inner space of the pipe wall, and the pipe wall is provided with Air intake hole, rear bluff body is set behind the air intake hole. The invention adds several pairs of bluff body groups on the basis of the traditional combustion chamber, which can replace the swirler, improve the mixing effect of oil and gas, and play the role of stabilizing the flame.
Description
技术领域technical field
本发明涉及的是一种燃气轮机,具体地说是燃气轮机的燃烧室结构。The present invention relates to a gas turbine, in particular to a combustion chamber structure of the gas turbine.
背景技术Background technique
燃气轮机具有功率密度大、机动性强的特点,主要部件包括压气机、燃烧室、涡轮,是一种典型的动力装置。压气机对来流气体做功提高压力,燃料在燃烧室中点燃与来流高压气体掺混推动涡轮做功,涡轮产生的功用于带动压气机旋转,形成布雷顿循环。然而,燃烧室中存在燃料燃烧不充分以及燃烧不稳定的问题,极大地影响了燃气轮机的工作稳定性,为此需要设计一种结构在提高油气掺混效果的同时起到稳焰的作用。Gas turbine has the characteristics of high power density and strong maneuverability. Its main components include compressor, combustion chamber, and turbine. It is a typical power plant. The compressor does work on the incoming gas to increase the pressure, the fuel is ignited in the combustion chamber and mixed with the incoming high-pressure gas to push the turbine to do work, and the work generated by the turbine is used to drive the compressor to rotate, forming a Brayton cycle. However, there are problems of insufficient fuel combustion and unstable combustion in the combustion chamber, which greatly affects the working stability of the gas turbine. Therefore, it is necessary to design a structure that can improve the mixing effect of oil and gas and stabilize the flame.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供能提高油气掺混效果和稳焰效果的一种基于钝体组的燃烧室掺混结构。The purpose of the present invention is to provide a combustion chamber mixing structure based on a bluff body group which can improve the oil-gas mixing effect and the flame stabilization effect.
本发明的目的是这样实现的:The object of the present invention is achieved in this way:
本发明一种基于钝体组的燃烧室掺混结构,其特征是:包括燃烧室、钝体组,燃烧室包括前壁及其后方的管壁,前壁上安装喷嘴,所述钝体组包括前钝体和后钝体,所述前钝体包括外壁和内壁,内壁位于喷嘴外部,外壁位于内壁外部,外壁与内壁之间形成流道,流道连通管壁内部空间,管壁上设置进气孔,进气孔后方设置后钝体。A combustion chamber mixing structure based on a bluff body group of the present invention is characterized in that it includes a combustion chamber and a bluff body group, the combustion chamber includes a front wall and a pipe wall behind it, a nozzle is installed on the front wall, and the bluff body group Including a front bluff body and a rear bluff body, the front bluff body includes an outer wall and an inner wall, the inner wall is located outside the nozzle, the outer wall is located outside the inner wall, a flow channel is formed between the outer wall and the inner wall, the flow channel communicates with the inner space of the pipe wall, and the pipe wall is provided with Air intake hole, rear bluff body is set behind the air intake hole.
本发明还可以包括:The present invention can also include:
1、所述后钝体采用扇形截面通过自身连杆固定于管壁上,阻挡进入管壁内部的气流。1. The rear bluff body adopts a fan-shaped section and is fixed on the pipe wall through its own connecting rod, so as to block the airflow entering the inside of the pipe wall.
2、所述前钝体的外壁与内壁均采用梯形截面,外壁与内壁均周向布置6个,梯形截面使得气流产生脱体涡;所述后钝体周向均匀布置6个;前钝体与后钝体空间交叉形式布置。2. The outer wall and inner wall of the front bluff body adopt trapezoidal sections, and the outer wall and the inner wall are arranged with 6 circumferentially, and the trapezoidal section causes the airflow to generate a detachment vortex; the rear bluff body is evenly arranged circumferentially 6; It is arranged in the form of crossing with the rear bluff space.
本发明的优势在于:本发明在传统燃烧室基础上加设数对钝体组,可以代替旋流器,提高油气掺混效果的同时起到稳焰的作用。The advantage of the present invention is: the present invention adds several pairs of bluff body groups on the basis of the traditional combustion chamber, which can replace the swirler, improve the mixing effect of oil and gas, and play the role of stabilizing the flame.
附图说明Description of drawings
图1为本发明的结构示意图;Fig. 1 is the structural representation of the present invention;
图2为前钝体和后钝体示意图;Figure 2 is a schematic diagram of the front bluff body and the rear bluff body;
图3为前钝体和后钝体交叉布置示意图;Figure 3 is a schematic diagram of the cross arrangement of the front bluff body and the rear bluff body;
图4为前钝体、后钝体和燃烧室管壁进气孔沿轴向布置示意图;Figure 4 is a schematic diagram of the axial arrangement of the front bluff body, the rear bluff body and the air inlet holes of the combustion chamber wall;
图5为前钝体组成的示意图;Figure 5 is a schematic diagram of the composition of the front bluff body;
图6为后钝体的示意图;Fig. 6 is the schematic diagram of rear bluff body;
图7为增加钝体组2后燃烧室1内流场的流线图。FIG. 7 is a streamline diagram of the flow field in the combustion chamber 1 after the bluff body group 2 is added.
