CN108657672A - Satellite container - Google Patents
Satellite container Download PDFInfo
- Publication number
- CN108657672A CN108657672A CN201710193405.5A CN201710193405A CN108657672A CN 108657672 A CN108657672 A CN 108657672A CN 201710193405 A CN201710193405 A CN 201710193405A CN 108657672 A CN108657672 A CN 108657672A
- Authority
- CN
- China
- Prior art keywords
- case lid
- frame
- satellite
- lid
- case
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000013011 mating Effects 0.000 claims abstract description 18
- 238000007789 sealing Methods 0.000 claims description 15
- 239000002390 adhesive tape Substances 0.000 claims description 5
- 239000012530 fluid Substances 0.000 claims 1
- 239000000565 sealant Substances 0.000 claims 1
- 230000032258 transport Effects 0.000 description 31
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 238000001514 detection method Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 239000012945 sealing adhesive Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D90/00—Component parts, details or accessories for large containers
- B65D90/02—Wall construction
- B65D90/04—Linings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D90/00—Component parts, details or accessories for large containers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D90/00—Component parts, details or accessories for large containers
- B65D90/02—Wall construction
- B65D90/08—Interconnections of wall parts; Sealing means therefor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Closures For Containers (AREA)
Abstract
The invention discloses a kind of satellite transport cases, including：Bottom and case lid.Edge on the upside of the bottom is provided with mating surface, and the mating surface is plane.The case lid ordinatedly covers conjunction in the mating surface of the bottom, the space for accommodating satellite is formed between the case lid and the bottom, wherein, the side wall of the case lid is provided with U-frame, the U-frame opening upwards and the lower end for engaging the side wall in lower end, and the bottom of the U-frame connects with the bottom, wherein, the U-frame is provided with outwardly projecting flange, and the bottom is provided with bottom frame corresponding with the flange on the outside, and the flange and the bottom frame are connected by connector.Satellite transport case bottom and the case lid engagement of the present invention is close, has good air-tightness, disclosure satisfy that the transportation demand to the whole star of satellite under different condition.
Description
Technical field
The present invention relates to container technology fields, and in particular to a kind of satellite transport case.
Background technology
Satellite after finishing assembly, often there is one section of very long distance from grown place to county of emission, to make safety satellite without
It accidentally transports to launching site, there is higher requirement to satellite transport case.To adapt to the long-distance transportation and storage of different satellites
Demand meets the whole star product of satellite from general assembly factory to highway transportation, the railway transportation of long range and the wanting for air transport in transmitting target range
It asks, and ensures that satellite storage environment reaches：In the case of being filled with the high pure nitrogen of 2KPa in satellite transport cases, babinet leakage
Gas rate is not more than 600Pa/24h.A kind of satellite transport case that reliable, safety, high sealing require thus is needed to be produced to complete satellite
The storage of product and ensure Satellite Product transport reliability.
In order to solve the above problems at least partly, the present invention proposes a kind of Container Transport case.
Invention content
A series of concept of reduced forms is introduced in Summary, this will in the detailed description section into
One step is described in detail.The Summary of the present invention is not meant to attempt to limit technical solution claimed
Key feature and essential features do not mean that the protection domain for attempting to determine technical solution claimed more.
In order to solve the above problems at least partly, the invention discloses a kind of satellite transport cases, including：
Bottom, the bottom are provided with mating surface in the edge of upside, and the mating surface is plane；And
Case lid, the case lid ordinatedly cover conjunction in the mating surface of the bottom, the case lid and the bottom it
Between formed accommodate satellite space,
Wherein, the side wall of the case lid is provided with U-frame in lower end, and the U-frame opening upwards are simultaneously engaged in surrounding
The lower end of the side wall, the bottom of the U-frame are plane, and with the mating surface airtight joint of the bottom,
Wherein, the U-frame is provided with outwardly projecting flange, and the bottom is provided with corresponding with the flange on the outside
Bottom frame, the flange and the bottom frame are connected by connector.
