CN102689752A - Side-opened package box for transporting whole satellite or satellite cabin - Google Patents
Side-opened package box for transporting whole satellite or satellite cabin Download PDFInfo
- Publication number
- CN102689752A CN102689752A CN2012101711919A CN201210171191A CN102689752A CN 102689752 A CN102689752 A CN 102689752A CN 2012101711919 A CN2012101711919 A CN 2012101711919A CN 201210171191 A CN201210171191 A CN 201210171191A CN 102689752 A CN102689752 A CN 102689752A
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- guide rail
- door
- chamber door
- casing
- retarder
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Abstract
The invention relates to a side-opened package box for transporting the whole satellite or a satellite cabin and belongs to the technical field of satellites. The package box mainly adopts a side-opened structure and comprises a box body, a box door, and a door open/shut mechanism. A guide rail A is arranged on the inner side of the box door and a guide rail B is arranged on the bottom surface of the box body. When the box door is opened, the guide rail A on the inner side of the box door and the guide rail B on the bottom surface of the box body are positioned on the same plane and can realize seamless connection through a transitional guide rail C; and after the box door is opened, a sliding trolley can freely slide on a horizontal guide rail formed by the guide rails A, B, and C. The door open/shut mechanism comprises a pulley block, a rocking handle, a reducer, and a cable wire, wherein the pulley block is mounted on the top surface of the box body, the reducer is mounted on a lateral surface of the box body, the rocking handle is mounted on the reducer, and the cable wire is connected with the reducer, the pulley block, and the box door sequentially. The invention has the advantages that no hoist is needed, the requirement on operation spaces in factory buildings is low, and the satellites can be taken into and out of the box conveniently, safely, and reliably.
Description
Technical field
The side that the present invention relates to whole star of satellite or the transportation of the single cabin packing chest that opens the door; Be used for the design of Satellite Product ground long-distance transportation packing chest; Be applicable to domestic medium-and-large-sized satellite, such as: navigation satellite, communication satellite, remote sensing satellite, lunar exploration satellite etc. belong to the satellite technology field.
Background technology
The satellite transport package box be satellite in important general assembly operate ground frock of AIT stage, be used to provide the suitable environmental conditions of satellite, ensure long-distance transportation.Transport package box have preserve moisture, insulation, pressure holding function, and can be applicable to long-distance transportation.
At present, domestic big-and-middle-sized satellite generally adopts highway and railway transportation, in the development that has restricted packing chest aspect the general assembly operational space.Traditional bell-jar packing box structure is simple, be prone to realize that advantage is to rely on the deadweight of case cover that sealing force is provided, and seals very reliably, and missile armament and most of satellite packing chest all adopt this form.Shortcoming is because top lifting can not be adopted when the space is not enough, in addition when the size of product with weight greatly the time, hoisting height that need be higher and bigger hanging device, the bell-jar structure has increased hoisting difficulty and operational risk.
Summary of the invention
The objective of the invention is the deficiency that exists in the prior art in order to solve, the side that proposes whole star of satellite or the transportation of the single cabin packing chest that opens the door, this packing chest can not use crane, requires little to the factory building operational space; The turnover case of product is simple to operate, safe, reliable; Materials used and good seal performance, suitable satellite long-distance transport.
The objective of the invention is to realize through following technical scheme.
The side of whole star of satellite of the present invention or the transportation of the single cabin packing chest that opens the door, packing chest is the side opening structure totally, comprises casing, chamber door and door opening and closing mechanism; Casing is connected through bottom hinge with chamber door; The switch of chamber door is controlled through door opening and closing mechanism; When chamber door is closed and the space that surrounds of casing is in sealing state; There is guide rail A the chamber door inboard, and guide rail B is arranged on the tank floor, and when chamber door was opened, the guide rail B in the chamber door on side rails A and the tank floor was positioned on the same horizontal surface, and can realize seamless connection through transition guide rail C; Place shipping products in the slip unwheeling, after chamber door was opened, the slip unwheeling can be free to slide on the horizontal guide rail that guide rail A, guide rail B and transition guide rail C are linked to be.
Door opening and closing mechanism comprises assembly pulley, rocking handle, retarder, reducer stent, steel rope, steel rope guard shield and retarder guard shield; Assembly pulley is installed on the end face of casing, and retarder is installed in the side of casing through reducer stent and protects through the retarder guard shield, and rocking handle is installed on the retarder; Steel rope be linked in sequence retarder, assembly pulley and chamber door, steel rope is protected through the steel rope guard shield.
