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CN115930262A - Support plate flame stabilizer with U-shaped grooves - Google Patents

Support plate flame stabilizer with U-shaped grooves Download PDF

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CN115930262A
CN115930262A CN202310022673.6A CN202310022673A CN115930262A CN 115930262 A CN115930262 A CN 115930262A CN 202310022673 A CN202310022673 A CN 202310022673A CN 115930262 A CN115930262 A CN 115930262A
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flame stabilizer
support plate
shaped groove
hoof
shaped
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CN115930262B (en
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廖文彬
盛志强
钟尉
胡晓安
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Nanchang Hangkong University
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Nanchang Hangkong University
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Abstract

本发明涉及一种带蹄形凹槽的支板火焰稳定器,支板火焰稳定器由前缘、平直段、V型底面组成,在平直段两侧面都布置有3~5个蹄形凹槽。本发明的优点和取得的有益效果为:加力燃烧室采用该带蹄形凹槽的支板火焰稳定器,火焰稳定性能好,燃烧效率高,流阻损失小。

Figure 202310022673

The invention relates to a support plate flame stabilizer with a shoe-shaped groove. The support plate flame stabilizer is composed of a front edge, a straight section and a V-shaped bottom surface. groove. The advantages and beneficial effects of the invention are: the afterburner adopts the support plate flame stabilizer with shoe-shaped grooves, which has good flame stability, high combustion efficiency and small flow resistance loss.

Figure 202310022673

Description

一种带蹄形凹槽的支板火焰稳定器A support plate flame stabilizer with a shoe-shaped groove

技术领域technical field

本发明涉及一种带蹄形凹槽的支板火焰稳定器,其可用于高推重比航空发动机的一体化加力燃烧室,属于航空技术领域。The invention relates to a support plate flame stabilizer with a shoe-shaped groove, which can be used for an integrated afterburner of an aero-engine with a high thrust-to-weight ratio, and belongs to the field of aviation technology.

背景技术Background technique

新一代加力涡扇发动机追求高的推重比,在加力燃烧室方面,就要求零部件简洁,冷态流阻损失低,加力段长度占比小,同时加力燃烧效率高。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。新一代加力涡扇发动机大多采用整流支板与火焰稳定器一体化设计的一体化加力燃烧室。但常规支板火焰稳定器产生卡门涡街型回流涡,其回流涡稳定性较差,会导致局部不稳定的燃烧。The new-generation afterburning turbofan engine pursues a high thrust-to-weight ratio. In terms of the afterburner, it requires simple parts, low cold flow resistance loss, a small proportion of the length of the afterburner section, and high afterburner efficiency. The afterburner uses a flame stabilizer to stabilize the flame and organize combustion, and the performance of the flame stabilizer is a decisive factor affecting the performance of the afterburner. Most of the new generation of afterburning turbofan engines use an integrated afterburner with an integrated design of rectifying struts and flame stabilizers. However, the conventional support plate flame stabilizer produces Karman vortex street type recirculation vortex, which has poor stability and will lead to local unstable combustion.

因加力段长度占比小,燃油喷射到火焰稳定器后缘距离相应变小,在被点燃前燃油雾化、蒸发和掺混不充分,容易导致燃烧不稳定,与回流涡导致的不稳定燃烧叠加后,会放大燃烧不稳定问题,进而影响燃烧反应进程;火焰稳定器后缘到喷管出口距离相应变小,燃烧段变短,火焰稳定器后回流区火焰在横向来不及传遍整个燃烧室,部分油气混合物未被充分燃烧,部分油气混合物未参与燃烧而被直接排出,因而严重影响了加力燃烧效率。Due to the small proportion of the length of the afterburner section, the distance from the fuel injection to the trailing edge of the flame stabilizer is correspondingly reduced, and the fuel atomization, evaporation and mixing are insufficient before being ignited, which easily leads to combustion instability and instability caused by the backflow vortex. After the combustion is superimposed, the problem of combustion instability will be magnified, which will affect the combustion reaction process; the distance from the rear edge of the flame stabilizer to the outlet of the nozzle will be correspondingly reduced, the combustion section will be shortened, and the flame in the recirculation area behind the flame stabilizer will not have time to spread throughout the entire combustion in the horizontal direction In the chamber, part of the oil-air mixture is not fully burned, and part of the oil-air mixture is directly discharged without participating in the combustion, thus seriously affecting the afterburner efficiency.

