CN202368795U - Temperature-regulating cabin with temperature regulation performance and buffer supporting performance - Google Patents
Temperature-regulating cabin with temperature regulation performance and buffer supporting performance Download PDFInfo
- Publication number
- CN202368795U CN202368795U CN 201120408628 CN201120408628U CN202368795U CN 202368795 U CN202368795 U CN 202368795U CN 201120408628 CN201120408628 CN 201120408628 CN 201120408628 U CN201120408628 U CN 201120408628U CN 202368795 U CN202368795 U CN 202368795U
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- cabin
- hatchcover
- cabin body
- temperature
- heat
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- Body Structure For Vehicles (AREA)
Abstract
The utility model belongs to an emission technology and in particular discloses a temperature-regulating cabin with temperature regulation performance and buffer supporting performance. The temperature-regulating cabin comprises a lower cabin body and a cabin cover, wherein an auxiliary supporting structure is arranged in the lower cabin body and comprises a supporting frame which is fixed on a connecting seat; disc spring guide rods are arranged at two ends of the supporting frame; a disc spring and a washer are sleeved outside each disc spring guide rod; and a supporting seat is arranged above the disc spring guide rods. By design of the auxiliary supporting structure, equipment in the cabin is subjected to buffer supporting, so the service life and reliability of the equipment are ensured; by design of a 6-shaped sealing strip, the temperature-regulating cabin has a function of preserving the heat of the equipment in the cabin; and furthermore, by design of a locking structure which consists of a lock head, a lock plate and an oil cylinder, the lower cabin body and the cabin cover can be self-locked, so the safety of the equipment in the cabin is ensured, and a closed state is reliable.
Description
Technical field
The utility model belongs to lift-off technology, is specifically related to a kind of heat-controlled cabin.
Background technology
Be used for the cabin body of Product transport in the past, mainly played rainproof effect, do not possess heat insulation function, not high to seal request.The form of uncapping is to uncap in both sides, has increased the link of uncapping, and has reduced reliability.In the face of seal request and the high service conditions of reliability requirement; Such work chamber can't satisfy operating needs, simultaneously, and in the lift-off technology field; Equipment component requires to be supported and to protect in storage, transportation, and can remain under certain storing temperature.Therefore, need a kind of novel heat-controlled cabin, can support, protect, have the heat-insulation and heat-preservation function below deck equipment with insulation and cushioned support performance, and have cooperate in other system regulate temperature in the cabin down, in functions such as use equipment front opening hatchcovers.
Summary of the invention
The purpose of the utility model is to provide a kind of can keep temperature in the cabin, and can open, close the heat-controlled cabin with temperature adjustment and cushioned support performance of hatchcover effectively.
The technical scheme of the utility model is following:
A kind of heat-controlled cabin with temperature adjustment and cushioned support performance; It comprises cabin body and hatchcover down; Be equipped with adapter plate on described cabin body down and the hatchcover outer wall, axis of revolution passes adapter plate, and hatchcover is connected with following cabin body; Be arranged with Connection Block in the body of cabin under described, on Connection Block, be fixed with auxiliary support structure; Described auxiliary support structure comprises the bracing frame that is fixed on the Connection Block, and the two ends of this bracing frame are provided with dish spring pilot bar, and described dish spring pilot bar is with dish spring and pad outward, and described dish spring pilot bar top is provided with bracket.
In above-mentioned heat-controlled cabin: be provided with " 6 " font sealing band on the edge of described cabin body down with temperature adjustment and cushioned support performance.
In the above-mentioned heat-controlled cabin with temperature adjustment and cushioned support performance: described latching device comprises locking cylinder and the tapered end that is fixed on the external wall in following cabin; Locking cylinder drives the tapered end telescopic moving; The outer wall of described hatchcover is provided with locking plate, and locking plate is positioned at the below of the tapered end that stretches out.
In the above-mentioned heat-controlled cabin with temperature adjustment and cushioned support performance: described latching device comprises the magnetic force lock lock body that is fixed on the following external wall in cabin, and the outer wall of described hatchcover is provided with magnetic force lock iron plate, and magnetic force lock lock body is locked iron plate magnetic with magnetic force and inhaled mutually.
The beneficial effect of the utility model is: through the design auxiliary support structure, makes below deck equipment obtain cushioned support, thereby guaranteed the service life of equipment, and reliability; Through having designed " 6 " font sealing band, make heat-controlled cabin play heat insulation function to below deck equipment; Further, through design tapered end and locking plate, and the locking mechanism formed of oil cylinder, make that down cabin body and hatchcover can self-lockings, thereby guaranteed the safety of below deck equipment, make the closure state more reliable.
