CN113551261B - Wave V type flame stabilizer - Google Patents
Wave V type flame stabilizer Download PDFInfo
- Publication number
- CN113551261B CN113551261B CN202110812824.9A CN202110812824A CN113551261B CN 113551261 B CN113551261 B CN 113551261B CN 202110812824 A CN202110812824 A CN 202110812824A CN 113551261 B CN113551261 B CN 113551261B
- Authority
- CN
- China
- Prior art keywords
- shaped
- wave
- flame stabilizer
- wavy
- flame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000003381 stabilizer Substances 0.000 title claims abstract description 29
- 238000002485 combustion reaction Methods 0.000 abstract description 8
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 230000003134 recirculating effect Effects 0.000 description 1
Images
Classifications
-
- 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
- F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
-
- 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
- F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Of Fluid Fuel (AREA)
- Spark Plugs (AREA)
Abstract
Description
技术领域technical field
本发明涉及一种波浪形V型火焰稳定器,其可用于航空发动机的加力燃烧室,属于航空技术领域。The invention relates to a wave-shaped V-shaped flame stabilizer, which can be used in an afterburner of an aero-engine and belongs to the technical field of aviation.
背景技术Background technique
喷气式航空发动机的加力燃烧室采用火焰稳定器稳定火焰组织燃烧,火焰稳定器的性能是加力燃烧室性能的决定性影响因素。加力燃烧室大多采用结构简单的V型火焰稳定器。常规V型火焰稳定器虽结构简单易加工制造,但因其产生卡门涡街型回流涡,其回流涡稳定性较差,导致某些情况下火焰稳定性较差,局部燃烧不稳定也会降低燃烧效率,且回流涡交替脱落对流场的扰动也引起了额外的流动损失。The afterburner of the jet aircraft engine adopts the flame stabilizer to stabilize the flame to organize the combustion. The performance of the flame stabilizer is the decisive factor affecting the performance of the afterburner. Most of the afterburners use V-shaped flame stabilizers with a simple structure. Although the conventional V-type flame stabilizer has a simple structure and is easy to manufacture, it produces a Karman vortex street type recirculation vortex, and its recirculation vortex stability is poor, resulting in poor flame stability and local combustion instability in some cases. The combustion efficiency, and the disturbance of the flow field caused by the alternate shedding of recirculating vortices also cause additional flow losses.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供一种波浪形V型火焰稳定器,以提高火焰稳定性,减小流动损失,增大燃烧效率。The purpose of the present invention is to provide a wave-shaped V-shaped flame stabilizer to improve flame stability, reduce flow loss and increase combustion efficiency.
本发明通过如下技术方案实现。The present invention is realized through the following technical solutions.
一种波浪形V型火焰稳定器,具波浪形几何特征,含3~5个波长,其各处横截面形状相同,所述的波浪形V型火焰稳定器,展长由具体发动机确定,主要由前缘、V型面、V型尾缘组成,在横截面上,前缘为对V型面倒圆角得到,圆角半径1.5~5mm,V型面宽20~30mm,V型面的V形夹角25°~40°,V型尾缘宽26~36mm,V型尾缘的前V形夹角55°~70°,V型尾缘的后V形夹角100°~150°,侧面平直段宽1.5~3mm,所述的波浪形几何特征,在波峰位置起始和终止,波浪形为在锯齿形波的波峰和波谷倒圆角得到,圆角半径15~30mm,锯齿形波振幅为6~15mm。A wave-shaped V-shaped flame stabilizer has wave-shaped geometric features, contains 3 to 5 wavelengths, and has the same cross-sectional shape everywhere. It is composed of leading edge, V-shaped surface and V-shaped trailing edge. In cross section, the leading edge is obtained by rounding the V-shaped surface. The included angle of the V-shaped trailing edge is 25°~40°, the width of the V-shaped trailing edge is 26-36mm, the front V-shaped included angle of the V-shaped trailing edge is 55°~70°, and the rear V-shaped included angle of the V-shaped trailing edge is 100°~150°. The width of the straight section on the side is 1.5-3mm. The wave-shaped geometric feature starts and ends at the crest position. The wave-shape is obtained by rounding the crest and trough of the sawtooth wave. The radius of the rounded corner is 15-30mm. The wave amplitude is 6 to 15 mm.