具体实施方式Detailed ways
下面结合附图举例对本发明做更详细地描述:The present invention will be described in more detail below in conjunction with the accompanying drawings:
结合图1-7,本发明包括:燃烧室1和钝体组2。其中,燃烧室包括前壁1.1、管壁1.2、喷嘴1.3;钝体组2包括前钝体2.1与后钝体2.2。1-7 , the present invention includes: a combustion chamber 1 and a bluff body group 2 . The combustion chamber includes a front wall 1.1, a pipe wall 1.2, and a nozzle 1.3; the bluff body group 2 includes a front bluff body 2.1 and a rear bluff body 2.2.
前钝体2.1由外壁2.1.1和内壁2.1.2组成,外壁2.1.1和内壁2.1.2间构成流道。The front bluff body 2.1 is composed of an outer wall 2.1.1 and an inner wall 2.1.2, and a flow channel is formed between the outer wall 2.1.1 and the inner wall 2.1.2.
前钝体2.1采用梯形横截面,固定于燃烧室1的前壁1.1上,周向均匀布置6个;梯形截面在产生前钝体2.1后脱体涡的同时还能保证管壁1.2侧稳定进气。The front bluff body 2.1 adopts a trapezoidal cross-section, which is fixed on the front wall 1.1 of the combustion chamber 1, and 6 are evenly arranged in the circumferential direction; the trapezoidal cross-section can ensure the stable feeding of the pipe wall 1.2 side while generating the front bluff body 2.1 and the rear detachment vortex. gas.
后钝体2.2采用扇形截面通过自身连杆固定于燃烧室1的管壁1.2上,周向均匀布置6个,仅对主要气流起阻挡作用,产生涡流的同时不会造成过大的总压损失。The rear bluff body 2.2 is fixed on the tube wall 1.2 of the combustion chamber 1 through its own connecting rod with a fan-shaped section, and 6 are evenly arranged in the circumferential direction, which only blocks the main air flow and generates eddy current without causing excessive total pressure loss. .
燃烧室1管壁1.2的进气孔位于前钝体2.1和后钝体2.2之间,进气孔在周向两前钝体2.1中间,布置形式如图1。The air inlet hole of the tube wall 1.2 of the combustion chamber 1 is located between the front bluff body 2.1 and the rear bluff body 2.2, and the air inlet hole is in the middle of the two front bluff bodies 2.1 in the circumferential direction. The layout is shown in Figure 1.
前钝体2.1和后钝体2.2呈交叉形式布置,布置形式如图3。The front bluff body 2.1 and the rear bluff body 2.2 are arranged in a cross form, as shown in Figure 3.
如图7,后钝体2.2前存在由主要气流产生的大漩涡,前钝体2.1与大漩涡之间存在脱体涡,两漩涡区组成较为紧密的大范围漩涡区。As shown in Figure 7, there is a large vortex generated by the main air flow in front of the rear bluff body 2.2, and there is a detachment vortex between the front bluff body 2.1 and the large vortex, and the two vortex areas form a relatively close large-scale vortex area.
当燃气轮机正常工作时,由压气机来的高压气流分为两股,一股主要气流由燃烧室1管壁1.2的进气孔进入燃烧室1内,另一股次要气流由前钝体2.1的流道进入。主要气流由管壁1.2进气孔进入后被后钝体2.2阻挡产生漩涡,次要气流由前钝体2.1狭窄流道进入后形成被高速后受涡流团阻挡形成较为紧凑的脱体涡。从整体上看,主要气流和次要气流在钝体组2的作用下形成大面积紧密的漩涡区,有利于油气掺混效果并稳定火焰。When the gas turbine is working normally, the high-pressure air flow from the compressor is divided into two parts, one main air flow enters the combustion chamber 1 through the air inlet hole of the tube wall 1.2 of the combustion chamber 1, and the other secondary air flow enters the combustion chamber 1 from the front bluff body 2.1 into the flow channel. The main air flow enters through the air inlet hole of the pipe wall 1.2 and is blocked by the rear bluff body 2.2 to generate a vortex. The secondary air flow enters the narrow flow channel of the front bluff body 2.1 to form a relatively compact detached vortex that is blocked by the vortex mass at a high speed. On the whole, under the action of the bluff body group 2, the main air flow and the secondary air flow form a large and compact vortex area, which is conducive to the mixing effect of oil and gas and stabilizes the flame.
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Cited By (1)
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CN115949528A (en) * | 2023-01-30 | 2023-04-11 | 厦门大学 | Rotary grid type rear duct ejector for variable cycle engine |
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Application publication date: 20220722 |