CN112537633A - Automatic device of reprinting of spacecraft thermal control multilayer - Google Patents

Automatic device of reprinting of spacecraft thermal control multilayer Download PDF

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Publication number
CN112537633A
CN112537633A CN202011418313.0A CN202011418313A CN112537633A CN 112537633 A CN112537633 A CN 112537633A CN 202011418313 A CN202011418313 A CN 202011418313A CN 112537633 A CN112537633 A CN 112537633A
Authority
CN
China
Prior art keywords
chain
chain wheel
connecting frame
thermal control
pair
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
Application number
CN202011418313.0A
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Chinese (zh)
Inventor
王哲
傅浩
范子琦
彭鹤
周众鑫
于洋
戎建臣
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beijing Institute of Spacecraft Environment Engineering
Original Assignee
Beijing Institute of Spacecraft Environment Engineering
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Beijing Institute of Spacecraft Environment Engineering filed Critical Beijing Institute of Spacecraft Environment Engineering
Priority to CN202011418313.0A priority Critical patent/CN112537633A/en
Publication of CN112537633A publication Critical patent/CN112537633A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65GTRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
    • B65G47/00Article or material-handling devices associated with conveyors; Methods employing such devices
    • B65G47/74Feeding, transfer, or discharging devices of particular kinds or types
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65GTRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
    • B65G47/00Article or material-handling devices associated with conveyors; Methods employing such devices
    • B65G47/74Feeding, transfer, or discharging devices of particular kinds or types
    • B65G47/90Devices for picking-up and depositing articles or materials

Abstract

The application provides a spacecraft thermal control multilayer automatic transfer device which comprises a connecting frame, wherein a pair of transmission mechanisms are arranged on two sides of the connecting frame, and a clamping mechanism is connected between the pair of transmission mechanisms; the transmission mechanism comprises a driving motor, a chain wheel and a chain, a driving chain wheel and a driven chain wheel are respectively arranged at two ends of one side of the corresponding connecting frame, the chain is meshed and connected between the driving chain wheel and the driven chain wheel, and an output shaft of the driving motor is connected with the driving chain wheel; the driving motors of the pair of transmission mechanisms work synchronously; the clamping mechanism comprises a connecting rod and a plurality of fixing clamps for clamping materials, the two ends of the connecting rod are fixedly connected to a pair of chains, and the fixing clamps are arranged on the connecting rod at equal intervals. The beneficial effect of this application is: through fixation clamp centre gripping thermal control multilayer, it is rotatory to drive the sprocket through driving motor for the chain with sprocket meshing is around connecting the frame transmission, thereby realizes the automatic transmission reprint of thermal control multilayer, and reprint efficiency is higher.