Preferably, the bottom is provided with sealing joint strip in upside, when the case lid is closed by lid in the bottom, institute
U-frame is stated to be located above the sealing joint strip and squeeze the sealing joint strip.
Preferably, the bottom is additionally provided with adhesive tape fixed seat, and the sealing joint strip is mounted in the adhesive tape fixed seat.
Preferably, the case lid is provided with for the pressure relief opening and inflating port to the satellite transport case pressure release or inflation.
Preferably, one in the bottom and the case lid is provided with positioning pin, in the bottom and the case lid
Another is provided with location hole corresponding with the positioning pin, and when the case lid lid closes the bottom, the positioning pin passes through
The location hole realizes positioning.
Preferably, the guide rod upwardly extended is provided in the bottom, the case lid is provided with guide rod seat, when the case lid
When lid closes the bottom, the guide rod is connected to the guide rod seat.
Preferably, the bottom is provided with directive wheel in bottom.
Preferably, the bottom is provided with forklift groove in lower part.
Preferably, it is provided with lifting lug on the outside of the bottom and/or the case lid.
Preferably, the case lid is being internally provided with insulating layer.
Description of the drawings
The following drawings of embodiment of the present invention is used to understand the present invention in this as the part of the present invention.Show in attached drawing
Embodiments of the present invention and its description, principle used to explain the present invention are gone out.In the accompanying drawings,
Fig. 1 is the schematic cross-sectional view according to the satellite transport case of a preferred embodiment of the present invention；
Fig. 2 is the partial enlarged view of the part A in Fig. 1；
Fig. 3 is the schematic elevation view of the satellite transport case in Fig. 1；
Fig. 4 is the partial enlarged view of the part B in Fig. 3；
Fig. 5 is the vertical view of the bottom of the satellite transport case in Fig. 1；
Fig. 6 is the schematic elevation view of the bottom of the satellite transport case in Fig. 1；And
Fig. 7 is the schematic cross-sectional view of the bottom of the satellite transport case in Fig. 1.
Specific implementation mode
In the following description, a large amount of concrete details are given in order to provide more thorough understanding of the invention.So
And it will be apparent to one skilled in the art that embodiment of the present invention may not need it is one or more of these thin
It saves and is carried out.In other examples, in order to avoid obscuring with embodiment of the present invention, for well known in the art
Some technical characteristics are not described.
In order to thoroughly understand embodiment of the present invention, detailed structure will be proposed in following description.Obviously, of the invention
The execution of embodiment is not limited to the specific details that those skilled in the art is familiar with.
Fig. 1 to Fig. 7 schematically illustrates the satellite transport case 100 of the present invention.It is appreciated that the satellite transport of the present invention
Case 100 can be used for transporting satellite, can be used for transporting other cargos.
Satellite transport case 100 includes bottom 2 and case lid 1.Bottom 2 and case lid 1 match the collection for being assembled into hexahedron
Vanning forms the space for accommodating satellite between case lid 1 and bottom 2.Insulating layer 12 is provided on case lid 1.Certainly, do not show at other
In the embodiment gone out, bottom 2 and case lid 1 can have other shapes.
Bottom 2 is provided with mating surface in the edge of upside, and mating surface is plane.It is appreciated that the vertical view of mating surface
Figure is around the surrounding being arranged in bottom 2.Mating surface is smooth, can coordinate with case lid 1, the air-tightness in guard box body.
The side wall of case lid 1 is provided with U-frame 16 in lower end, and U-frame 16 is U-shaped, the U-shaped opening along the section perpendicular to the direction of side wall
Upwards.The side wall of case lid 1 is put into from the opening seat of U-frame 16 in U-frame 16 so that U-frame 16 connects with the lower end of side wall
It closes.
U-frame 16 is provided with outwardly projecting flange, and bottom 2 is provided with bottom frame 17 corresponding with flange on the outside, convex
Edge and bottom frame 17 are linked together by connector (being bolt 6 in present embodiment).Match with bottom 2 the bottom of U-frame 16
Conjunction face airtight joint.
