CN112066406A - A new type of combustion chamber - Google Patents
A new type of combustion chamber Download PDFInfo
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- CN112066406A CN112066406A CN202010905003.5A CN202010905003A CN112066406A CN 112066406 A CN112066406 A CN 112066406A CN 202010905003 A CN202010905003 A CN 202010905003A CN 112066406 A CN112066406 A CN 112066406A
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- combustion chamber
- flange
- carbon fiber
- cavity
- fiber layer
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M5/00—Casings; Linings; Walls
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M2700/00—Constructional details of combustion chambers
- F23M2700/005—Structures of combustion chambers or smoke ducts
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M2900/00—Special features of, or arrangements for combustion chambers
- F23M2900/05004—Special materials for walls or lining
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gasket Seals (AREA)
Abstract
本发明公开了一种新型的燃烧室,包括腔体和端头,端头可拆卸连接于腔体的端口,腔体包括有碳纤维层和隔热层,隔热层贴合于碳纤维层的内壁;碳纤维层的内壁设置有限位部,隔热层外壁设置有卡位部,卡位部和限位部卡紧配合。本发明中,隔热层能够隔绝腔体内部大部分的热量,碳纤维层的温度不会过高,其性能能够保持稳定;碳纤维层重量轻,抗张强度高,减少了燃烧室的重量,满足燃烧室的高压需求;卡位部和限位部卡紧配合,限制了隔热层的移动,提高了燃烧室的使用稳定性;腔体和端头之间可拆卸连接,用户使用时可根据使用的气压要求、温度要求,进而替换不同长度、不同厚度、不同内径的腔体,满足不同场景不同需求的应用。
The present invention discloses a novel combustion chamber, comprising a cavity and an end head, the end head is detachably connected to the port of the cavity, the cavity comprises a carbon fiber layer and a heat insulation layer, the heat insulation layer is attached to the inner wall of the carbon fiber layer; the inner wall of the carbon fiber layer is provided with a limiting portion, the outer wall of the heat insulation layer is provided with a clamping portion, and the clamping portion and the limiting portion are clamped together. In the present invention, the heat insulation layer can isolate most of the heat inside the cavity, the temperature of the carbon fiber layer will not be too high, and its performance can be kept stable; the carbon fiber layer is light in weight and high in tensile strength, which reduces the weight of the combustion chamber and meets the high pressure requirements of the combustion chamber; the clamping portion and the limiting portion are clamped together, which limits the movement of the heat insulation layer and improves the use stability of the combustion chamber; the cavity and the end head are detachably connected, and the user can replace the cavity of different lengths, thicknesses, and inner diameters according to the air pressure requirements and temperature requirements when using it, so as to meet the application of different scenarios and different requirements.
Description
技术领域technical field
本发明涉及燃烧室技术领域,特别是指一种新型的燃烧室。The invention relates to the technical field of combustion chambers, in particular to a novel combustion chamber.
背景技术Background technique
现有燃烧室结构以一体成型的金属内胆为前提的情况下,外层缠绕碳纤维层来实现燃烧室的高压要求。然而金属内胆易导热,金属内胆内部的热量容易传导到碳纤维层,高温会降低碳纤维层的各方面性能。并且,金属内胆的内部气压要求过高的情况下,金属内胆的厚度也相应增加,极大的增加了整体的重量。The existing combustion chamber structure is based on the premise of an integrally formed metal liner, and the outer layer is wound with a carbon fiber layer to meet the high pressure requirement of the combustion chamber. However, the metal liner is easy to conduct heat, and the heat inside the metal liner is easily conducted to the carbon fiber layer, and the high temperature will reduce the performance of the carbon fiber layer in all aspects. Moreover, when the internal air pressure of the metal liner is too high, the thickness of the metal liner also increases accordingly, which greatly increases the overall weight.
发明内容SUMMARY OF THE INVENTION
本发明要解决的技术问题是根据上述现有技术的不足,提出一种新型的燃烧室,解决了现有燃烧室耐高温性能差和重量大的问题。。The technical problem to be solved by the present invention is to propose a new type of combustion chamber based on the above-mentioned shortcomings of the prior art, which solves the problems of poor high temperature resistance and heavy weight of the existing combustion chamber. .