Above-mentioned assembly pulley installation form is fixed pulley, installs and can make steel rope arrive the chamber door center of top from the side of casing through switching-over so that steel rope is changed direction after through assembly pulley through the assembly pulley distribution of varying number;
The reduction ratio of above-mentioned retarder was greater than 40: 1.
Beneficial effect
Packing chest of the present invention is unpacked can not use crane; Require little to the factory building operational space; The turnover case of product is simple to operate, safe, reliable, suitable satellite long-distance transport.
Different with traditional bell-jar packing chest; Packing chest is the side opening structure totally, and after door opening and closing mechanism was opened chamber door, the product that is loaded in the slip unwheeling skidded off along the guide rail on casing and chamber door plane; Can reduce the FCL hoisting height like this, strengthen the comformability of this packing chest different places.That is: in limited operational space, open the side chamber door voluntarily; Chamber door flushes with at the bottom of the case, and guide piece is set, and satellite can be released through slide rail smoothly in the case.
Description of drawings
Fig. 1 closes scheme drawing for the open the door chamber door of packing chest of side of the present invention;
Fig. 2 opens scheme drawing for the open the door chamber door of packing chest of side of the present invention;
Wherein, 1-casing, 2-chamber door, 3-hinge, 4-guide rail A, 5-guide rail B, 6-transition guide rail C, 7-assembly pulley, 8-rocking handle, 9-retarder, 10-steel rope, 11-slip unwheeling, 12-satellite.
The specific embodiment
Below in conjunction with accompanying drawing and embodiment the present invention is described further.
Embodiment
The side of the whole star of the satellite packing chest that opens the door, packing chest is the side opening structure totally, comprises casing 1, chamber door 2 and door opening and closing mechanism; Casing 1 is connected through bottom hinge 3 with chamber door 2; The switch of chamber door 2 is controlled through door opening and closing mechanism; When chamber door 2 is closed and the space that surrounds of casing 1 is in sealing state, and is as shown in Figure 1; There is guide rail A4 chamber door 2 inboards, and casing has guide rail B5 on 1 bottom surface, and when chamber door 2 was opened, the guide rail B5 in the chamber door 2 on side rails A4 and casing 1 bottom surface was positioned on the same horizontal surface, and can realize seamless connection through transition guide rail C6, and are as shown in Figure 2; The whole star of satellite places in the slip unwheeling 11, and slip unwheeling 11 can slide on the horizontal guide rail that guide rail A4, guide rail B5 and transition guide rail C6 are linked to be and skid off, and accomplishes vanning, the outlet operation of the whole star of satellite.
Door opening and closing mechanism comprises assembly pulley 7, rocking handle 8, retarder 9, reducer stent, steel rope 10, steel rope guard shield and retarder guard shield; Assembly pulley 7 is installed on the end face of casing 1, and retarder 9 is installed in the side of casing 1 through reducer stent and protects through the retarder guard shield, and rocking handle 8 is installed on the retarder 9; Steel rope 10 be linked in sequence retarder 9, assembly pulley 7 and chamber door 2, steel rope 10 is protected through the steel rope guard shield.
Above-mentioned assembly pulley 7 is 3 groups of fixed pulleys; Steel rope 10 is changed direction after through assembly pulley 7, make steel rope 10 arrive chamber door 2 center of top through switching-over from the side of casing 1.
The open the door effect of door-opening mechanism of packing chest of side is that the moment of rotation that manpower applies is converted into the used pulling force of packing chest folding.During operation, personnel's cw or conter clockwise shake rocking handle 8 and drive retarder 9 rotations, tighten up the steel rope 10 on the assembly pulley 7, close gradually or open thereby drive chamber door 2.
Guide rail A4, guide rail B5 and transition guide rail C6 are " u " type channel-section steel, are connected through pre-buried girder steel skeleton tapped bore in screw and casing 1 or the chamber door 2; Transition guide rail C6 can make centre of gration with trip shaft, the folding or expansion of guide rail A4 relatively; When the whole star of satellite need pass in and out packing chest, transition guide rail C6 launched along trip shaft, with the guide pass of guide rail A4 and guide rail B5 on same horizontal surface, other mode of operation foldable for storage.
According to the working direction of the whole star product of satellite, confirm the side opening position of packing chest chamber door 2, chamber door 2 is set is connected through hinge 3 with casing 1.Its effect is to make packing chest realize sealing, for the slip unwheeling 11 that skids off packing casing 1 service platform is provided simultaneously.During chamber door 2 switching manipulations, be the door opening and closing mechanism with casing 1 one sides, hinge is the axle rotation along the bottom to drive it.The lateral surface of chamber door 2 is equipped with 4 supporting pad pin.When chamber door 2 was opened fully, guide rail B5 and detouchable transition guide rail C6 plane kept level in medial surface guide rail A4 plane and the casing 1.