In order to enable the bottom of U-frame 16 more closely connects with bottom 2, it is provided in the mating surface above bottom 2
Double sealing adhesive tape 10 and adhesive tape fixed seat 11 for installing sealing joint strip 10.When operating personnel are by 1 lid mould assembling bottom 2 of case lid
And after being fixed U-frame 16 and bottom frame 17 with bolt 6, sealing joint strip 10 is in compressive state.The upper surface of sealing joint strip 10
With 16 airtight joint of U-frame, that is to say, that in the present embodiment, the upper surface of sealing joint strip 10 is formed as being arranged in bottom 2
Mating surface.It is appreciated that in other unshowned embodiments, mating surface may be other forms, as long as can protect
The bottom airtight joint of card and U-frame 16.
The setting of U-frame 16 and sealing joint strip 10 ensure that being tightly engaged into for case lid 1 and bottom 2, to ensure satellite
Good air-tightness in transport case 100.Further, the insulating layer 12 filled in case lid 1 then may insure the constant temperature of babinet
Constant humidity.
It is appreciated that in present embodiment, the lower surface of U-frame 16 is also smooth plane, by bolt 6 by U-frame
16 and bottom frame 17 closely connect, enable to the sealing joint strip 10 being arranged on the lower surface and bottom 2 of U-frame 16 to be closely pressed together on
Together, make container 100 has very high air-tightness, provides safeguard for satellite transport.
Pressure relief opening 14 and inflating port 15 are provided on the side wall of case lid 1.When test box interior sealing or to inflated with nitrogen in case
When, it can be inflated into babinet by inflating port 15, and when needing pressure release, then pressure relief opening 14 is opened.
Bottom 2 and case lid 1 are provided with lifting lug on the outside.Specifically, the lifting lug in bottom 2 is divided into be arranged in bottom 2
Bottom lifting lug 13 at four angles, and the aviation Special lifting lug 3 in 2 side of bottom is set.Lifting lug on case lid 1 is that setting exists
The Lifting Lug 7 of 1 vertex of case lid.The setting of lifting lug facilitates the handling to satellite transport case 100.
Positioning pin 5 is provided in bottom 2.At 1 lid mould assembling bottom 2 of case lid, positioning pin 5 passes through the location hole on case lid 1, with
Just case lid 1 is limited and is oriented to during case lid 1 and the lid of bottom 2 close, so that case lid 1 and bottom 2 are quickly right
Standard is simultaneously assembled.It can be seen from figure 4 that after case lid 1 is bonded to by lid in bottom 2, positioning pin 5 is similar with bolt 6, can also play
The effect of connection.It is similar with the effect of positioning pin 5, it is additionally provided with the guide rod 4 upwardly extended in bottom 2, is provided with and leads on case lid 1
Pole socket 9, guide rod 4 pass through guide rod seat 9 to playing the role of limit and guiding to case lid 1, at the same also avoid in assembly and
The shaking of case lid 1 in subsequent transportational process.
The lower part of the surrounding of bottom 2 is provided with forklift groove 18, the prong of fork truck is facilitated to enter, thus by satellite transport case
100 lift.There are four dismountable directive wheels 8 in bottom setting for bottom 2, to facilitate the shifting of satellite transport case 100 on the ground
It is dynamic.
Present embodiment Satellite transport case 100 has Lifting Lug 7, bottom lifting lug 13, aviation Special lifting lug 3 simultaneously,
And forklift groove 18 and directive wheel 8 so that satellite transport case 100 can be moved and be transported in several ways, Ke Yitong
The means of transportation such as highway, railway and aviation are crossed to transport satellite transport case 100.It is to be understood that being not shown at other
Embodiment in, can only be arranged one or several in a variety of lifting lugs, forklift groove 18 and directive wheel 8.
