CN115164236A - Heat insulation assembly suitable for oil thrower disc combustion chamber - Google Patents
Heat insulation assembly suitable for oil thrower disc combustion chamber Download PDFInfo
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- CN115164236A CN115164236A CN202210673950.5A CN202210673950A CN115164236A CN 115164236 A CN115164236 A CN 115164236A CN 202210673950 A CN202210673950 A CN 202210673950A CN 115164236 A CN115164236 A CN 115164236A
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- diffuser
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- 238000002485 combustion reaction Methods 0.000 title claims abstract description 63
- 238000009413 insulation Methods 0.000 title claims abstract description 17
- 229910001220 stainless steel Inorganic materials 0.000 claims description 6
- 239000010935 stainless steel Substances 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 3
- 230000003746 surface roughness Effects 0.000 claims description 3
- NMFHJNAPXOMSRX-PUPDPRJKSA-N [(1r)-3-(3,4-dimethoxyphenyl)-1-[3-(2-morpholin-4-ylethoxy)phenyl]propyl] (2s)-1-[(2s)-2-(3,4,5-trimethoxyphenyl)butanoyl]piperidine-2-carboxylate Chemical compound C([C@@H](OC(=O)[C@@H]1CCCCN1C(=O)[C@@H](CC)C=1C=C(OC)C(OC)=C(OC)C=1)C=1C=C(OCCN2CCOCC2)C=CC=1)CC1=CC=C(OC)C(OC)=C1 NMFHJNAPXOMSRX-PUPDPRJKSA-N 0.000 description 22
- 230000005855 radiation Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 238000001816 cooling Methods 0.000 description 3
- 239000012530 fluid Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Classifications
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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
- F23R3/38—Continuous 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)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
Description
技术领域technical field
本发明涉及甩油盘燃烧室技术领域,具体来说,涉及一种适用于甩油盘燃烧室的隔热组件。The invention relates to the technical field of an oil slinger combustion chamber, in particular to a heat insulation assembly suitable for an oil slinger combustion chamber.
背景技术Background technique
甩油盘式燃烧室在微小型发动机上应用较为广泛,微小型发动机转速较高,在4W-10W转之间,该转速产生的离心力可大大提高燃油的雾化效果。高温燃气增加了燃烧室对周边零件的热辐射,其中影响较大的是压气机部件。The oil throwing disc type combustion chamber is widely used in micro and small engines, and the micro and small engines have a high rotational speed. Between 4W-10W revolutions, the centrifugal force generated by this rotational speed can greatly improve the atomization effect of fuel. The high temperature gas increases the heat radiation of the combustion chamber to the surrounding parts, among which the compressor parts are the most affected.
现有甩油盘式燃烧室的外环和压气机扩压器之间无阻碍热辐射的设计,导致燃烧室向压气机部件辐射大量的热,压气机温度升高、效率下降。同时扩压器温度升高会导致零件刚性变差、形变增加,带来零件热态变形加大、压气机间隙变化等风险,可能进一步导致效率下降。The existing design of unobstructed heat radiation between the outer ring of the oil throwing pan combustion chamber and the compressor diffuser causes the combustion chamber to radiate a large amount of heat to the compressor components, increasing the temperature of the compressor and decreasing the efficiency. At the same time, the increase of the temperature of the diffuser will lead to the deterioration of the rigidity of the parts and the increase of the deformation, which will bring risks such as increased thermal deformation of the parts and changes in the compressor clearance, which may further lead to a decrease in efficiency.
针对相关技术中的问题,目前尚未提出有效的解决方案。For the problems in the related technologies, no effective solutions have been proposed so far.
发明内容SUMMARY OF THE INVENTION
针对相关技术中的问题,本发明提出一种适用于甩油盘燃烧室的隔热组件,通过在燃烧室和扩压器直接设置隔热屏,可有效降低燃烧室向扩压器的热辐射,降低扩压器温度,提高压气机效率,以克服现有相关技术所存在的上述技术问题。In view of the problems in the related art, the present invention proposes a heat insulation assembly suitable for the combustion chamber of the oil slinger. By directly arranging the heat shield on the combustion chamber and the diffuser, the heat radiation from the combustion chamber to the diffuser can be effectively reduced , reduce the temperature of the diffuser and improve the efficiency of the compressor, so as to overcome the above-mentioned technical problems existing in the related art.
本发明的技术方案是这样实现的:The technical scheme of the present invention is realized as follows:
一种适用于甩油盘燃烧室的隔热组件,包括:燃烧室和扩压器,所述燃烧室和所述扩压器之间形成环腔;A heat insulation assembly suitable for an oil slinger combustion chamber, comprising: a combustion chamber and a diffuser, an annular cavity is formed between the combustion chamber and the diffuser;
所述环腔内设有隔热屏,所述隔热屏底端与所述扩压器连接,且所述隔热屏与所述燃烧室之间形成气流流道,气流从上往下通过气流流道流向所述燃烧室入口。The annular cavity is provided with a heat shield, the bottom end of the heat shield is connected to the diffuser, and an airflow channel is formed between the heat shield and the combustion chamber, and the airflow passes from top to bottom The airflow runner flows toward the combustion chamber inlet.