发明内容Contents of the invention

本发明的目的在于提供一种带蹄形凹槽的支板火焰稳定器,在支板火焰稳定器两侧面布置蹄形凹槽,以提高火焰稳定性,减小流动损失,增大燃烧效率。The object of the present invention is to provide a support plate flame stabilizer with a shoe-shaped groove, and the shoe-shaped grooves are arranged on both sides of the support plate 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.

一种带蹄形凹槽的支板火焰稳定器,在支板火焰稳定器两侧面都均匀布置3~5个蹄形凹槽。A support plate flame stabilizer with shoe-shaped grooves, 3 to 5 shoe-shaped grooves are evenly arranged on both sides of the support plate flame stabilizer.

进一步,所述的支板火焰稳定器,弦长90~150mm,展长由具体发动机确定,由前缘、平直段、V型底面组成,前缘为椭圆型面,椭圆长轴尺寸是短轴的1.7~2.5倍,前缘与平直段相切连续,平直段宽24~36mm,V型底面夹角100°~150°。Further, the support plate flame stabilizer has a chord length of 90 to 150 mm, and the spread length is determined by a specific engine, and is composed of a front edge, a straight section, and a V-shaped bottom surface. The front edge is an elliptical surface, and the major axis of the ellipse is short 1.7 to 2.5 times the axis, the front edge is tangent and continuous to the straight section, the width of the straight section is 24 to 36 mm, and the included angle of the V-shaped bottom surface is 100° to 150°.

进一步,所述的蹄形凹槽,其尾缘与支板火焰稳定器尾缘齐平,蹄形凹槽尾缘长40~50mm,高1~2mm,蹄形凹槽底面前低后高,与平直段表面夹角10~20°,蹄形凹槽的两条前缘曲线都为连接顶点和尾缘端点的样条线,在俯视方向,在平直段表面内的前缘曲线的顶点到尾缘的距离为23~28mm,在底面内的前缘曲线的顶点到尾缘的距离为20~25mm。Further, the tail edge of the shoe-shaped groove is flush with the tail edge of the support plate flame stabilizer, the tail edge of the shoe-shaped groove is 40-50mm long, and the height is 1-2mm. The angle between the surface of the straight section and the straight section is 10-20°, and the two leading edge curves of the shoe-shaped groove are both splines connecting the apex and the end point of the trailing edge. The distance from the apex to the trailing edge is 23-28 mm, and the distance from the apex to the trailing edge of the leading edge curve in the bottom surface is 20-25 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 prior art, advantage of the present invention and the beneficial effect that obtain are:

第一,火焰稳定性能好。常规支板火焰稳定器产生卡门涡街型回流涡,其回流涡脱落频率较高,回流涡稳定性较差,容易出现燃烧不稳定问题。且燃油喷出到回流区距离非常短,燃油蒸发和掺混不充分,容易导致不稳定的燃烧。在常规支板火焰稳定器两侧布置蹄形凹槽后,蹄形凹槽内形成牛角形驻涡,有利于燃油的蒸发和掺混;稳定器后的卡门涡街型回流涡的脱落频率也降低很多,回流涡稳定性增强。因而布置蹄形凹槽后火焰稳定性能更好。First, the flame stability is good. The conventional support plate flame stabilizer produces Karman vortex street type reflux vortex, the frequency of reflux vortex shedding is high, the stability of reflux vortex is poor, and combustion instability is prone to occur. Moreover, the distance from the fuel injection to the recirculation area is very short, and the evaporation and mixing of the fuel are not sufficient, which easily leads to unstable combustion. After the shoe-shaped grooves are arranged on both sides of the conventional support plate flame stabilizer, a cow-horn-shaped dwelling vortex is formed in the shoe-shaped grooves, which is beneficial to the evaporation and mixing of fuel oil; the shedding frequency of the Karman vortex street type return vortex behind the stabilizer It is much lower, and the stability of the reflux vortex is enhanced. Therefore, the flame stability performance is better after the shoe-shaped groove is arranged.