与现有技术相比,本发明的优点和取得的有益效果为:Compared with the prior art, the advantages of the present invention and the beneficial effects obtained are:
第一,火焰稳定性好。常规V型火焰稳定器产生卡门涡街型回流涡,其回流涡稳定性较差。将常规V型火焰稳定器改成波浪形V型火焰稳定器,其后产生K-H型回流涡,且回流涡在展向有分量,波峰、波谷回流区之间存在热质对流传输,因而火焰稳定性好。First, the flame stability is good. The conventional V-type flame stabilizer produces a Karman vortex street-type recirculation vortex, and its recirculation vortex is less stable. The conventional V-type flame stabilizer is changed to a wave-shaped V-type flame stabilizer, and then a K-H type recirculation vortex is generated, and the recirculation vortex has a component in the span. good sex.
第二,流动损失小。常规V型火焰稳定器产生的是卡门涡街型回流涡,波浪形V型火焰稳定器产生的是K-H型回流涡,相比卡门涡街型回流涡,K-H型回流涡引起的流动损失要小的多,因而流动损失小。Second, the flow loss is small. The conventional V-type flame stabilizer produces a Karman vortex street type recirculation vortex, and the wave-shaped V-type flame stabilizer produces a K-H type recirculation vortex. Compared with the Karman vortex street type recirculation vortex, the flow loss caused by the K-H type recirculation vortex is smaller. more, so the flow loss is small.
第三,燃烧效率高。波浪形V型火焰稳定器产生的是K-H型回流涡,其火焰稳定性好,同时回流涡展向分量使波峰、波谷回流区之间产生热质对流传输,使回流区内燃油雾化、蒸发和掺混更充分,从而保证了回流区内稳定高效的燃烧,因而燃烧效率高。Third, the combustion efficiency is high. The wave-shaped V-shaped flame stabilizer produces K-H-type recirculation vortex, which has good flame stability. At the same time, the spanwise component of the recirculation vortex generates heat and mass convective transfer between the peak and trough recirculation areas, so that the fuel in the recirculation area is atomized and evaporated. And blending is more sufficient, thus ensuring stable and efficient combustion in the recirculation zone, so the combustion efficiency is high.
附图说明Description of drawings
图1为本发明中波浪形V型火焰稳定器的等轴视图。Figure 1 is an isometric view of the wave V-shaped flame stabilizer of the present invention.
图2为本发明中波浪形V型火焰稳定器的侧视图。Figure 2 is a side view of the wave-shaped V-shaped flame stabilizer in the present invention.
图3为本发明中波浪形V型火焰稳定器的俯视图。FIG. 3 is a top view of the wave-shaped V-shaped flame stabilizer in the present invention.
图4为本发明中波浪形V型火焰稳定器的前视图。Figure 4 is a front view of the wave-shaped V-shaped flame stabilizer of the present invention.
图5为本发明中波浪形V型火焰稳定器的后视图。Figure 5 is a rear view of the wave-shaped V-shaped flame stabilizer of the present invention.
图6为本发明中波浪形V型火焰稳定器的纵向截面VX分布。Fig. 6 is the longitudinal section V X distribution of the wave-shaped V-shaped flame stabilizer in the present invention.
图7为本发明中波浪形V型火焰稳定器的横向截面VX分布。Fig. 7 is the V X distribution of the transverse section of the wave-shaped V-shaped flame stabilizer in the present invention.
图8为本发明中波浪形V型火焰稳定器的流线图。FIG. 8 is a streamline diagram of the wave-shaped V-shaped flame stabilizer in the present invention.
图9为本发明中波浪形V型火焰稳定器的另一视角流线图。FIG. 9 is another view of the streamline diagram of the wave-shaped V-shaped flame stabilizer in the present invention.
在附图中,1为前缘;2为V型面;3为V型尾缘。In the drawings, 1 is the leading edge; 2 is the V-shaped surface; 3 is the V-shaped trailing edge.
具体实施方式Detailed ways
下面将结合附图1~5和实施例对本发明进行进一步详细说明。The present invention will be further described in detail below with reference to the accompanying drawings 1 to 5 and the embodiments.
