CN107997904A - The split type cabin of ring flange connection - Google Patents
The split type cabin of ring flange connection Download PDFInfo
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- CN107997904A CN107997904A CN201810048323.6A CN201810048323A CN107997904A CN 107997904 A CN107997904 A CN 107997904A CN 201810048323 A CN201810048323 A CN 201810048323A CN 107997904 A CN107997904 A CN 107997904A
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- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61G—TRANSPORT, PERSONAL CONVEYANCES, OR ACCOMMODATION SPECIALLY ADAPTED FOR PATIENTS OR DISABLED PERSONS; OPERATING TABLES OR CHAIRS; CHAIRS FOR DENTISTRY; FUNERAL DEVICES
- A61G10/00—Treatment rooms or enclosures for medical purposes
- A61G10/02—Treatment rooms or enclosures for medical purposes with artificial climate; with means to maintain a desired pressure, e.g. for germ-free rooms
- A61G10/023—Rooms for the treatment of patients at over- or under-pressure or at a variable pressure
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Abstract
本发明提供了法兰盘连接的分体式舱，包括前舱体、后舱体和舱体集成组合，所述舱体集成组合一端与前舱体固定连接，舱体集成组合另一端与后舱体固定连接，所述舱体集成组合包括若干首尾依次连接的连接舱体，所述前舱体与舱体集成组合一端的连接舱体相连接，后舱体与舱体集成组合另一端的连接舱体相连接，该发明使用连接舱将若干舱体连接在一起，连接舱与舱体可拆卸连接设置，该设计方便舱体的运输、搬运、储藏以及使用的灵活度，减小占地空间并根据现场空间合理组合使用，该分体式舱拆卸安装简单，密封性好。另外，此发明还可将舱体分段批量生产，这样可以更好的完善生产工艺，提高生产质量。
The invention provides a split cabin connected by a flange, comprising a front cabin body, a rear cabin body and a cabin integration combination, one end of the cabin integration combination is fixedly connected to the front cabin body, and the other end of the cabin integration combination is connected to the rear cabin The cabin body is fixedly connected, and the cabin body integration combination includes several connecting cabin bodies connected head to tail in sequence, the front cabin body is connected with the connecting cabin body at one end of the cabin body integration combination, and the rear cabin body is connected with the other end of the cabin body integration combination The cabins are connected. The invention uses a connecting cabin to connect several cabins together. The connecting cabin and the cabins are detachably connected. This design facilitates the flexibility of the transportation, handling, storage and use of the cabins, and reduces the occupied space. And it can be reasonably combined and used according to the site space. The split cabin is easy to disassemble and install, and has good sealing performance. In addition, this invention can also mass-produce the cabin body in sections, so that the production process can be better improved and the production quality can be improved.
Description
技术领域technical field
本发明涉及氧舱制备和使用的技术领域。The invention relates to the technical field of oxygen chamber preparation and use.
具体地说，是涉及一种用于医疗和保健领域的分体式舱。In particular, it relates to a split cabin for the medical and health care field.
背景技术Background technique
高压舱包括医用高压氧舱和保健舱等，目前市面上的氧舱或者保健舱由于体积大、重量重的原因，导致运输、装卸、移动、使用灵活程度等方面受到严重制约，从而造成了使用上的局限性。Hyperbaric chambers include medical hyperbaric oxygen chambers and health care chambers. Due to their large size and heavy weight, the oxygen chambers or health care chambers currently on the market are severely restricted in terms of transportation, loading and unloading, movement, and flexibility in use. on the limitations.
发明内容Contents of the invention
本发明的目的在于克服上述传统技术的不足之处，提供一种通过多个舱舱体分段进行拼接的法兰盘连接的分体式舱，运输过程中将舱拆分运输，到达目的地后重新进行拼接。The purpose of the present invention is to overcome the shortcomings of the above-mentioned traditional technology, to provide a split cabin connected by a flange connected by a plurality of cabin body segments, the cabin is disassembled and transported during transportation, and after arriving at the destination Re-stitch.
