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CN113551261B - Wave V type flame stabilizer - Google Patents

Wave V type flame stabilizer Download PDF

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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
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shaped
wave
flame stabilizer
wavy
flame
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CN113551261A (en
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盛志强
但誉
张澜
江平
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Nanchang Hangkong University
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous 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
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means

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  • 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

The invention relates to a wavy V-shaped flame stabilizer which consists of a wavy front edge, a wavy V-shaped surface and a wavy V-shaped tail edge. The advantages and the obtained beneficial effects of the invention are as follows: by adopting the wave-shaped V-shaped flame stabilizer, the flame stability is good, the flow loss is small, and the combustion efficiency is high.

Description

一种波浪形V型火焰稳定器A wavy V-shaped flame stabilizer

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-shaped surface 2, and V-shaped trailing edge 3. In cross section, the leading edge 1 is obtained by rounding the V-shaped surface 2. , the radius of the fillet is 1.5~5mm, this embodiment is 2.5mm, the width of V-shaped surface 2 is 20~30mm, this embodiment is 24mm, the V-shaped angle of V-shaped surface 2 is 25°~40°, this embodiment Specifically, it is 30°, the width of the V-shaped trailing edge 3 is 26 to 36 mm, and the embodiment is 30 mm. The front V-shaped angle of the V-shaped trailing edge 3 is 55° to 70°. The rear V-shaped included angle of the edge 3 is 100°~150°, which is 120° in this embodiment, and the width of the flat side section is 1.5~3mm, which is 2mm in this embodiment. Begin and end, the wave shape is obtained by rounding the crest and trough of the sawtooth wave, the fillet radius is 15-30mm, the embodiment is 18mm, the sawtooth wave amplitude is 6-15mm, and the embodiment is 12mm.

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)

1. A wave-shaped V-shaped flame stabilizer is characterized by having wave-shaped geometrical characteristics, containing 3-5 wavelengths and having the same cross section shape at each part; the wavy V-shaped flame stabilizer mainly comprises a front edge (1), a V-shaped surface (2) and a V-shaped tail edge (3), wherein on the cross section, the front edge (1) is obtained by rounding the V-shaped surface (2), the radius of the fillet is 1.5-5 mm, the width of the V-shaped surface (2) is 20-30 mm, the V-shaped included angle of the V-shaped surface (2) is 25-40 degrees, the width of the V-shaped tail edge (3) is 26-36 mm, the front V-shaped included angle of the V-shaped tail edge (3) is 55-70 degrees, the rear V-shaped included angle of the V-shaped tail edge (3) is 100-150 degrees, and the width of a side flat section is 1.5-3 mm; the wave geometric characteristics start and end at the peak position, the wave is obtained by rounding off the peaks and the troughs of the sawtooth waves, the radius of the rounded corners is 15-30 mm, and the amplitude of the sawtooth waves is 6-15 mm.
2. The wavy V-shaped flame holder of claim 1, wherein the unfolding length of the wavy V-shaped flame holder is determined by a specific engine.
CN202110812824.9A 2021-07-19 2021-07-19 Wave V type flame stabilizer Active CN113551261B (en)

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Families Citing this family (3)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (9)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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 *

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