CN110979590A - Semi-automatic cabin device of dismouting of glider under water - Google Patents
Semi-automatic cabin device of dismouting of glider under water Download PDFInfo
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- CN110979590A CN110979590A CN201911350292.0A CN201911350292A CN110979590A CN 110979590 A CN110979590 A CN 110979590A CN 201911350292 A CN201911350292 A CN 201911350292A CN 110979590 A CN110979590 A CN 110979590A
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- bottom plate
- base
- worm
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Abstract
The invention discloses a semi-automatic cabin dismounting device for an underwater glider, which comprises a base, a front sliding seat bottom plate and a rear sliding seat bottom plate, wherein one end of the base is provided with a vertical plate, the vertical plate is connected with a baffle through a spring, and the base is symmetrically provided with two guide rails; a worm is fixed between the two guide rails through a worm fixing seat, the tail ends of the two guide rails are connected with a rotating wheel through a bearing and a connecting shaft, a gear is arranged on the connecting shaft, and a bevel gear meshed with the gear is arranged at the tail end of the worm; the bottom of preceding slide bottom plate and back slide bottom plate all is equipped with rail block and fixing base, and preceding slide bottom plate, back slide bottom plate pass through rail block swing joint on the guide rail, fixing base and worm swing joint, and the upper surface of preceding slide bottom plate and back slide bottom plate all is equipped with the base that is used for placing the withstand voltage cabin of glider, is equipped with buckle and lock hoop on the base.
Description
Technical Field
The invention relates to the field of underwater glider loading and unloading, in particular to a semi-automatic cabin dismounting device for an underwater glider.
Background
The existing underwater glider is developing towards a deeper and farther direction. With the continuous updating and upgrading of products, some traditional methods for assembling and testing gliders are not suitable for the current gliders.
In the development process of the glider, a large number of laboratory tests and high-pressure simulation tests are needed before formal launching, and the pressure-resistant cabin needs to be frequently disassembled and assembled in the test process. These tasks can be solved completely for a small glider by manual operation and can achieve better results. However, this operation is not suitable for a glider with a large volume and a heavy weight.
The large-depth glider requires a large submergence depth and a high pressure, and therefore, has a higher requirement for sealing performance. In the assembly process, alignment assembly needs to be strictly guaranteed, and the sealing surface cannot be scratched. However, due to the fact that the structure is large in size and heavy in weight, the task which can be completed by two persons of the small-sized glider is at least four persons for the large-depth glider, the precision of cabin loading is low by means of manual positioning in the assembling process, the sealing surface is easy to damage due to shaking, or the problems that assembling cannot be conducted and assembling is difficult due to misalignment are solved.
Disclosure of Invention
The invention aims to overcome the defects in the prior art and solve the problem of cabin dismounting and mounting of the existing glider with larger volume and heavier weight in the test process.
The purpose of the invention is realized by the following technical scheme:
a semi-automatic cabin dismounting and mounting device for an underwater glider comprises a base, a front sliding seat bottom plate and a rear sliding seat bottom plate, wherein a vertical plate is arranged at one end of the base, a baffle is connected onto the vertical plate through a spring, and two guide rails are symmetrically arranged on the base; a worm is fixed between the two guide rails through a worm fixing seat, the tail ends of the two guide rails are connected with a rotating wheel through a bearing and a connecting shaft, a gear is arranged on the connecting shaft, and a bevel gear meshed with the gear is arranged at the tail end of the worm; the bottom of preceding slide bottom plate and back slide bottom plate all is equipped with rail block and fixing base, preceding slide bottom plate, back slide bottom plate pass through rail block swing joint is on the guide rail, the fixing base with worm swing joint, the upper surface of preceding slide bottom plate and back slide bottom plate all is equipped with the base that is used for placing the withstand voltage cabin of glider, be equipped with buckle and lock hoop on the base.
Preferably, the middle parts of the two guide rails are provided with positioning sliders.