本发明的目的是通过以下技术措施来达到的：法兰盘连接的分体式舱，包括前舱体、后舱体和舱体集成组合，其特征在于：所述舱体集成组合一端与前舱体固定连接，舱体集成组合另一端与后舱体固定连接，所述舱体集成组合包括若干首尾依次连接的连接舱体，所述前舱体与舱体集成组合一端的连接舱体相连接，后舱体与舱体集成组合另一端的连接舱体相连接，所述前舱体与连接舱体相连接的一端、后舱体与连接舱体相连接的一端以及连接舱体两端均固定连接有连接法兰盘，所述连接法兰盘上设有连接通道，所述连接通道周向设有若干连接孔，所述连接法兰盘一端设有螺栓，螺栓穿过两个相邻的连接法兰盘上的连接孔，螺栓配合有螺母，螺栓与螺母将两个相邻的连接法兰盘固定。The object of the present invention is achieved through the following technical measures: a split cabin connected by a flange, including a front cabin body, a rear cabin body and a cabin body integrated combination, which is characterized in that: one end of the cabin integration combination is connected to the front cabin The other end of the cabin integration combination is fixedly connected to the rear cabin body. The cabin integration combination includes several connecting cabins connected head to tail in sequence, and the front cabin is connected to the connection cabin at one end of the cabin integration combination. , the rear cabin is connected to the connecting cabin at the other end of the cabin integration combination, the end of the front cabin connected to the connecting cabin, the end connected to the rear cabin and the connecting cabin, and the two ends of the connecting cabin are all A connecting flange is fixedly connected, and a connecting channel is provided on the connecting flange, and a number of connecting holes are provided in the circumferential direction of the connecting channel, and a bolt is provided at one end of the connecting flange, and the bolt passes through two adjacent connecting channels. In the connecting holes on the flanges, the bolts are fitted with nuts, and the bolts and the nuts fix two adjacent connecting flanges.
作为上述技术方案的一种改进：所述前舱体远离连接法兰盘的一端设有前端盖，所述前端盖包括两层前端板，两层前端板之间设有前加强筋，所述前加强筋交叉设置。As an improvement of the above technical solution: the end of the front cabin body away from the connecting flange is provided with a front cover, the front cover includes two layers of front end plates, and a front reinforcing rib is arranged between the two layers of front end plates. Front rib cross setting.
作为上述技术方案的一种改进：所述前端盖上设有进舱通道，进舱通道穿过两层前端板，进舱通道上设有舱门。As an improvement of the above technical solution: the front end cover is provided with a cabin entry channel, the cabin entry channel passes through two layers of front end plates, and a cabin door is provided on the cabin entry channel.
作为上述技术方案的一种改进：所述舱门包括两层门板，所述两层门板之间设有舱门加强筋，所述舱门加强筋交叉设置。As an improvement of the above technical solution: the hatch includes two layers of door panels, a hatch door reinforcing rib is provided between the two layers of door panels, and the hatch door reinforcing ribs are intersected.
作为上述技术方案的一种改进：所述舱门外侧设有舱门把手，舱门把手设置在门板上。As an improvement of the above technical solution: a door handle is provided on the outside of the door, and the door handle is arranged on the door panel.
作为上述技术方案的一种改进：所述后舱体远离连接法兰盘的一端设有后端盖，所述后端盖包括两层后端板，两层后端板之间设有后加强筋，所述后加强筋交叉设置。As an improvement of the above technical solution: the end of the rear cabin body away from the connecting flange is provided with a rear end cover, the rear end cover includes two layers of rear end plates, and a rear reinforcement is provided between the two layers of rear end plates Ribs, the rear reinforcing ribs are arranged crosswise.