第二,燃烧效率高。在常规支板火焰稳定器两侧布置蹄形凹槽后,蹄形凹槽内形成牛角形驻涡,有利于燃油的蒸发和掺混;稳定器后的卡门涡街型回流涡的脱落频率也降低很多,回流涡稳定性增强。因而布置蹄形凹槽后有利于获得更稳定高效的燃烧,从而达成更高的燃烧效率。Second, the combustion efficiency is high. After the shoe-shaped grooves are arranged on both sides of the conventional support plate flame stabilizer, a cow-horn-shaped dwelling vortex is formed in the shoe-shaped grooves, which is beneficial to the evaporation and mixing of fuel oil; the shedding frequency of the Karman vortex street type return vortex behind the stabilizer It is much lower, and the stability of the reflux vortex is enhanced. Therefore, the arrangement of the shoe-shaped groove is conducive to obtaining more stable and efficient combustion, thereby achieving higher combustion efficiency.

第三,流阻损失小。要达到同样的火焰稳定性能、燃烧效率,与增加常规支板火焰稳定器的堵塞宽度相比,在常规支板火焰稳定器两侧布置蹄形凹槽,所引起的流阻损失更小,而且,减小卡门涡街型回流涡的脱落频率,有利于减小流阻损失。Third, the flow resistance loss is small. To achieve the same flame stability performance and combustion efficiency, compared with increasing the plugging width of the conventional support plate flame stabilizer, arranging shoe-shaped grooves on both sides of the conventional support plate flame stabilizer will cause less flow resistance loss, and , reducing the shedding frequency of the Karman vortex street type return vortex is beneficial to reducing the loss of flow resistance.

附图说明Description of drawings

图1为本发明中带蹄形凹槽的支板火焰稳定器的等轴视图。BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is an isometric view of a shoe-shaped grooved strut flame holder of the present invention.

图2为本发明中带蹄形凹槽的支板火焰稳定器的侧视图。Fig. 2 is a side view of a support plate flame stabilizer with a shoe-shaped groove in the present invention.

图3为本发明中带蹄形凹槽的支板火焰稳定器的俯视图。Fig. 3 is a top view of a support plate flame stabilizer with a shoe-shaped groove in the present invention.

图4为本发明中带蹄形凹槽的支板火焰稳定器的前视图。Fig. 4 is a front view of a support plate flame stabilizer with a shoe-shaped groove in the present invention.

图5为本发明中带蹄形凹槽的支板火焰稳定器的后视图。Fig. 5 is a rear view of a support plate flame stabilizer with a shoe-shaped groove in the present invention.

图6为常规支板火焰稳定器的纵向截面VX分布。Fig. 6 is a longitudinal section V X distribution of a conventional strut plate flame holder.

图7为常规支板火焰稳定器的横向截面VX分布。Fig. 7 is a cross-sectional V X distribution of a conventional strut plate flame holder.

图8为本发明中带蹄形凹槽的支板火焰稳定器的纵向截面VX分布。Fig. 8 is the longitudinal section V X distribution of the support plate flame stabilizer with shoe-shaped groove in the present invention.

图9为本发明中带蹄形凹槽的支板火焰稳定器的横向截面VX分布。Fig. 9 is the cross-section V X distribution of the support plate flame stabilizer with shoe-shaped grooves in the present invention.

图10为本发明中带蹄形凹槽的支板火焰稳定器的流线图一。Fig. 10 is the streamline diagram 1 of the support plate flame stabilizer with shoe-shaped groove in the present invention.