This packing chest form is applicable to all satellites and the limited workplace of other spacecraft product, especially height space.In the transportation of general module series satellite and general assembly operation, have more advantage, finish Satellite Product and packing chest one in the past and join one equipment pattern, saving lead time and development cost.Like 16 satellites of No. two first phases of the Big Dipper and the second stage of task of navigating, also may be used on space station Large Spacecraft portion assembling structure etc.
Claims (6)
1. the side of whole star of satellite or the transportation of the single cabin packing chest that opens the door is characterized in that:
Packing chest is the side opening structure totally, comprises casing (1), chamber door (2) and door opening and closing mechanism; Casing (1) is connected through bottom hinge (3) with chamber door (2); The switch of chamber door (2) is controlled through door opening and closing mechanism; Chamber door (2) and space of surrounding of casing (1) when closing is in sealing state; There is guide rail A (4) chamber door (2) inboard, and casing (1) has guide rail B (5) on the bottom surface, and when chamber door (2) when opening, interior side rails A of chamber door (2) (4) and guide rail B (5) on casing (1) bottom surface are positioned on the same horizontal surface, and can be through transition guide rail C (6) realization seamless connection; Slip unwheeling (11) is gone up and is placed shipping products, and after chamber door (2) was opened, slip unwheeling (11) can be free to slide on the horizontal guide rail that guide rail A (4), guide rail B (5) and transition guide rail C (6) are linked to be;
Door opening and closing mechanism comprises assembly pulley (7), rocking handle (8), retarder (9) and steel rope (10), and assembly pulley (7) is installed on the end face of casing (1), and retarder (9) is installed in the side of casing (1), and rocking handle (8) is installed on the retarder (9); Steel rope (10) be linked in sequence retarder (9), assembly pulley (7) and chamber door (2).
2. the side of whole star of satellite according to claim 1 or the transportation of the single cabin packing chest that opens the door; It is characterized in that: retarder (9) is installed in the side of casing (1) through reducer stent and protects through the retarder guard shield, and steel rope (10) is protected through the steel rope guard shield.
3. the side of whole star of satellite according to claim 1 or the transportation of the single cabin packing chest that opens the door, it is characterized in that: assembly pulley (7) is 3 groups of fixed pulleys; Steel rope (10) is changed direction after through assembly pulley (7), and steel rope (10) arrives chamber door (2) center of top from the side of casing (1) through switching-over.
4. the side of whole star of satellite according to claim 1 or the transportation of the single cabin packing chest that opens the door, it is characterized in that: the reduction ratio of retarder (9) was greater than 40: 1.
5. according to the side of whole star of claim 1 or 4 described satellites or the transportation of the single cabin packing chest that opens the door, it is characterized in that: retarder (9) is the worm type of reduction gearing of auto-lock function, and reduction ratio is 50: 1.
6. the side of whole star of satellite according to claim 1 or the transportation of the single cabin packing chest that opens the door; It is characterized in that: guide rail A (4), guide rail B (5) and transition guide rail C (6) are " u " type channel-section steel, and guide rail A (4) is connected through pre-buried girder steel skeleton tapped bore in screw and the chamber door (2); Guide rail B (5) is connected through pre-buried girder steel skeleton tapped bore in screw and the casing (1); Transition guide rail C (6) makes centre of gration with trip shaft, the folding or expansion of guide rail A (4) relatively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101711919A CN102689752A (en) | 2012-05-25 | 2012-05-25 | Side-opened package box for transporting whole satellite or satellite cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101711919A CN102689752A (en) | 2012-05-25 | 2012-05-25 | Side-opened package box for transporting whole satellite or satellite cabin |