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:
一种新型的燃烧室,包括腔体和端头,所述端头可拆卸连接于所述腔体的端口,所述腔体包括有碳纤维层和隔热层,所述隔热层贴合于所述碳纤维层的内壁;所述碳纤维层的内壁设置有限位部,所述隔热层外壁设置有卡位部,所述卡位部和限位部卡紧配合。A new type of combustion chamber includes a cavity and an end, the end is detachably connected to the port of the cavity, the cavity includes a carbon fiber layer and a thermal insulation layer, and the thermal insulation layer is attached to the cavity. The inner wall of the carbon fiber layer; the inner wall of the carbon fiber layer is provided with a limiting portion, and the outer wall of the thermal insulation layer is provided with a locking portion, and the locking portion and the limiting portion are tightly matched.
进一步地,所述隔热层通过黏胶贴合于所述碳纤维层的内壁。Further, the heat insulating layer is attached to the inner wall of the carbon fiber layer by adhesive.
进一步地,所述卡位部和限位部中,任意一者为凸台,另外一者为凹槽,所述凸台嵌入所述凹槽中进而卡紧配合。Further, any one of the locking portion and the limiting portion is a boss, and the other is a groove, and the boss is embedded in the groove for clamping fit.
进一步地,所述碳纤维层为一体成型。Further, the carbon fiber layer is integrally formed.
进一步地,所述隔热层为三元乙丙橡胶。Further, the heat insulating layer is EPDM rubber.
进一步地,所述腔体的端部设置有第一法兰,所述端头的端部设置有第二法兰,所述第一法兰和第二法兰贴合并通过卡箍可拆卸抱紧连接。Further, the end of the cavity is provided with a first flange, the end of the end head is provided with a second flange, and the first flange and the second flange are attached and detachably held by a clamp. Tight connection.
进一步地,所述第一法兰和第二法兰之间设置有石棉垫片。Further, an asbestos gasket is arranged between the first flange and the second flange.
进一步地,所述第一法兰和第二法兰的外侧面均为斜坡结构。Further, the outer surfaces of the first flange and the second flange are both slope structures.
进一步地,所述第一法兰一体成型于所述碳纤维层的端部。Further, the first flange is integrally formed at the end of the carbon fiber layer.
采用上述技术方案,本发明的有益效果在于:Adopting the above-mentioned technical scheme, the beneficial effects of the present invention are:
(1)隔热层能够隔绝腔体内部大部分的热量,碳纤维层的温度不会过高,其性能能够保持稳定;碳纤维层重量轻,抗张强度高,减少了燃烧室的重量,满足燃烧室的高压需求。(1) The thermal insulation layer can isolate most of the heat inside the cavity, the temperature of the carbon fiber layer will not be too high, and its performance can remain stable; the carbon fiber layer is light in weight and high in tensile strength, which reduces the weight of the combustion chamber and meets the requirements of combustion high pressure requirements of the chamber.
(2)卡位部和限位部卡紧配合,限制了隔热层的移动,提高了燃烧室的使用稳定性。(2) The clamping part and the limiting part are tightly matched, which restricts the movement of the heat insulation layer and improves the use stability of the combustion chamber.
(3)腔体和端头之间可拆卸连接,用户使用时可根据使用的气压要求、温度要求,进而替换不同长度、不同厚度、不同内径的腔体,满足不同场景不同需求的应用。(3) The connection between the cavity and the end is detachable. Users can replace the cavity with different lengths, different thicknesses and different inner diameters according to the air pressure requirements and temperature requirements used to meet the needs of different scenarios and applications.
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,下面将对实施例或现有技术描述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 explain the embodiments of the present invention or the technical solutions in the prior art more clearly, the following briefly introduces the accompanying drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only These are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained according to these drawings without creative efforts.
图1为实施例的立体图。FIG. 1 is a perspective view of an embodiment.
图2为实施例的立体剖面图。FIG. 2 is a perspective cross-sectional view of the embodiment.
图3是图2上M处的放大图。FIG. 3 is an enlarged view of M in FIG. 2 .
图中,10-腔体,11-碳纤维层,12-隔热层,13-限位部,14-卡位部,15-第一法兰,16-定位凹槽,20-端头,21-第二法兰,30-卡箍,40-石棉垫片。In the figure, 10-cavity, 11-carbon fiber layer, 12-insulation layer, 13-limiting part, 14-positioning part, 15-first flange, 16-positioning groove, 20-end, 21 -Second flange, 30-clamp, 40-asbestos gasket.