Description

Automatic device of reprinting of spacecraft thermal control multilayer
Technical Field
The utility model relates to a spacecraft thermal control multilayer reprints transportation technical field, concretely relates to spacecraft thermal control multilayer automatic reprinting device.
Background
The thermal control multilayer is a flexible product on the spacecraft and is arranged on the surfaces of the spacecraft and equipment, and the quality of the thermal control multilayer directly influences the temperature control and on-orbit operation effects of the spacecraft. In the face of the development of various complex spacecrafts, the quantity and difficulty of manufacturing thermal control multilayer represented by a space complex curved surface are continuously increased. Under traditional multilayer mode of making, cut out the multilayer and need two at least people with multilayer material core, level and smooth the laying on the cutting bed, lay the precision not high, consume time long.
In order to solve the problems, a spacecraft thermal control multilayer automatic transfer research is developed, a spacecraft thermal control multilayer automatic transfer device is developed, the multilayer is quickly and automatically transferred from a seam paving all-in-one machine to multi-function cutting equipment in the process of manufacturing the spacecraft thermal control multilayer, the problems of inaccurate positioning and low transfer efficiency in the process of transferring the thermal control multilayer are solved, and a foundation guarantee is provided for automatic production of the thermal control multilayer.
Disclosure of Invention
The purpose of this application is to provide a device is carried in automatic reprinting of spacecraft thermal control multilayer to above problem.
In a first aspect, the application provides a spacecraft thermal control multilayer automatic transfer device, which comprises a connecting frame, wherein a pair of transmission mechanisms are arranged on two sides of the connecting frame, and a clamping mechanism is connected between the pair of transmission mechanisms; the transmission mechanism comprises a driving motor, a chain wheel and a chain, a driving chain wheel and a driven chain wheel are respectively arranged at two ends of one side of the corresponding connecting frame, the chain is meshed and connected between the driving chain wheel and the driven chain wheel, and an output shaft of the driving motor is connected with the driving chain wheel; the driving motors of the pair of transmission mechanisms work synchronously; the clamping mechanism comprises a connecting rod and a plurality of fixing clamps for clamping materials, two ends of the connecting rod are fixedly connected to the pair of chains, and the fixing clamps are arranged on the connecting rod at equal intervals.
According to the technical scheme provided by the embodiment of the application, the lower part of the connecting frame corresponds to the chain is provided with a plurality of auxiliary tugs, and the auxiliary tugs support and transmit the chain below the connecting frame and are connected with the chain in a meshed mode.
According to the technical scheme that this application embodiment provided, the top of connecting frame corresponds the chain sets up supplementary rail that drags, supplementary transmission direction along the chain that drags the rail sets up, supplementary rail setting that drags is in the bottom of the chain of transmission in the connecting frame top, the transmission is at the surface transmission of supplementary rail that drags of chain in the connecting frame top.
The invention has the beneficial effects that: the application provides an automatic reprint device of spacecraft thermal control multilayer, through the hot accuse multilayer of fixation clamp centre gripping of clamping mechanism, it is rotatory to drive the sprocket through driving motor for the chain with the sprocket meshing is around the linking frame transmission, makes the clamping mechanism who fixes on the chain transmit between the linking frame, thereby realizes the automatic transmission reprint of hot accuse multilayer, and reprint efficiency is higher, and the reprint in-process location is accurate.
Drawings
FIG. 1 is a schematic front view of a first embodiment of the present application;
FIG. 2 is a schematic top view of a first embodiment of the present application;
FIG. 3 is a schematic structural view of a clamping mechanism according to a first embodiment of the present application;
the text labels in the figures are represented as: 1. a sprocket; 2. a drive motor; 3. a connecting frame; 4. an auxiliary tug; 5. auxiliary dragging rails; 6. a clamping mechanism; 7. a chain; 8. a connecting rod; 9. a fixing clip; 10. thermally controlled multilayers.
Detailed Description
In order that those skilled in the art will better understand the technical solutions of the present invention, the following detailed description of the present invention is provided in conjunction with the accompanying drawings, and the description of the present section is only exemplary and explanatory, and should not be construed as limiting the scope of the present invention in any way.
As shown in fig. 1 and fig. 2, a schematic diagram of a first embodiment of the present application includes a connecting frame 3, a pair of transmission mechanisms is disposed on two sides of the connecting frame 3, and a clamping mechanism 6 is connected between the pair of transmission mechanisms; the transmission mechanism comprises a driving motor 2, a chain wheel 1 and a chain 7, a driving chain wheel 1 and a driven chain wheel 1 are respectively arranged at two ends of one side corresponding to the connecting frame 3, the chain 7 is meshed and connected between the driving chain wheel 1 and the driven chain wheel 1, and an output shaft of the driving motor 2 is connected with the driving chain wheel 1; the driving motors 2 of the pair of transmission mechanisms work synchronously; as shown in fig. 3, the clamping mechanism 6 includes a connecting rod 8 and a plurality of fixing clips 9 for clamping the material, two ends of the connecting rod 8 are fixedly connected to the pair of chains 7, and the fixing clips 9 are uniformly arranged on the connecting rod 8 at intervals.
In this embodiment, the connecting frame 3 is formed into an integral structure by sectional material splicing. Driving motor 2 is connected with sprocket 1, and driving sprocket 1 is rotatory for the chain 7 meshing transmission of connection between driving sprocket 1 and driven sprocket 1, because thermal-control multilayer 10 clamping is on fixation clamp 9, and the both ends of connecting rod 8 are connected on a pair of chain 7, consequently realize that thermal-control multilayer 10 automatic transfer, reprint on linking frame 3, reprint efficiency is higher, positioning accuracy is high.
In a preferred embodiment, a plurality of auxiliary tugs 4 are arranged below the connecting frame 3 corresponding to the chains 7, and the auxiliary tugs 4 support the chains 7 which are transmitted below the connecting frame 3 and are in meshed connection with the chains 7. In the preferred embodiment, the frame of the connecting frame 3 is provided with a plurality of auxiliary tow wheels 4 downwards, so that the auxiliary tow wheels 4 are abutted to the upper side of the chain 7 transmitted to the lower side of the frame of the connecting frame 3, and are used for assisting the chain 7 to move stably, thereby preventing the chain 7 from derailing in the transmission process and influencing the transmission of the thermal control multilayer 10.
In a preferred embodiment, an auxiliary dragging rail 5 is arranged above the connecting frame 3 corresponding to the chain 7, the auxiliary dragging rail 5 is arranged along the conveying direction of the chain 7, the auxiliary dragging rail 5 is arranged at the bottom of the chain 7 conveyed above the connecting frame 3, and the chain 7 conveyed above the connecting frame 3 is conveyed on the surface of the auxiliary dragging rail 5. In the preferred embodiment, the auxiliary dragging rail 5 is arranged above the frame of the connecting frame 3, so that the chain 7 transmitted to the upper side of the frame of the connecting frame 3 is transmitted on the surface of the auxiliary dragging rail 5, and further, a guiding effect is provided for the transmission of the chain 7, and the working stability of the transmission mechanism is ensured.
The principles and embodiments of the present application are explained herein using specific examples, which are presented only to assist in understanding the method and its core concepts of the present application. The foregoing is only a preferred embodiment of the present application, and it should be noted that there are objectively infinite specific structures due to the limited character expressions, and it will be apparent to those skilled in the art that a plurality of modifications, decorations or changes may be made without departing from the principle of the present application, and the technical features described above may be combined in a suitable manner; such modifications, variations, combinations, or adaptations of the invention using its spirit and scope, as defined by the claims, may be directed to other uses and embodiments, or may be learned by practice of the invention.