The satellite transport case 100 of present embodiment is a kind of closed, heat preservation, the body structure opened up and down, can be realized
The whole star product of satellite disclosure satisfy that height of the satellite transport for box body tightness in ground storage, transhipment, transport, packaging
It is required that.Meanwhile satellite transport case 100 also can be used as the device of satellite leak detection.
Unless otherwise defined, those skilled in the art of technical and scientific term used herein and the present invention
Normally understood meaning is identical.Term used herein is intended merely to describe specifically to implement purpose, it is not intended that limitation is originally
Invention.Terms such as herein presented " settings " can both indicate that a component was attached directly to another component, also may be used
To indicate that a component is attached to another component by middleware.The feature that describes in one embodiment can be with herein
Individually or with other feature in combination be applied to another embodiment, unless this feature in the another embodiment not
It is applicable in or is otherwise noted.
The present invention is illustrated by the above embodiment, but it is to be understood that, the above embodiment is
Purpose for illustrating and illustrating, and be not intended to limit the invention within the scope of described embodiment.Art technology
Personnel are it is understood that introduction according to the present invention can also make more kinds of variants and modifications, these variants and modifications
It all falls within scope of the present invention.
Claims (10)
1. a kind of satellite transport case, which is characterized in that including：
Bottom, the bottom are provided with mating surface in the edge of upside, and the mating surface is plane；And
Case lid, the case lid ordinatedly cover conjunction in the mating surface of the bottom, shape between the case lid and the bottom
At accommodate satellite space,
Wherein, the side wall of the case lid is provided with U-frame in lower end, and the U-frame opening upwards are simultaneously engaged in described in surrounding
The lower end of side wall, the bottom of the U-frame are plane, and with the mating surface airtight joint of the bottom,
Wherein, the U-frame is provided with outwardly projecting flange, and the bottom is provided with bottom corresponding with the flange on the outside
Frame connects the flange and the bottom frame by connector.
2. satellite transport case according to claim 1, which is characterized in that the bottom is provided with sealing joint strip in upside,
When the case lid is closed by lid in the bottom, the U-frame is located above the sealing joint strip and squeezes the fluid sealant
Item.
3. satellite transport case according to claim 2, which is characterized in that the bottom is additionally provided with adhesive tape fixed seat, institute
Sealing joint strip is stated in the adhesive tape fixed seat.
4. satellite transport case according to claim 1, which is characterized in that the case lid is provided with for being transported to the satellite
The pressure relief opening and inflating port of defeated case pressure release or inflation.
5. satellite transport case according to claim 1, which is characterized in that a setting in the bottom and the case lid
There is positioning pin, another in the bottom and the case lid is provided with location hole corresponding with the positioning pin,
Wherein, when the case lid lid closes the bottom, the positioning pin passes through the location hole to realize positioning.
6. satellite transport case according to claim 1, which is characterized in that the bottom is provided with the guide rod upwardly extended,
It is provided with guide rod seat on the case lid,
Wherein, when the case lid lid closes the bottom, the guide rod is connected to the guide rod seat.
7. satellite transport case according to claim 1, which is characterized in that the bottom is provided with directive wheel in bottom.
8. satellite transport case according to claim 1, which is characterized in that the bottom is provided with forklift groove in lower part.
9. satellite transport case according to claim 1, which is characterized in that the bottom and/or the case lid are set on the outside
It is equipped with lifting lug.