图11为本发明中带蹄形凹槽的支板火焰稳定器的流线图二。Fig. 11 is the second streamline diagram of the support plate flame stabilizer with shoe-shaped grooves in the present invention.

在附图中,1为前缘;2为平直段;3为V型底面;4为蹄形凹槽;L1为支板火焰稳定器弦长;L2为蹄形凹槽在蹄形凹槽底面内的前缘曲线的顶点到尾缘的距离;L3为蹄形凹槽在平直段表面内的前缘曲线的顶点到尾缘的距离;W1为平直段宽;W2为蹄形凹槽尾缘高;H1为支板火焰稳定器展长;H2为蹄形凹槽尾缘长;α为支板火焰稳定器V型底面夹角;In the accompanying drawings, 1 is the front edge; 2 is the straight section; 3 is the V-shaped bottom surface; 4 is the shoe-shaped groove; L1 is the chord length of the support plate flame stabilizer; L2 is the shoe-shaped groove in the shoe-shaped groove The distance from the vertex of the leading edge curve in the bottom surface to the trailing edge; L3 is the distance from the vertex of the leading edge curve to the trailing edge of the shoe-shaped groove in the straight section surface; W1 is the width of the straight section; W2 is the shoe-shaped concave The height of the tail edge of the groove; H1 is the extension length of the flame stabilizer of the support plate; H2 is the length of the tail edge of the shoe-shaped groove; α is the included angle of the V-shaped bottom surface of the flame stabilizer of the support plate;

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 in conjunction with accompanying drawings 1 to 5 and embodiments.

一种带蹄形凹槽的支板火焰稳定器,在支板火焰稳定器两侧面都均匀布置3~5个蹄形凹槽4,本实施例具体为3个。A support plate flame stabilizer with shoe-shaped grooves, 3 to 5 shoe-shaped grooves 4 are evenly arranged on both sides of the support plate flame stabilizer, specifically 3 in this embodiment.

作为本发明实施例的进一步改进,所述的支板火焰稳定器,弦长L1为90~150mm,本实施例具体为120mm,展长H1由具体发动机确定,本实施例具体为180mm,由前缘1、平直段2、V型底面3组成,前缘1为椭圆型面,椭圆长轴尺寸是短轴的1.7~2.5倍,本实施例具体为1.77倍,前缘1与平直段2相切连续,平直段2宽W1为24~36mm,本实施例具体为26mm,V型底面3夹角α为100°~150°,本实施例具体为120°。As a further improvement of the embodiment of the present invention, the support plate flame stabilizer has a chord length L1 of 90 to 150 mm, specifically 120 mm in this embodiment, and the extension H1 is determined by a specific engine, specifically 180 mm in this embodiment, as stated in the previous Edge 1, straight section 2, and V-shaped bottom surface 3. Front edge 1 is an elliptical surface. 2 is tangentially continuous, the width W1 of the straight section 2 is 24-36 mm, specifically 26 mm in this embodiment, and the included angle α of the V-shaped bottom surface 3 is 100°-150°, specifically 120° in this embodiment.

作为本发明实施例的进一步改进,所述的蹄形凹槽4,其尾缘与支板火焰稳定器尾缘齐平,蹄形凹槽尾缘长H2为40~50mm,本实施例具体为46mm,蹄形凹槽尾缘高w2为1~2mm,本实施例具体为1mm,蹄形凹槽底面前低后高,与平直段表面夹角10~20°,本实施例具体为15°,蹄形凹槽的两条前缘曲线都为连接顶点和尾缘端点的样条线,在俯视方向,在平直段表面内的前缘曲线的顶点到尾缘的距离L3为23~28mm,本实施例具体为25mm,在底面内的前缘曲线的顶点到尾缘的距离L2为20~25mm,本实施例具体为22mm。As a further improvement of the embodiment of the present invention, the trailing edge of the shoe-shaped groove 4 is flush with the trailing edge of the support plate flame stabilizer, and the length H2 of the trailing edge of the shoe-shaped groove is 40-50mm. This embodiment is specifically 46mm, the height w2 of the trailing edge of the hoof-shaped groove is 1-2mm, specifically 1mm in this embodiment, the front of the bottom of the hoof-shaped groove is low and the rear is high, and the angle with the surface of the straight section is 10-20°, and this embodiment is specifically 15 °, the two leading edge curves of the shoe-shaped groove are both splines connecting the apex and the trailing edge endpoint, and in the top view direction, the distance L3 from the vertex of the leading edge curve to the trailing edge in the straight section surface is 23~ 28 mm, specifically 25 mm in this embodiment, and the distance L2 from the apex of the leading edge curve in the bottom surface to the trailing edge is 20-25 mm, specifically 22 mm in this embodiment.