进一步的,所述隔热屏位于燃烧室和扩压器之间,且所述隔热屏的底端通过螺栓与所述扩压器固定连接。Further, the heat shield is located between the combustion chamber and the diffuser, and the bottom end of the heat shield is fixedly connected to the diffuser through bolts.
进一步的,所述隔热屏的材料为S304不锈钢或S310不锈钢。Further, the material of the heat shield is S304 stainless steel or S310 stainless steel.
进一步的,所述隔热屏为曲面结构。Further, the heat shield has a curved structure.
进一步的,所述隔热屏的表面粗糙度大于3.2mm。Further, the surface roughness of the heat shield is greater than 3.2 mm.
进一步的,所述隔热屏的厚度为1mm~3mm。Further, the thickness of the heat shield is 1mm˜3mm.
本发明的有益效果:Beneficial effects of the present invention:
1、本发明适用于甩油盘燃烧室的隔热组件,通过在燃烧室和扩压器直接设置隔热屏,可有效降低燃烧室向扩压器的热辐射,降低扩压器温度,提高压气机效率。1. The present invention is suitable for the heat insulation assembly of the oil throwing pan combustion chamber. By directly setting the heat shield in the combustion chamber and the diffuser, the heat radiation from the combustion chamber to the diffuser can be effectively reduced, the temperature of the diffuser can be reduced, and the temperature of the diffuser can be increased. Compressor efficiency.
2、本发明适用于甩油盘燃烧室的隔热组件,气流流入环腔并通过隔热屏形成气流流道从上往下流向所述燃烧室入口,起到了导流的作用,而且曲面结构的隔热屏使得环腔流道变窄,其气流通过气流流道流速增加,提高了燃烧室入口气流的射流深度,进而提高冷却效果。2. The present invention is suitable for the heat insulation assembly of the oil throwing pan combustion chamber. The air flow flows into the annular cavity and forms an air flow channel through the heat shield to flow from top to bottom to the entrance of the combustion chamber, which plays the role of diversion, and the curved surface structure The heat shield makes the annular cavity flow channel narrow, and the flow velocity of the airflow through the airflow flow channel increases, which increases the jet depth of the airflow at the inlet of the combustion chamber, thereby improving the cooling effect.
附图说明Description of drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the accompanying drawings required in the embodiments will be briefly introduced below. Obviously, the drawings in the following description are only some of the present invention. In the embodiments, for those of ordinary skill in the art, other drawings can also be obtained according to these drawings without any creative effort.
图1是根据本发明实施例的一种适用于甩油盘燃烧室的隔热组件的结构示意图;FIG. 1 is a schematic structural diagram of a thermal insulation assembly suitable for an oil slinger combustion chamber according to an embodiment of the present invention;
图中:In the picture:
1、隔热屏;2、燃烧室;3、扩压器;4、环腔;5、气流流道。1. Heat shield; 2. Combustion chamber; 3. Diffuser; 4. Ring cavity; 5. Air flow channel.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments in the present invention, all other embodiments obtained by those of ordinary skill in the art fall within the protection scope of the present invention.
根据本发明的实施例,提供了一种适用于甩油盘燃烧室的隔热组件。According to an embodiment of the present invention, a thermal insulation assembly suitable for use in a slinger combustion chamber is provided.
如图1所示,根据本发明实施例的适用于甩油盘燃烧室的隔热组件,包括:燃烧室2和扩压器3,燃烧室2和扩压器3之间形成环腔4;As shown in FIG. 1 , the thermal insulation assembly suitable for the combustion chamber of the oil slinger according to the embodiment of the present invention includes: a
环腔4内设有隔热屏1,隔热屏1底端与扩压器3连接,且隔热屏1与燃烧室2之间形成气流流道5,气流从上往下通过气流流道5流向燃烧室2入口。The
借助于上述技术方案,通过在燃烧室2和扩压器3直接设置隔热屏1,可有效降低燃烧室2向扩压器3的热辐射,降低扩压器3温度,提高压气机效率。With the help of the above technical solution, by directly installing the
另外,隔热屏1位于燃烧室2和扩压器3之间,且隔热屏1的底端通过螺栓与扩压器3固定连接。In addition, the
本技术方案,甩油盘燃烧室一股气流从压气机出口折回180°向下流入燃烧室2和扩压器3之间的环腔4,该环腔4由于增加了隔热屏1,致使一股气流只能从隔热屏1和燃烧室2之间的气流流道5流入燃烧室2入口,起到了导流的作用。In this technical solution, an air flow from the combustion chamber of the oil throwing pan is folded back 180° from the compressor outlet and flows downward into the
另外,本技术方案,隔热屏1的材料为S304不锈钢或S310不锈钢;隔热屏1为曲面结构;隔热屏1的表面粗糙度大于3.2mm;隔热屏1的厚度为1mm~3mm。In addition, in this technical solution, the material of the
具体的,通过环腔4由于增加了隔热屏1,气流通过隔热屏1和燃烧室2之间的气流流道5流入燃烧室2入口,其隔热屏1使得一股气流的流道变窄,气体流速增加,提高了燃烧室2前端气流的射流深度,进而提高其冷却效果。Specifically, due to the addition of the