作为上述技术方案的一种改进：所述前舱体、连接舱体和后舱体内均设有若干舱体加强筋，舱体加强筋沿着前舱体、连接舱体和后舱体内壁平行设置，舱体加强筋固定设置在前舱体、连接舱体和后舱体内壁上。As an improvement of the above technical solution: the front cabin body, the connecting cabin body and the rear cabin body are all provided with several cabin reinforcement ribs, and the cabin body reinforcement ribs are parallel to the inner walls of the front cabin body, the connection cabin body and the rear cabin body. Arrangement, the cabin body stiffener is fixedly arranged on the front cabin body, the connecting cabin body and the rear cabin inner wall.
作为上述技术方案的一种改进：所述相邻的两个连接法兰盘之间设有密封条。As an improvement of the above technical solution: a sealing strip is provided between the two adjacent connecting flanges.
作为上述技术方案的一种改进：所述密封条沿着连接法兰盘的外周设置，并且螺栓穿过密封条。As an improvement of the above technical solution: the sealing strip is arranged along the outer periphery of the connecting flange, and the bolts pass through the sealing strip.
作为上述技术方案的一种改进：所述连接通道与加舱体强筋组成的形状相同，连接通道与舱体加强筋内部设有内固定板。As an improvement of the above technical solution: the shape of the connecting channel and the reinforcing rib of the cabin body is the same, and an internal fixing plate is provided inside the connecting channel and the reinforcing rib of the cabin body.
由于采用了上述技术方案，与现有技术相比，本发明的优点是：该发明使用连接舱将若干舱体连接在一起，连接舱与舱体可拆卸连接设置，该设计方便舱体的运输、搬运、储藏以及使用的灵活度，减小占地空间并根据现场空间合理组合使用，该分体式舱拆卸安装简单，密封性好。另外，此发明还可将舱体分段批量生产，这样可以更好的完善生产工艺，提高生产质量。Due to the adoption of the above technical solution, compared with the prior art, the present invention has the advantages that: the invention uses a connecting cabin to connect several cabins together, and the connecting cabin and the cabins are detachably connected, and the design facilitates the transportation of the cabins , transportation, storage and use flexibility, reduce the floor space and use it in a reasonable combination according to the site space. The split cabin is easy to disassemble and install, and has good sealing performance. In addition, this invention can also mass-produce the cabin body in sections, so that the production process can be better improved and the production quality can be improved.
下面结合附图和具体实施方式对本发明作进一步说明。The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.
附图说明Description of drawings
附图1是本发明法兰盘连接的分体式舱的立体图。Accompanying drawing 1 is the perspective view of the split cabin connected by the flange of the present invention.
附图2是图1的局部放大图。Accompanying drawing 2 is the partial enlarged view of Fig. 1.
附图3是本发明前封头的结构示意图。Accompanying drawing 3 is the structural representation of the front head of the present invention.
附图4是本发明前端盖与前舱体的剖视图。Accompanying drawing 4 is the sectional view of front end cover and front cabin body of the present invention.
附图5是本发明后端盖的结构示意图。Accompanying drawing 5 is the structure diagram of rear end cover of the present invention.
附图6是本发明后舱体的剖视图。Accompanying drawing 6 is the sectional view of rear cabin body of the present invention.
附图7是本发明连接舱体的剖视图。Accompanying drawing 7 is the cross-sectional view of the connecting cabin body of the present invention.
附图8是本发明连接法兰盘的结构示意图。Accompanying drawing 8 is the structure diagram of connecting flange of the present invention.