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 implementation manners described above 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 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 determined by the protection scope of the claims.

Claims (1)

1. A supporting plate flame stabilizer with hoof-shaped grooves is characterized in that 3-5 hoof-shaped grooves (4) are uniformly arranged on two side surfaces of the supporting plate flame stabilizer; the support plate flame stabilizer has a chord length of 90-150 mm, an extension length is determined by a specific engine, the support plate flame stabilizer consists of a front edge (1), a straight section (2) and a V-shaped bottom surface (3), the front edge (1) is an elliptical profile, the size of the long axis of the ellipse is 1.7-2.5 times of that of the short axis, the front edge (1) is tangent and continuous with the straight section (2), the straight section (2) is 24-36mm wide, and an included angle of the V-shaped bottom surface (3) is 100-150 degrees; the tail edge of the hoof-shaped groove (4) is flush with the tail edge of the support plate flame stabilizer, the length of the tail edge of the hoof-shaped groove (4) is 40-50 mm, the height of the tail edge of the hoof-shaped groove (4) is 1-2 mm, the front of the bottom surface of the hoof-shaped groove (4) is low, the rear of the bottom surface of the hoof-shaped groove (4) is high, an included angle between the bottom surface of the hoof-shaped groove (4) and the surface of the straight section (2) is 10-20 degrees, two front edge curves of the hoof-shaped groove (4) are sample lines connecting a vertex and tail edge end points, the distance from the vertex of the front edge curve in the surface of the straight section (2) to the tail edge is 23-28 mm in the overlooking direction, and the distance from the vertex of the front edge curve in the bottom surface of the hoof-shaped groove (4) to the tail edge is 20-25 mm.
CN202310022673.6A 2023-01-08 2023-01-08 A flame stabilizer with a support plate having a horseshoe-shaped groove Active CN115930262B (en)

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108131684A (en) * 2017-12-14 2018-06-08 西北工业大学 A kind of annular oil feeding type integration after-burner
CN113551262A (en) * 2021-07-19 2021-10-26 南昌航空大学 A strut flame holder with a crescent dune profile
CN113566236A (en) * 2021-07-19 2021-10-29 南昌航空大学 A wave trailing edge support plate flame stabilizer with a vortex generator
CN113701190A (en) * 2021-09-01 2021-11-26 南昌航空大学 Take fin vortex generator's extension board flame holder
CN114857617A (en) * 2022-05-20 2022-08-05 南昌航空大学 Take supporting plate flame stabilizer of sawtooth pattern recess vortex generator

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108131684A (en) * 2017-12-14 2018-06-08 西北工业大学 A kind of annular oil feeding type integration after-burner
CN113551262A (en) * 2021-07-19 2021-10-26 南昌航空大学 A strut flame holder with a crescent dune profile
CN113566236A (en) * 2021-07-19 2021-10-29 南昌航空大学 A wave trailing edge support plate flame stabilizer with a vortex generator
CN113701190A (en) * 2021-09-01 2021-11-26 南昌航空大学 Take fin vortex generator's extension board flame holder
CN114857617A (en) * 2022-05-20 2022-08-05 南昌航空大学 Take supporting plate flame stabilizer of sawtooth pattern recess vortex generator

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