When the loading cabin, place suitable position with two slides earlier, then put two sections gliders withstand voltage cabin respectively on two slides, the adjustment is suitable, locks, then promotes the back slide, makes the withstand voltage cabin of fixing on the slide of back and baffle paste tightly, then slowly rotates the runner, and preceding slide drives another section withstand voltage cabin and is close to another section withstand voltage cabin gradually. After the two cabin bodies are aligned, the rotating wheel can be continuously rotated until the two cabin bodies are completely connected in place. When the cabin is disassembled, the positions of the two sliding seats are adjusted, the two sections of pressure-resistant cabins are respectively placed on the front sliding seat and the rear sliding seat, then the position of the rear sliding seat is fixed by the fixed sliding block, and then the rotating wheel is slowly rotated to enable the front sliding seat to drive one section of cabin body to move until the two sections of cabin bodies are completely separated.
Compared with the prior art, the technical scheme of the invention has the following beneficial effects:
1. install two bases the same with the withstand voltage cabin diameter of glider on every slide, withstand voltage cabin firmly fixed with the glider, rely on mechanical structure to guarantee the axiality precision of two sections withstand voltage cabins, it is more accurate than traditional dismouting mode of relying on eyes to observe and manual complex far away.
2. The transmission of gear and turbine worm is adopted, and the power that provides during the in-service use is far more than artifical dragging and extrusion stronger, and the problem of not opening and not installing because of the not enough dismantlement that leads to of strength during the manual disassembly and assembly is solved.
3. A spring is installed on one side of the baffle, a certain buffering effect can be achieved when the pressure-resistant cabin of the glider is assembled, hard installation is changed into soft installation, and the O-shaped ring is prevented from being broken in the installation process.
4. The glider can be assembled and disassembled only by one person, at least three persons are needed during normal manual operation, more hands are needed for the glider with larger weight and larger depth, and the minimum requirement of the production glider on the number of the persons can be obviously reduced.
5. The base design above the slide is for replacing the structure, simultaneously for the resistant cabin of glider of different diameters withstand voltage corresponding base has been designed, withstand voltage cabin through the base of changing above the slide alright dismouting different specifications of glider, furthest's satisfaction commonality.
Drawings
FIG. 1 is a structural diagram of the overall state of the present invention;
FIG. 2 is a schematic top view of the structure of FIG. 1;
FIG. 3 is a partial schematic view of the present invention;
FIG. 4 is a schematic view of a base structure according to the present invention;
FIG. 5 is a schematic view of the guide rail structure of the present invention;
FIG. 6 is a schematic view of the baffle structure of the present invention;
FIG. 7 is a schematic view of the front and rear sliding seats of the present invention;
FIG. 8 is a schematic view of the front carriage of the present invention;
FIG. 9 is a schematic view of a base structure of the present invention;
reference numerals: 1-base, 2-guide rail, 3-rear slide base plate, 4-positioning slide block, 5-front slide base plate, 6-runner, 7-glider pressure-resistant cabin, 8-baffle, 9-spring, 10-worm fixing seat, 11-worm, 12-worm fixing seat, 13-bevel gear, 14-bearing, 15-locking hoop, 16-buckle, 17-guide rail slide block, 18-worm fixing seat and 19-base.
Detailed Description
The invention is described in further detail below with reference to the figures and specific examples. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
As shown in fig. 1 to 9, the semi-automatic cabin dismounting and mounting device for an underwater glider provided by the invention comprises a base 1, a guide rail 2, a rear sliding seat bottom plate 3, a positioning slider 4, a front sliding seat bottom plate 5, a rotating wheel 6, a glider pressure-resistant cabin 7, a baffle 8, a spring 9, a worm fixing seat 10, a worm 11, a worm fixing seat 12, a bevel gear 13, a bearing 14, a locking hoop 15, a buckle 16, a guide rail slider 17, a worm fixing seat 18 and a base 19.
Wherein, the base 1, the guide rail 2, the baffle 8, the spring 9, the worm fixing seat 10, the worm 11, the worm fixing seat 12, the bevel gear 13 and the bearing 14 form a fixed structure which is used as a bearing main body and a force application main body, and the disassembly and assembly process mainly depends on the mutual matching between the rear sliding seat and the front sliding seat. The front sliding seat is composed of a front sliding seat bottom plate 5, a locking hoop 15, a buckle 16, a guide rail sliding block 17, a worm fixing seat 18 and a base 19, and the rear sliding seat is composed of a rear sliding seat bottom plate 3, a locking hoop 15, a buckle 16, a guide rail sliding block 17, a worm fixing seat 18 and a base 19. The force application main body comprises a rotating wheel 6, a worm fixing seat 10, a worm 11, a worm fixing seat 12, a bevel gear 13, a bearing 14 and the like, the rotating wheel 6 is rotated manually to drive the bevel gear 13 to rotate, the bevel gear 13 drives the worm 11, and the worm 11 drives the front sliding seat to move back and forth.