Description of drawings
Fig. 1 is the heat-controlled cabin structural representation with temperature adjustment and cushioned support performance of the utility model;
Fig. 2 is the auxiliary support structure scheme drawing;
Fig. 3 is an auxiliary support structure installation site scheme drawing;
Fig. 4 is the sealing band scheme of installation;
Fig. 5 is the partial enlarged drawing at the I place in the middle of Fig. 4;
Fig. 6 is " 6 " font sealing band schematic cross-section;
Fig. 7 is locking cylinder, tapered end and locking plate scheme of installation;
Fig. 8 is magnetic force lock lock body and magnetic force lock iron plate scheme of installation;
Among the figure: 1. hatchcover; 2. descend the cabin body; 3. auxiliary support structure; 4. the oil cylinder of uncapping; 5. axis of revolution; 6. adapter plate; 7. bracing frame; 8. dish spring; 9. dish spring pilot bar; 10. pad; 11. rubber spring; 12. bracket; 13. Connection Block; " 14. 6 " font sealing band; 15. locking cylinder; 16. tapered end; 17. locking plate; 18. magnetic force lock iron plate; 19. magnetic force lock lock body.
The specific embodiment
Below in conjunction with accompanying drawing and specific embodiment the utility model is done further explain.
As shown in Figure 1, following cabin body 2 is installed together with hatchcover 1, all is processed with adapter plate 6 on following cabin body 2 and hatchcover 1 outer wall, through axis of revolution 5 is installed on adapter plate 6, makes hatchcover 1 and following cabin body 2 wraparound rotating shaft 5 to open perhaps closed.On the adapter plate 6 on hatchcover 1 outer wall, connect the oil cylinder 4 of uncapping, just can drive hatchcover 1 and open perhaps closed.The internal fixation of body 2 is equipped with auxiliary support structure 3 in following cabin.
Auxiliary support structure scheme drawing as shown in Figure 2; It comprises bracing frame 7; Two ends at bracing frame 7 are equipped with dish spring pilot bar 9 through bolt respectively, and this dish spring pilot bar 9 is with dish spring 8, and each dish also is equipped with pad 10 yellow 8 times; Rubber spring 11 is installed on the bracing frame 7, on dish spring pilot bar 9, adds a cover a bracket 12 again.
As shown in Figure 3, the stationkeeping of cabin body 2 axis is installed two Connection Blocks 13 under the inside of cabin body 2 is symmetrical in down, and above-mentioned auxiliary support structure 3 is installed in through screw retention, and on the Connection Block 13, thereby auxiliary support structure 3 is sitting at down cabin body 2 axis below.
Like Fig. 4 and shown in Figure 5, in order to let down cabin body 2 and hatchcover 1 seal closure, on following cabin body 2 and the edge that hatchcover 1 contacts " 6 " font sealing band 14 has been installed.
As shown in Figure 6, the cross sectional shape of " 6 " font sealing band is near the numeral " 6 " of traverse, and its long limit is fitted in down on the edge of cabin body 2.
As shown in Figure 7; In order to let down cabin body 2 and the hatchcover 1 can self-locking; On the outer wall of following cabin body 2 and hatchcover 1 junction, fixedly mounted locking cylinder 15, the front end of locking cylinder 15 is installed a tapered end 16, and this tapered end 5 is realized transversal stretching through the driving of locking cylinder 15.And on the outer wall of hatchcover 1, also being installed with locking plate 17, tapered end 16 is blocked in the below when this locking plate 17 just in time is positioned at tapered end 16 and stretches out.Locking cylinder 15 drive tapered ends 16 stretch out like this, and locking plate 17 retainings below tapered end 16, will be descended cabin body 2 and hatchcover 1 locking.
The utility model also provides other a kind of locking mode; As shown in Figure 8; Fixed installation magnetic force lock iron plate 18 has fixedly mounted magnetic force lock lock body 19, when the cabin body is closed on the outer wall of following cabin body 2 and hatchcover 1 junction on the edge of hatchcover 1; Magnetic force lock iron plate 18 is inhaled with magnetic force lock lock body 19 mutually, with hatchcover 1 and 2 lockings of following cabin body.
During work,, drive opening, closing of hatchcover through the oil cylinder of uncapping.Auxiliary support structure 3 is installed on down cabin body 2,, when storage, transportation, cushioned support is provided below deck equipment through auxiliary support structure 3.Airtight through in " 6 " font sealing band 14 and tapered end 16, the closed rear deck of locking plate 17 realization combining plays heat insulation function to below deck equipment.