此外,通过曲面结构的隔热屏1经CFD(Computational Fluid Dynamics,计算流体动力学)计算有效降低了气体流动损失。另外,隔热屏1气流入口处进行倒圆角以降低流动损失。In addition, the gas flow loss is effectively reduced through CFD (Computational Fluid Dynamics, Computational Fluid Dynamics) calculation through the
综上,借助于本发明的上述技术方案,可实现如下效果:To sum up, with the aid of the above-mentioned technical solutions of the present invention, the following effects can be achieved:
1、本发明适用于甩油盘燃烧室的隔热组件,通过在燃烧室2和扩压器3直接设置隔热屏1,可有效降低燃烧室2向扩压器3的热辐射,降低扩压器3温度,提高压气机效率。1. The present invention is suitable for the heat insulation assembly of the combustion chamber of the oil slinger. By directly setting the
2、本发明适用于甩油盘燃烧室的隔热组件,气流流入环腔4并通过隔热屏1形成气流流道5从上往下流向燃烧室2入口,起到了导流的作用,而且曲面结构的隔热屏1使得环腔4流道变窄,其气流通过气流流道5流速增加,提高了燃烧室2入口气流的射流深度,进而提高冷却效果。2. The present invention is suitable for the heat insulation assembly of the oil throwing pan combustion chamber. The air flow flows into the
3、本发明适用于甩油盘燃烧室的隔热组件,隔热屏1通过结构设计降低了气体流动损失。3. The present invention is suitable for the heat insulation assembly of the oil throwing pan combustion chamber, and the
以上仅为本发明的较佳实施例而已,并不用以限制本发明,本领域技术人员在考虑说明书及实施例处的公开后,将容易想到本公开的其它实施方案。本申请旨在涵盖本公开的任何变型、用途或者适应性变化,这些变型、用途或者适应性变化遵循本公开的一般性原理并包括本公开未公开的本技术领域中的公知常识或惯用技术手段。说明书和实施例仅被视为示例性的,本公开的真正范围和精神由权利要求指出。The above are only preferred embodiments of the present invention, and are not intended to limit the present invention. Those skilled in the art will easily think of other embodiments of the present disclosure after considering the disclosure in the description and the examples. This application is intended to cover any variations, uses, or adaptations of the present disclosure that follow the general principles of the present disclosure and include common knowledge or techniques in the technical field not disclosed by the present disclosure . The specification and examples are to be regarded as exemplary only, with the true scope and spirit of the disclosure being indicated by the claims.
应当理解的是,本公开并不局限于上面已经描述并在附图中示出的精确结构,并且可以在不脱离其范围进行各种修改和改变。本公开的范围仅由所附的权利要求来限制。It is to be understood that the present disclosure is not limited to the precise structures described above and illustrated in the accompanying drawings, and that various modifications and changes may be made without departing from the scope thereof. The scope of the present disclosure is limited only by the appended claims.
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB686908A (en) * | 1948-11-30 | 1953-02-04 | Szydlowski Joseph | Improvements in or relating to combustion apparatus for a gas turbine unit |
CA2618781A1 (en) * | 2007-01-16 | 2008-07-16 | Honeywell International Inc. | Combustion systems with rotary fuel slingers |
CN203395943U (en) * | 2013-06-18 | 2014-01-15 | 中国航空动力机械研究所 | Combustion chamber flame tube |
CN205842740U (en) * | 2016-06-16 | 2016-12-28 | 上海和兰透平动力技术有限公司 | There is the toroidal combustion chamber of the gas turbine of self-cooling function |
CN107339712A (en) * | 2017-06-13 | 2017-11-10 | 中国航发湖南动力机械研究所 | Radial flow combustor diffuser and gas turbine |
WO2021176335A1 (en) * | 2020-03-02 | 2021-09-10 | Briggs & Stratton, Llc | Internal combustion engine with reduced oil maintenance |
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2022
- 2022-06-15 CN CN202210673950.5A patent/CN115164236A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB686908A (en) * | 1948-11-30 | 1953-02-04 | Szydlowski Joseph | Improvements in or relating to combustion apparatus for a gas turbine unit |
CA2618781A1 (en) * | 2007-01-16 | 2008-07-16 | Honeywell International Inc. | Combustion systems with rotary fuel slingers |
CN203395943U (en) * | 2013-06-18 | 2014-01-15 | 中国航空动力机械研究所 | Combustion chamber flame tube |
CN205842740U (en) * | 2016-06-16 | 2016-12-28 | 上海和兰透平动力技术有限公司 | There is the toroidal combustion chamber of the gas turbine of self-cooling function |
CN107339712A (en) * | 2017-06-13 | 2017-11-10 | 中国航发湖南动力机械研究所 | Radial flow combustor diffuser and gas turbine |
WO2021176335A1 (en) * | 2020-03-02 | 2021-09-10 | Briggs & Stratton, Llc | Internal combustion engine with reduced oil maintenance |
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