10. satellite transport case according to claim 1, which is characterized in that the case lid is being internally provided with insulating layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710193405.5A CN108657672A (en) | 2017-03-28 | 2017-03-28 | Satellite container |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710193405.5A CN108657672A (en) | 2017-03-28 | 2017-03-28 | Satellite container |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108657672A true CN108657672A (en) | 2018-10-16 |
Family
ID=63785841
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710193405.5A Pending CN108657672A (en) | 2017-03-28 | 2017-03-28 | Satellite container |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108657672A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850406A (en) * | 2018-10-24 | 2019-06-07 | 芜湖中义玻璃有限公司 | A kind of bottled red packing box for transportation |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1126695A (en) * | 1955-06-22 | 1956-11-28 | Rayonne Soc Ind Pour La | Manufacturing process and assembly of lightweight isothermal plastic panels |
| GB883960A (en) * | 1959-04-27 | 1961-12-06 | Airtech Ltd | Improvements in transportable containers |
| WO1992015507A1 (en) * | 1991-03-05 | 1992-09-17 | Eurotainer Ab | Shipping container for goods sensitive of temperature |
| JP2009023711A (en) * | 2007-07-23 | 2009-02-05 | Omega:Kk | Panel structure |
| CN102774576A (en) * | 2012-07-31 | 2012-11-14 | 北京卫星环境工程研究所 | Universal transport packing case for remote sensing satellite |
| CN204280354U (en) * | 2014-11-14 | 2015-04-22 | 沈阳黎明航空发动机(集团)有限责任公司 | A kind of aero-engine anti-corrosion type packing chest |
| CN105836318A (en) * | 2016-06-03 | 2016-08-10 | 北京航天发射技术研究所 | Sealing device for transportation of aviation product and sling of sealing device |
| CN205771093U (en) * | 2016-05-24 | 2016-12-07 | 大连中集物流装备有限公司 | Guiding mechanism and there is its container |
| CN207107502U (en) * | 2017-03-28 | 2018-03-16 | 扬州通利冷藏集装箱有限公司 | Satellite transport case |
-
2017
- 2017-03-28 CN CN201710193405.5A patent/CN108657672A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1126695A (en) * | 1955-06-22 | 1956-11-28 | Rayonne Soc Ind Pour La | Manufacturing process and assembly of lightweight isothermal plastic panels |
| GB883960A (en) * | 1959-04-27 | 1961-12-06 | Airtech Ltd | Improvements in transportable containers |
| WO1992015507A1 (en) * | 1991-03-05 | 1992-09-17 | Eurotainer Ab | Shipping container for goods sensitive of temperature |
| JP2009023711A (en) * | 2007-07-23 | 2009-02-05 | Omega:Kk | Panel structure |
| CN102774576A (en) * | 2012-07-31 | 2012-11-14 | 北京卫星环境工程研究所 | Universal transport packing case for remote sensing satellite |
| CN204280354U (en) * | 2014-11-14 | 2015-04-22 | 沈阳黎明航空发动机(集团)有限责任公司 | A kind of aero-engine anti-corrosion type packing chest |
| CN205771093U (en) * | 2016-05-24 | 2016-12-07 | 大连中集物流装备有限公司 | Guiding mechanism and there is its container |
| CN105836318A (en) * | 2016-06-03 | 2016-08-10 | 北京航天发射技术研究所 | Sealing device for transportation of aviation product and sling of sealing device |
| CN207107502U (en) * | 2017-03-28 | 2018-03-16 | 扬州通利冷藏集装箱有限公司 | Satellite transport case |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850406A (en) * | 2018-10-24 | 2019-06-07 | 芜湖中义玻璃有限公司 | A kind of bottled red packing box for transportation |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information |
Address after: 225102 east side of Maqiao section, Shiqiao Town, Yangzhou Economic Development Zone, Yangzhou City, Jiangsu Province Applicant after: YANGZHOU TONGLEE REEFER CONTAINER Co.,Ltd. Applicant after: CHINA INTERNATIONAL MARINE CONTAINERS (GROUP) Ltd. Applicant after: CIMC Container (Group) Co.,Ltd. Address before: 225102 east side of Maqiao section, Shiqiao Town, Yangzhou Economic Development Zone, Yangzhou City, Jiangsu Province Applicant before: YANGZHOU TONGLEE REEFER CONTAINER Co.,Ltd. Applicant before: CHINA INTERNATIONAL MARINE CONTAINERS (GROUP) Ltd. Applicant before: CIMC CONTAINERS HOLDING Co.,Ltd. |
|
| CB02 | Change of applicant information |