One end of the base 1 is provided with a vertical plate, the vertical plate is connected with a baffle plate 8 through a spring 9, and the base 1 is symmetrically provided with two guide rails 2; a worm 11 is fixed between the two guide rails 2 through a worm fixing seat 18, the tail ends of the two guide rails 2 are connected with a rotating wheel 6 through a bearing 14 and a connecting shaft, a gear is arranged on the connecting shaft, and a bevel gear 13 meshed with the gear is arranged at the tail end of the worm 11; the bottom of preceding slide bottom plate 5 and back slide bottom plate 3 all is equipped with guide rail slide 17 and worm fixing base 18, and preceding slide bottom plate, back slide bottom plate pass through guide rail slide 17 swing joint on guide rail 2, worm fixing base 18 and worm 11 swing joint, and the upper surface of preceding slide bottom plate and back slide bottom plate all is equipped with the base 19 that is used for placing the resistant cabin of glider, is equipped with buckle 16 and lock hoop 15 on the base 19.
When the device is used for disassembling the cabin, the positions of the front sliding seat and the rear sliding seat are firstly adjusted, and the glider can be stably put down. After the glider is put down, the position is adjusted to ensure that the front cabin and the rear cabin are respectively put on the front sliding seat and the rear sliding seat, then the glider is fixed on the base 19 by the locking hoop 15 and the buckle 16, and simultaneously the rear sliding seat bottom plate 3 is positioned by the positioning slide block 4. Then the rotating wheel 6 is slowly rotated, whether the abnormality exists is observed in the rotating process, if the abnormality occurs, the inspection is stopped, and if the abnormality occurs, the two cabins can be slowly separated. After the cabin is successfully disassembled, the buckle 16 and the locking hoop 15 are opened, and the two sections of pressure-resistant cabins are respectively taken down.
When the device is used for loading, two sliding seats are placed at proper positions, two sections of pressure-resistant cabins 7 of the glider are placed on the two sliding seats respectively, the two sections of pressure-resistant cabins are adjusted properly and locked by a buckle 16 and a locking hoop 15, then a rear sliding seat bottom plate 3 is pushed slowly, the pressure-resistant cabins fixed on the rear sliding seat bottom plate 3 are attached to a baffle plate 8, then a rotating wheel 6 is rotated slowly, and a front sliding seat bottom plate 5 drives one section of pressure-resistant cabin to gradually approach the other section of pressure-resistant cabin. After the two cabin bodies are checked to be correct and have no problem, the rotating wheel 6 can be continuously rotated until the two cabin bodies are completely aligned, then the rotating wheel 6 is slowly and reversely rotated, so that the pressure-resistant cabin 7 of the glider tightly attached to the baffle plate 8 is slowly separated, and the baffle plate 8 is prevented from popping up the pressure-resistant cabin due to sudden stress. Wherein, the spring 9 is arranged between the baffle 8 and the base 1 to prevent the pressure-resistant cabin from being damaged and scratched due to strong and hard installation, and the spring 9 can play a certain role in buffering and protecting.
The present invention is not limited to the above-described embodiments. The foregoing description of the specific embodiments is intended to describe and illustrate the technical solutions of the present invention, and the above specific embodiments are merely illustrative and not restrictive. Those skilled in the art can make many changes and modifications to the invention without departing from the spirit and scope of the invention as defined in the appended claims.
Claims (2)
1. A semi-automatic cabin dismounting and mounting device for an underwater glider is characterized by comprising a base, a front sliding seat bottom plate and a rear sliding seat bottom plate, wherein a vertical plate is arranged at one end of the base, a baffle is connected onto the vertical plate through a spring, and two guide rails are symmetrically arranged on the base; a worm is fixed between the two guide rails through a worm fixing seat, the tail ends of the two guide rails are connected with a rotating wheel through a bearing and a connecting shaft, a gear is arranged on the connecting shaft, and a bevel gear meshed with the gear is arranged at the tail end of the worm; the bottom of preceding slide bottom plate and back slide bottom plate all is equipped with rail block and fixing base, preceding slide bottom plate, back slide bottom plate pass through rail block swing joint is on the guide rail, the fixing base with worm swing joint, the upper surface of preceding slide bottom plate and back slide bottom plate all is equipped with the base that is used for placing the withstand voltage cabin of glider, be equipped with buckle and lock hoop on the base.