一种波浪形V型火焰稳定器,具波浪形几何特征,含3~5个波长,本实施例具体为3个,其各处横截面形状相同,所述的波浪形V型火焰稳定器,展长由具体发动机确定,本实施例具体为180mm,主要由前缘1、V型面2、V型尾缘3组成,在横截面上,前缘1为对V型面2倒圆角得到,圆角半径1.5~5mm,本实施例具体为2.5mm,V型面2宽20~30mm,本实施例具体为24mm,V型面2的V形夹角25°~40°,本实施例具体为30°,V型尾缘3宽26~36mm,本实施例具体为30mm,V型尾缘3的前V形夹角55°~70°,本实施例具体为60°,V型尾缘3的后V形夹角100°~150°,本实施例具体为120°,侧面平直段宽1.5~3mm,本实施例具体为2mm,所述的波浪形几何特征,在波峰位置起始和终止,波浪形为在锯齿形波的波峰和波谷倒圆角得到,圆角半径15~30mm,本实施例具体为18mm,锯齿形波振幅为6~15mm,本实施例具体为12mm。A wave-shaped V-shaped flame stabilizer has a wave-shaped geometric feature, and contains 3 to 5 wavelengths. In this embodiment, there are 3 wavelengths, and the cross-sectional shapes are the same everywhere. The wave-shaped V-shaped flame stabilizer, The length is determined by the specific engine. In this embodiment, it is 180mm, which is mainly composed of leading edge 1, V-
以上所述实施方式仅为本发明的优选实施例,而并非本发明可行实施的穷举。对于本领域的一般技术人员而言,在不背离本发明原理和精神的前提下对其所做出的任何显而易见的改动,都应当被认为包含在本发明的权利要求保护范围之内。因此,本发明的保护范围应以所述权利要求的保护范围为准。The above-mentioned embodiments are only preferred embodiments of the present invention, rather than an exhaustive list of feasible implementations of the present invention. For those skilled in the art, any obvious changes made to it without departing from the principle and spirit of the present invention should be considered to be included in the protection scope of the claims of the present invention. Therefore, the protection scope of the present invention should be based on the protection scope of the claims.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110812824.9A CN113551261B (en) | 2021-07-19 | 2021-07-19 | Wave V type flame stabilizer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110812824.9A CN113551261B (en) | 2021-07-19 | 2021-07-19 | Wave V type flame stabilizer |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN113551261A CN113551261A (en) | 2021-10-26 |
| CN113551261B true CN113551261B (en) | 2022-06-14 |
Family
ID=78103354
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110812824.9A Active CN113551261B (en) | 2021-07-19 | 2021-07-19 | Wave V type flame stabilizer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113551261B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115823616B (en) * | 2022-12-02 | 2024-11-26 | 南昌航空大学 | A V-shaped flame stabilizer with serrated trailing edge and ribs |
| CN115854384B (en) * | 2023-01-08 | 2025-06-24 | 南昌航空大学 | Support plate flame stabilizer with wavy concave cavities |
| CN116428613B (en) * | 2023-04-17 | 2025-06-24 | 南昌航空大学 | A flame stabilizer with double corrugated ribs |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1153034A (en) * | 1965-09-21 | 1969-05-21 | Rolls Royce | Combustion Apparatus |
| CN102607061A (en) * | 2012-03-26 | 2012-07-25 | 北京航空航天大学 | Geometrical variable flame stabilizing device |
| CN104048324A (en) * | 2014-07-24 | 2014-09-17 | 南京航空航天大学 | Evaporation type flame stabilizer |
| CN105841191A (en) * | 2016-03-30 | 2016-08-10 | 中国科学院工程热物理研究所 | Tail edge structure of V-shaped flame stabilizer |
| WO2017092044A1 (en) * | 2015-12-04 | 2017-06-08 | 深圳智慧能源技术有限公司 | Flame stabilizer of venturi burner |
| CN109631084A (en) * | 2018-12-13 | 2019-04-16 | 西安航天动力研究所 | Scramjet combustor stabilizer and steady flame method |
| CN110274259A (en) * | 2019-06-13 | 2019-09-24 | 中国人民解放军空军工程大学 | A kind of plasma excitation Formula V type flameholder |
| CN112728584A (en) * | 2020-11-24 | 2021-04-30 | 南京航空航天大学 | Flame stabilizer, radial flame stabilizer and combustion chamber |
| CN213300149U (en) * | 2020-06-24 | 2021-05-28 | 南昌航空大学 | V-shaped flame stabilizer with turbulence structure capable of being premixed |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100414668B1 (en) * | 2001-07-21 | 2004-01-07 | 삼성전자주식회사 | Flame stabilizer of burner for flame hydrolysis deposition process |
| US7013635B2 (en) * | 2003-12-30 | 2006-03-21 | United Technologies Corporation | Augmentor with axially displaced vane system |