Claims (4)
1. heat-controlled cabin with temperature adjustment and cushioned support performance; It comprises cabin body (2) and hatchcover (1) down, is equipped with adapter plate (6) on described cabin body (2) down and hatchcover (1) outer wall, and axis of revolution (5) passes adapter plate (6); Hatchcover (1) is connected with following cabin body (2); Be provided with latching device at hatchcover (1) and following cabin body (2) junction, it is characterized in that: be arranged with Connection Block (13) in the cabin body (2) under described, on Connection Block (13), be fixed with auxiliary support structure (3); Described auxiliary support structure (3) comprises the bracing frame (7) that is fixed on the Connection Block (13); The two ends of this bracing frame (7) are provided with dish spring pilot bar (9); Outer dish spring (8) and the pad (10) of being with of described dish spring pilot bar (9), described dish spring pilot bar (9) top is provided with bracket (12).
2. the heat-controlled cabin with temperature adjustment and cushioned support performance as claimed in claim 1 is characterized in that: the described edge of cabin body (2) down is provided with " 6 " font sealing band (14).
3. according to claim 1 or claim 2 heat-controlled cabin with temperature adjustment and cushioned support performance; It is characterized in that: described latching device comprises locking cylinder (15) and the tapered end (16) that is fixed on down on cabin body (2) outer wall; Locking cylinder (15) drives tapered end (16) telescopic moving; The outer wall of described hatchcover (1) is provided with locking plate (17), and locking plate (17) is positioned at the below in tapered end (16) of stretching out.
4. according to claim 1 or claim 2 heat-controlled cabin with temperature adjustment and cushioned support performance; It is characterized in that: described latching device comprises the magnetic force lock lock body (19) that is fixed on down on cabin body (2) outer wall; The outer wall of described hatchcover (1) is provided with magnetic force lock iron plate (18), and magnetic force lock lock body (19) is inhaled with magnetic force lock iron plate (18) magnetic mutually.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120408628 CN202368795U (en) | 2011-10-24 | 2011-10-24 | Temperature-regulating cabin with temperature regulation performance and buffer supporting performance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120408628 CN202368795U (en) | 2011-10-24 | 2011-10-24 | Temperature-regulating cabin with temperature regulation performance and buffer supporting performance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202368795U true CN202368795U (en) | 2012-08-08 |
Family
ID=46592510
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120408628 Expired - Fee Related CN202368795U (en) | 2011-10-24 | 2011-10-24 | Temperature-regulating cabin with temperature regulation performance and buffer supporting performance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202368795U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103786905A (en) * | 2014-01-02 | 2014-05-14 | 北京空间飞行器总体设计部 | Supporting and fastening device capable of adapting to two-way deformation of gas bottle |
| CN105485864A (en) * | 2016-02-02 | 2016-04-13 | 北京航天发射技术研究所 | Multichannel comprehensive environment regulating and control system |
| CN106394937A (en) * | 2016-09-20 | 2017-02-15 | 湖北航天技术研究院总体设计所 | Aircraft head heat container with repeatable disassembly and assembly |
| CN106586032A (en) * | 2016-11-14 | 2017-04-26 | 北京卫星环境工程研究所 | Method for adjusting equipment mounting accuracy under cabin closing state of spacecraft |
| CN114630548A (en) * | 2020-12-10 | 2022-06-14 | 中国科学院沈阳自动化研究所 | Internal locking heat conduction frame body of small cabin and installation method |
-
2011
- 2011-10-24 CN CN 201120408628 patent/CN202368795U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103786905A (en) * | 2014-01-02 | 2014-05-14 | 北京空间飞行器总体设计部 | Supporting and fastening device capable of adapting to two-way deformation of gas bottle |
| CN103786905B (en) * | 2014-01-02 | 2015-06-10 | 北京空间飞行器总体设计部 | Supporting and fastening device capable of adapting to two-way deformation of gas bottle |
| CN105485864A (en) * | 2016-02-02 | 2016-04-13 | 北京航天发射技术研究所 | Multichannel comprehensive environment regulating and control system |
| CN105485864B (en) * | 2016-02-02 | 2019-01-25 | 北京航天发射技术研究所 | A kind of multipath environment comprehensive regulation system |
| CN106394937A (en) * | 2016-09-20 | 2017-02-15 | 湖北航天技术研究院总体设计所 | Aircraft head heat container with repeatable disassembly and assembly |
| CN106394937B (en) * | 2016-09-20 | 2019-01-01 | 湖北航天技术研究院总体设计所 | A kind of Vehicle nose's insulated hold of repeatable disassembly assembling |
| CN106586032A (en) * | 2016-11-14 | 2017-04-26 | 北京卫星环境工程研究所 | Method for adjusting equipment mounting accuracy under cabin closing state of spacecraft |
| CN114630548A (en) * | 2020-12-10 | 2022-06-14 | 中国科学院沈阳自动化研究所 | Internal locking heat conduction frame body of small cabin and installation method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120808 Termination date: 20201024 |