2. The device for semi-automatically disassembling and assembling the cabin of the underwater glider according to claim 1, wherein a positioning slide block is arranged in the middle of each of the two guide rails.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911350292.0A CN110979590A (en) | 2019-12-24 | 2019-12-24 | Semi-automatic cabin device of dismouting of glider under water |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911350292.0A CN110979590A (en) | 2019-12-24 | 2019-12-24 | Semi-automatic cabin device of dismouting of glider under water |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110979590A true CN110979590A (en) | 2020-04-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911350292.0A Pending CN110979590A (en) | 2019-12-24 | 2019-12-24 | Semi-automatic cabin device of dismouting of glider under water |
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| CN (1) | CN110979590A (en) |
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| CN107030657A (en) * | 2017-05-24 | 2017-08-11 | 马爱华 | A kind of industrial computer maintenance platform |
| CN108000135A (en) * | 2017-12-05 | 2018-05-08 | 上海交通大学 | There is the large-scale Cylinder shape constructional element automatic butt posture adjustment positioner of the coordinated movement of various economic factors |
| CN108788602A (en) * | 2018-07-06 | 2018-11-13 | 浙江海洋大学 | A kind of device that boat segmental closes up |
| CN208376833U (en) * | 2018-06-29 | 2019-01-15 | 宿迁市金板木业有限公司 | A kind of transport device of the sheet fabrication convenient for feeding |
| CN109396784A (en) * | 2018-11-07 | 2019-03-01 | 北京特种机械研究所 | A kind of bay section automatic butt jointing device |
| CN110015326A (en) * | 2019-04-29 | 2019-07-16 | 张潇 | A kind of adjustable mold haulage equipment |
| CN110216439A (en) * | 2019-07-25 | 2019-09-10 | 中国计量大学 | A kind of Autonomous Underwater Vehicle cabin assembly and docking platform |
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2019
- 2019-12-24 CN CN201911350292.0A patent/CN110979590A/en active Pending
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6126693U (en) * | 1984-07-23 | 1986-02-17 | 三井造船株式会社 | Propeller shaft insertion device |
| CN201760779U (en) * | 2010-08-27 | 2011-03-16 | 哈尔滨四海数控科技股份有限公司 | Automatic centering clamping device |
| CN103551829A (en) * | 2013-09-16 | 2014-02-05 | 天津山河装备开发有限公司 | Crane jib assembling platform |
| CN104148931A (en) * | 2014-07-04 | 2014-11-19 | 上海拓璞数控科技有限公司 | Multipoint servo adjustment device for alignment of large barrel-section member and method thereof |
| CN205342382U (en) * | 2016-01-21 | 2016-06-29 | 武汉力地液压设备有限公司 | Large -scale horizontal pneumatic cylinder removes fitting work platform device |
| CN205572310U (en) * | 2016-04-29 | 2016-09-14 | 江景涛 | Be used for telescopic equipment of cylindrical watertight and dismantle platform |
| CN107030657A (en) * | 2017-05-24 | 2017-08-11 | 马爱华 | A kind of industrial computer maintenance platform |
| CN108000135A (en) * | 2017-12-05 | 2018-05-08 | 上海交通大学 | There is the large-scale Cylinder shape constructional element automatic butt posture adjustment positioner of the coordinated movement of various economic factors |
| CN208376833U (en) * | 2018-06-29 | 2019-01-15 | 宿迁市金板木业有限公司 | A kind of transport device of the sheet fabrication convenient for feeding |
| CN108788602A (en) * | 2018-07-06 | 2018-11-13 | 浙江海洋大学 | A kind of device that boat segmental closes up |
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| CN110015326A (en) * | 2019-04-29 | 2019-07-16 | 张潇 | A kind of adjustable mold haulage equipment |
| CN110216439A (en) * | 2019-07-25 | 2019-09-10 | 中国计量大学 | A kind of Autonomous Underwater Vehicle cabin assembly and docking platform |
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Application publication date: 20200410 |
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| RJ01 | Rejection of invention patent application after publication |