具体实施方式Detailed ways
实施例：如附图1-8所示，法兰盘连接的分体式舱，包括前舱体14、后舱体16和舱体集成组合，所述舱体集成组合一端与前舱体14固定连接，舱体集成组合另一端与后舱体16固定连接，所述舱体集成组合包括若干首尾依次连接的连接舱体15，所述前舱体14与舱体集成组合一端的连接舱体15相连接，后舱体16与舱体集成组合另一端的连接舱体15相连接，所述前舱体14与连接舱体15相连接的一端、后舱体16与连接舱体15相连接的一端以及连接舱体15两端均固定连接有连接法兰盘9，连接法兰盘9与其相连接的连接舱体15、前舱体14、后舱体16采用焊接的方式连接在一起。Embodiment: As shown in accompanying drawings 1-8, the split cabin connected by the flange includes the front cabin body 14, the rear cabin body 16 and the cabin body integrated combination, and one end of the cabin body integrated combination is fixed with the front cabin body 14 Connection, the other end of the cabin body integration combination is fixedly connected with the rear cabin body 16, and the cabin body integration combination includes several connecting cabin bodies 15 connected head to tail in sequence, and the connecting cabin body 15 at one end of the front cabin body 14 and the cabin body integration combination connected, the rear cabin body 16 is connected with the connecting cabin body 15 at the other end of the cabin body integration combination, the front cabin body 14 is connected with the connecting cabin body 15, the rear cabin body 16 is connected with the connecting cabin body 15 One end and both ends of the connecting cabin body 15 are fixedly connected with a connecting flange 9, and the connecting flange 9 is connected to the connecting cabin body 15, the front cabin body 14, and the rear cabin body 16 by welding.
所述连接法兰盘9上设有连接通道12，所述连接通道12周向设有若干连接孔10，连接孔10均匀排列在连接通道12的周向上，所述连接孔10设有28个，所述连接法兰盘9一端设有螺栓，螺栓穿过两个相邻的连接法兰盘9上的连接孔10，螺栓配合有螺母，螺栓与螺母将两个相邻的连接法兰盘9固定，所述前舱体14与相连接的连接舱体15上的连接法兰盘9通过上述连接方式将前舱体14与连接舱体15连接在一起，后舱体16与相连接的连接舱体15上的连接法兰盘9通过上述连接方式将后舱体16与连接舱体15连接在一起，两个相连接的连接舱体15上的连接法兰盘9通过上述连接方式将两个连接舱体15相连接。The connecting flange 9 is provided with a connecting channel 12, the connecting channel 12 is provided with several connecting holes 10 in the circumferential direction, the connecting holes 10 are evenly arranged in the circumferential direction of the connecting channel 12, and the connecting holes 10 are provided with 28. One end of the connecting flange 9 is provided with a bolt, the bolt passes through the connecting holes 10 on the two adjacent connecting flanges 9, the bolt is fitted with a nut, and the bolt and the nut fix the two adjacent connecting flanges 9 , the front cabin body 14 is connected with the connecting flange 9 on the connecting cabin body 15 through the above-mentioned connection method to connect the front cabin body 14 and the connecting cabin body 15 together, and the rear cabin body 16 is connected with the connecting cabin body The connection flange 9 on the body 15 connects the rear cabin body 16 and the connection cabin body 15 through the above-mentioned connection method, and the connection flange 9 on the two connected connection cabin bodies 15 connects the two through the above-mentioned connection method. The connecting cabin body 15 is connected.
所述前舱体14远离连接法兰盘9的一端设有前端盖，所述前端盖包括两层前端板1，两层前端板1之间设有前加强筋5，所述前加强筋5交叉设置，所述前加强筋5包括横向设置的前加强筋5和纵向设置的前加强筋5。The front cabin body 14 is provided with a front end cover away from the end of the connecting flange 9, and the front end cover includes two layers of front end plates 1, and a front reinforcing rib 5 is arranged between the two layers of front end plates 1, and the front reinforcing rib 5 Arranged crosswise, the front reinforcement ribs 5 include front reinforcement ribs 5 arranged transversely and front reinforcement ribs 5 arranged longitudinally.
所述前端盖上设有进舱通道2，进舱通道2穿过两层前端板1，进舱通道2上设有舱门，所述舱门包括两层门板3，所述两层门板3之间设有舱门加强筋7，所述舱门加强筋7交叉设置，所述舱门加强筋7包括横向设置的舱门加强筋7和纵向设置的舱门加强筋7，所述舱门外侧设有舱门把手4，舱门把手4设置在门板3上。The front end cover is provided with a cabin entry channel 2, and the cabin entry channel 2 passes through two layers of front end panels 1. The cabin entry channel 2 is provided with a hatch, and the hatch includes two layers of door panels 3, and the two layers of door panels 3 Door reinforcement ribs 7 are provided between them, and the hatch door reinforcement ribs 7 are arranged crosswise. A hatch handle 4 is provided on the outside, and the hatch handle 4 is arranged on the door panel 3 .