Claims (3)

1. The spacecraft thermal control multilayer automatic transfer device is characterized by comprising a connecting frame, wherein a pair of transmission mechanisms are arranged on two sides of the connecting frame, and a clamping mechanism is connected between the pair of transmission mechanisms;
the transmission mechanism comprises a driving motor, a chain wheel and a chain, a driving chain wheel and a driven chain wheel are respectively arranged at two ends of one side of the corresponding connecting frame, the chain is meshed and connected between the driving chain wheel and the driven chain wheel, and an output shaft of the driving motor is connected with the driving chain wheel; the driving motors of the pair of transmission mechanisms work synchronously;
the clamping mechanism comprises a connecting rod and a plurality of fixing clamps for clamping materials, two ends of the connecting rod are fixedly connected to the pair of chains, and the fixing clamps are arranged on the connecting rod at equal intervals.
2. The spacecraft thermal control multilayer automatic transfer device of claim 1, wherein a plurality of auxiliary tugs are arranged below the connecting frame corresponding to the chains, and the auxiliary tugs support the chains transmitted below the connecting frame and are meshed with the chains.
3. The spacecraft thermal control multilayer automatic transfer device according to claim 1, wherein an auxiliary dragging rail is arranged above the connecting frame corresponding to the chain, the auxiliary dragging rail is arranged along the transmission direction of the chain, the auxiliary dragging rail is arranged at the bottom of the chain transmitted above the connecting frame, and the chain transmitted above the connecting frame is transmitted on the surface of the auxiliary dragging rail.
CN202011418313.0A 2020-12-07 2020-12-07 Automatic device of reprinting of spacecraft thermal control multilayer Pending CN112537633A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011418313.0A CN112537633A (en) 2020-12-07 2020-12-07 Automatic device of reprinting of spacecraft thermal control multilayer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011418313.0A CN112537633A (en) 2020-12-07 2020-12-07 Automatic device of reprinting of spacecraft thermal control multilayer

Publications (1)

Publication Number Publication Date
CN112537633A true CN112537633A (en) 2021-03-23

Family

ID=75016284

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202011418313.0A Pending CN112537633A (en) 2020-12-07 2020-12-07 Automatic device of reprinting of spacecraft thermal control multilayer

Country Status (1)

Country Link
CN (1) CN112537633A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201343301Y (en) * 2008-11-25 2009-11-11 万修杰 Automatic bottle placement machine
CN101613000A (en) * 2008-06-26 2009-12-30 美达新科技(深圳)有限公司 A kind of later-model film conveying method for packing machine
CN104528267A (en) * 2014-12-28 2015-04-22 荣成金达不锈钢设备有限公司 Kelp clamping feeding device
CN104528263A (en) * 2014-12-28 2015-04-22 荣成金达不锈钢设备有限公司 Kelp clamping discharging device
CN105621099A (en) * 2016-02-26 2016-06-01 信义环保特种玻璃(江门)有限公司 Large glass hanging bracket
CN107214178A (en) * 2017-06-21 2017-09-29 河南地之绿环保科技有限公司 A kind of plastic garbage conveying equipment
CN208731871U (en) * 2018-08-28 2019-04-12 惠州竞铭机械有限公司 A kind of material clamp structure and plate material transportation system

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101613000A (en) * 2008-06-26 2009-12-30 美达新科技(深圳)有限公司 A kind of later-model film conveying method for packing machine
CN201343301Y (en) * 2008-11-25 2009-11-11 万修杰 Automatic bottle placement machine
CN104528267A (en) * 2014-12-28 2015-04-22 荣成金达不锈钢设备有限公司 Kelp clamping feeding device
CN104528263A (en) * 2014-12-28 2015-04-22 荣成金达不锈钢设备有限公司 Kelp clamping discharging device
CN105621099A (en) * 2016-02-26 2016-06-01 信义环保特种玻璃(江门)有限公司 Large glass hanging bracket
CN107214178A (en) * 2017-06-21 2017-09-29 河南地之绿环保科技有限公司 A kind of plastic garbage conveying equipment
CN208731871U (en) * 2018-08-28 2019-04-12 惠州竞铭机械有限公司 A kind of material clamp structure and plate material transportation system

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Application publication date: 20210323