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| CN102689752A true CN102689752A (en) | 2012-09-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012101711919A Pending CN102689752A (en) | 2012-05-25 | 2012-05-25 | Side-opened package box for transporting whole satellite or satellite cabin |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102897231A (en) * | 2012-11-02 | 2013-01-30 | 北京市华都峪口禽业有限责任公司 | Van for transporting hatching eggs |
| CN104085618A (en) * | 2014-06-30 | 2014-10-08 | 长兴百叶龙演出有限公司 | LED screen placing box |
| CN104443801A (en) * | 2014-11-05 | 2015-03-25 | 北京卫星环境工程研究所 | Flexible supporting system for remote sensing satellite whole-spacecraft transport |
| EP3245124A4 (en) * | 2015-01-14 | 2018-01-17 | Surma OY | A mine storage and handling unit |
| CN107600721A (en) * | 2017-09-30 | 2018-01-19 | 武汉资联虹康科技股份有限公司 | A kind of auto-manual system carrier package |
| CN109318783A (en) * | 2018-08-22 | 2019-02-12 | 艾迪森诺亚移动医院智能装备江苏有限公司 | A kind of Novel medical capsule vehicle |
| CN111746909A (en) * | 2020-07-20 | 2020-10-09 | 李小连 | Sample storage device for food detection |
| CN112591302A (en) * | 2020-11-12 | 2021-04-02 | 中船澄西船舶修造有限公司 | Burst wind tower transports frock |
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| US20050031437A1 (en) * | 2003-08-07 | 2005-02-10 | Doose Lawrence A. | Roll-off container |
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| CN201634125U (en) * | 2010-03-24 | 2010-11-17 | 中国石油集团西部钻探工程有限公司克拉玛依钻井工艺研究院 | Down hole casing valve storage and transportation ancillary all-in-one container device |
| CN201770208U (en) * | 2010-07-02 | 2011-03-23 | 河北杭萧钢构有限公司 | Conveying shelf for containers |
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| US1903633A (en) * | 1930-12-09 | 1933-04-11 | Gifford Wood Co | Gate |
| CN2632022Y (en) * | 2003-07-16 | 2004-08-11 | 扬州通利冷藏集装箱有限公司 | Cold storing container for easily loading/unloading |
| US20050031437A1 (en) * | 2003-08-07 | 2005-02-10 | Doose Lawrence A. | Roll-off container |
| CN2727103Y (en) * | 2004-08-13 | 2005-09-21 | 中国国际海运集装箱(集团)股份有限公司 | Container with discharging device |
| CN201109598Y (en) * | 2007-10-26 | 2008-09-03 | 王燕铭 | Container integrated loading-unloading device for large-scale equipments |
| CN201136746Y (en) * | 2007-11-15 | 2008-10-22 | 成都飞机工业（集团）有限责任公司 | Multifunctional service vehicle |
| CN201128579Y (en) * | 2007-12-18 | 2008-10-08 | 天津重钢机械装备有限公司 | Mobile shelf for loading and unloading goods to container |
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Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102897231A (en) * | 2012-11-02 | 2013-01-30 | 北京市华都峪口禽业有限责任公司 | Van for transporting hatching eggs |
| CN102897231B (en) * | 2012-11-02 | 2015-08-12 | 北京市华都峪口禽业有限责任公司 | The box-body truck of transport kind of egg |
| CN104085618A (en) * | 2014-06-30 | 2014-10-08 | 长兴百叶龙演出有限公司 | LED screen placing box |
| CN104085618B (en) * | 2014-06-30 | 2016-08-24 | 长兴百叶龙演出有限公司 | LED screen placing box |
| CN104443801A (en) * | 2014-11-05 | 2015-03-25 | 北京卫星环境工程研究所 | Flexible supporting system for remote sensing satellite whole-spacecraft transport |
| CN104443801B (en) * | 2014-11-05 | 2017-02-01 | 北京卫星环境工程研究所 | Flexible supporting system for remote sensing satellite whole-spacecraft transport |
| EP3245124A4 (en) * | 2015-01-14 | 2018-01-17 | Surma OY | A mine storage and handling unit |
| AU2016207935B2 (en) * | 2015-01-14 | 2020-09-24 | Surma Oy | A mine storage and handling unit |
| CN107600721A (en) * | 2017-09-30 | 2018-01-19 | 武汉资联虹康科技股份有限公司 | A kind of auto-manual system carrier package |
| CN109318783A (en) * | 2018-08-22 | 2019-02-12 | 艾迪森诺亚移动医院智能装备江苏有限公司 | A kind of Novel medical capsule vehicle |
| CN111746909A (en) * | 2020-07-20 | 2020-10-09 | 李小连 | Sample storage device for food detection |
| CN111746909B (en) * | 2020-07-20 | 2022-04-01 | 峡江县飞福科技有限公司 | Sample storage device for food detection |
| CN112591302A (en) * | 2020-11-12 | 2021-04-02 | 中船澄西船舶修造有限公司 | Burst wind tower transports frock |
| CN112591302B (en) * | 2020-11-12 | 2022-05-20 | 中船澄西船舶修造有限公司 | Burst wind tower transports frock |
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Application publication date: 20120926 |