所述后舱体16远离连接法兰盘9的一端设有后端盖，后端盖上设有输氧孔18，所述后端盖包括两层后端板11，输氧孔18穿过两层后短板11，两层后端板11之间设有后加强筋13，所述后加强筋13交叉设置，所述后加强筋13包括横向设置的后加强筋13和纵向设置的后加强筋13。The end of the rear cabin body 16 away from the connecting flange 9 is provided with a rear end cover, and the rear end cover is provided with an oxygen delivery hole 18. The rear end cover includes two layers of rear end plates 11, and the oxygen delivery hole 18 passes through the two layers. After the short plate 11, a rear reinforcing rib 13 is arranged between the two layers of rear end plates 11, and the rear reinforcing rib 13 is intersected. 13.
所述前舱体14、连接舱体15和后舱体16内均设有若干舱体加强筋8，舱体加强筋8沿着前舱体14、连接舱体15和后舱体16内壁平行设置，舱体加强筋8固定设置在前舱体14、连接舱体15和后舱体16内壁上，舱体加强筋8与舱体加强筋8之间的距离相等。The front cabin body 14, the connecting cabin body 15 and the rear cabin body 16 are all provided with some cabin body reinforcement ribs 8, and the cabin body reinforcement ribs 8 are parallel to the front cabin body 14, the connection cabin body 15 and the rear cabin body 16 inner walls. Arrangement, the cabin body reinforcing rib 8 is fixedly arranged on the front cabin body 14, the connecting cabin body 15 and the rear cabin body 16 inner walls, and the distance between the cabin body reinforcing rib 8 and the cabin body reinforcing rib 8 is equal.
所述相邻的两个连接法兰盘9之间设有密封条6，所述密封条6沿着连接法兰盘9的外周设置，并且螺栓穿过密封条6。A sealing strip 6 is provided between the two adjacent connecting flanges 9 , the sealing strip 6 is arranged along the outer circumference of the connecting flange 9 , and the bolts pass through the sealing strip 6 .
所述连接通道12与舱体加强筋8组成的形状相同，连接通道12与舱体加强筋8内部设有内固定板17，内固定板17通过螺钉固定设置在舱体加强筋8上。内固定板17依次首尾连接设置在舱体加强筋8与连接通道12构成的内壁上。The shape of the connecting channel 12 and the cabin reinforcing rib 8 is the same, the connecting channel 12 and the cabin reinforcing rib 8 are provided with an internal fixing plate 17, and the internal fixing plate 17 is fixed on the cabin reinforcing rib 8 by screws. The inner fixing plate 17 is arranged on the inner wall formed by the cabin reinforcing rib 8 and the connecting channel 12 sequentially end to end.
Claims (10)
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| CN201810048323.6A CN107997904A (en) | 2018-01-18 | 2018-01-18 | The split type cabin of ring flange connection |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110613570A (en) * | 2019-11-01 | 2019-12-27 | 烟台宏远氧业股份有限公司 | Combined air pressurization cabin system |
| CN110638596A (en) * | 2019-11-01 | 2020-01-03 | 烟台宏远氧业股份有限公司 | Modular assembled air supercharging device and system |
| CN110652412A (en) * | 2019-11-01 | 2020-01-07 | 烟台宏远氧业股份有限公司 | Cabin body structure of air pressurization cabin |
| CN114848337A (en) * | 2022-03-08 | 2022-08-05 | 上海谦尔泰技术开发有限公司 | A kind of oxygen cabin body which is convenient to transport and assemble and its construction method |
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| CN114848337A (en) * | 2022-03-08 | 2022-08-05 | 上海谦尔泰技术开发有限公司 | A kind of oxygen cabin body which is convenient to transport and assemble and its construction method |
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