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在没有作出创造性劳动前提下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, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
如图1所示,在本发明提供的实施例,一种新型的燃烧室,包括腔体10和端头20,端头20可拆卸连接于腔体10的端口。As shown in FIG. 1 , in the embodiment provided by the present invention, a novel combustion chamber includes a
如图2和图3所示,腔体10包括有碳纤维层11和隔热层12,隔热层12通过黏胶贴合于碳纤维层11的内壁。其中,碳纤维层11为一体成型,隔热层12为三元乙丙橡胶。隔热层12能够隔绝腔体10内部大部分的热量,碳纤维层11的温度不会过高,其性能能够保持稳定;碳纤维层11重量轻,抗张强度高,减少了燃烧室的重量,满足燃烧室的高压需求。As shown in FIG. 2 and FIG. 3 , the
如图2和图3所示,碳纤维层11的内壁设置有限位部13,隔热层12外壁设置有卡位部14,卡位部14和限位部13卡紧配合,限制了隔热层12的移动,提高了燃烧室的使用稳定性。其中,卡位部14和限位部13中,任意一者为凸台,另外一者为凹槽,凸台嵌入凹槽中进而卡紧配合。本实施例中,限位部13为凹槽,卡位部14位凸台。As shown in FIG. 2 and FIG. 3 , the inner wall of the
如图1~3所示,腔体10的端部设置有第一法兰15,端头20的端部设置有第二法兰21,第一法兰15和第二法兰21贴合并通过卡箍30可拆卸抱紧连接,进而使腔体10和端头20之间可拆卸连接。其中,用户使用时可根据使用的气压要求、温度要求,进而替换不同长度、不同厚度、不同内径的腔体10,满足不同场景不同需求的应用。As shown in FIGS. 1 to 3 , the end of the
如图3所示,第一法兰15和第二法兰21之间设置有石棉垫片40。第一法兰15的内侧面设置有定位凹槽16,石棉垫片40嵌入定位凹槽16内,进而实现定位。其中,石棉垫片40起到隔热和密封的作用。As shown in FIG. 3 , an
如图3所示,第一法兰15和第二法兰21的外侧面均为斜坡结构。其中,当卡箍30抱紧第一法兰15和第二法兰21时,斜波结构能够将往腔体10中心的抱紧力分解为对第一法兰15和第二法兰21的挤压力,使第一法兰15和第二法兰21贴紧密封。同时,斜坡结构能够实现对卡箍30起到导向作用,使用户把卡箍30套设在第一法兰15和第二法兰21时更加方便。As shown in FIG. 3 , the outer surfaces of the
如图3所示,第一法兰15一体成型于碳纤维层11的端部。其中,第一法兰15与碳纤维层11均为碳纤维材料,碳纤维强度高,使第一法兰15满足刚性连接的应用。As shown in FIG. 3 , the
以上所述仅为本发明的较佳实施例而已,并不用以限制本发明,凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the scope of the present invention. within the scope of protection.
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| US6151887A (en) * | 1997-07-17 | 2000-11-28 | Deutsches Zentrum Fuer Luft- Und Raumfahrt E.V. | Combustion chamber for rocket engine |
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| US20070202455A1 (en) * | 2004-08-10 | 2007-08-30 | Ibiden Co., Ltd. | Firing furnace, manufacturing method of a ceramic member using the firing furnace, ceramic member, and ceramic honeycomb filter |
| CN105864801A (en) * | 2015-02-09 | 2016-08-17 | 日本派欧尼株式会社 | Waste gas combustion type purifying device |
| CN109494677A (en) * | 2018-10-17 | 2019-03-19 | 中国航空工业集团公司洛阳电光设备研究所 | Vacuum cement is to temperature-height cable fast sealing device and encapsulating method |
| CN212511247U (en) * | 2020-09-01 | 2021-02-09 | 广东高沃科技有限公司 | Novel combustion chamber |
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2020
- 2020-09-01 CN CN202010905003.5A patent/CN112066406A/en active Pending
Patent Citations (6)
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|---|---|---|---|---|
| US6151887A (en) * | 1997-07-17 | 2000-11-28 | Deutsches Zentrum Fuer Luft- Und Raumfahrt E.V. | Combustion chamber for rocket engine |
| US20070202455A1 (en) * | 2004-08-10 | 2007-08-30 | Ibiden Co., Ltd. | Firing furnace, manufacturing method of a ceramic member using the firing furnace, ceramic member, and ceramic honeycomb filter |
| EP1795806A2 (en) * | 2005-12-06 | 2007-06-13 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Warm chamber |
| CN105864801A (en) * | 2015-02-09 | 2016-08-17 | 日本派欧尼株式会社 | Waste gas combustion type purifying device |
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