| DE102007043626A1 (en) * | 2007-09-13 | 2009-03-19 | Rolls-Royce Deutschland Ltd & Co Kg | Gas turbine lean burn burner with fuel nozzle with controlled fuel inhomogeneity |
-
2021
- 2021-07-19 CN CN202110812824.9A patent/CN113551261B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1153034A (en) * | 1965-09-21 | 1969-05-21 | Rolls Royce | Combustion Apparatus |
| CN102607061A (en) * | 2012-03-26 | 2012-07-25 | 北京航空航天大学 | Geometrical variable flame stabilizing device |
| CN104048324A (en) * | 2014-07-24 | 2014-09-17 | 南京航空航天大学 | Evaporation type flame stabilizer |
| WO2017092044A1 (en) * | 2015-12-04 | 2017-06-08 | 深圳智慧能源技术有限公司 | Flame stabilizer of venturi burner |
| CN105841191A (en) * | 2016-03-30 | 2016-08-10 | 中国科学院工程热物理研究所 | Tail edge structure of V-shaped flame stabilizer |
| CN109631084A (en) * | 2018-12-13 | 2019-04-16 | 西安航天动力研究所 | Scramjet combustor stabilizer and steady flame method |
| CN110274259A (en) * | 2019-06-13 | 2019-09-24 | 中国人民解放军空军工程大学 | A kind of plasma excitation Formula V type flameholder |
| CN213300149U (en) * | 2020-06-24 | 2021-05-28 | 南昌航空大学 | V-shaped flame stabilizer with turbulence structure capable of being premixed |
| CN112728584A (en) * | 2020-11-24 | 2021-04-30 | 南京航空航天大学 | Flame stabilizer, radial flame stabilizer and combustion chamber |
Non-Patent Citations (2)
| Title |
|---|
| 火焰稳定器综述;金莉;《火箭推进》;20060228;第32卷(第1期);第30-34页 * |
| 航空发动机环管燃烧室喷雾燃烧性能研究;王成军;《燃气涡轮试验与研究》;20140228;第27卷(第1期);第32-35页 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN113551261A (en) | 2021-10-26 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN113551261B (en) | Wave V type flame stabilizer | |
| CN113566236B (en) | A wave trailing edge support plate flame stabilizer with a vortex generator | |
| CN113701190B (en) | A support plate flame stabilizer with finned vortex generator | |
| CN113551259B (en) | A wavy mid-slit V-shaped flame stabilizer with a lobed dividing plate | |
| CN113551262B (en) | A strut flame holder with a crescent dune profile | |
| EP2824320B1 (en) | Reduced noise vortex generator for wind turbine blade | |
| CN113701192B (en) | A wave-shaped double V-shaped flame stabilizer with sawtooth | |
| CN112282857B (en) | Air film cooling hole type structure | |
| CN114857617B (en) | A support plate flame stabilizer with a saw-tooth groove vortex generator | |
| CN112178692B (en) | A longitudinal corrugated cooling structure with L-shaped impact orifice plate | |
| CN115854384B (en) | Support plate flame stabilizer with wavy concave cavities | |
| CN107013255A (en) | A kind of turbine blade tail flow-disturbing with continuous straight rib partly splits seam cooling structure | |
| CN112177683B (en) | A rosary-type turbine blade trailing edge split cooling structure | |
| CN115899763B (en) | Tail edge shearing strengthening flame stabilizer of stress application or stamping combustion chamber | |
| CN116379471B (en) | Support plate flame stabilizer combining vortex generator and concave cavity | |
| CN115930261B (en) | Flame stabilizer with ribs for corrugated tail edge support plate | |
| CN115823616B (en) | A V-shaped flame stabilizer with serrated trailing edge and ribs | |
| CN110107914A (en) | One kind being based on the impact-gaseous film control structure of triangular-section deflector (ring) | |
| CN116428613B (en) | A flame stabilizer with double corrugated ribs | |
| CN118292951A (en) | A C-type film hole cooling structure for hot end components of gas turbines | |
| CN115751378B (en) | Support plate flame stabilizer with trapezoidal ribs and triangular convex blocks | |
| CN117366624A (en) | Blunt body flame stabilizer capable of changing characteristics of backflow area | |
| CN115045719A (en) | A Turbine Blade Using Crescent Shield-Scale Composite Cooling Structure | |
| CN203928005U (en) | A kind of advanced vortex combustion cavity that installs long direction eddy generator additional | |
| CN113701191B (en) | A V-shaped flame stabilizer with staggered diversion and slits |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |