CN112589901B - Multi-functional equipment of tailorring of spacecraft thermal control multilayer - Google Patents

Multi-functional equipment of tailorring of spacecraft thermal control multilayer Download PDF

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Publication number
CN112589901B
CN112589901B CN202011364162.5A CN202011364162A CN112589901B CN 112589901 B CN112589901 B CN 112589901B CN 202011364162 A CN202011364162 A CN 202011364162A CN 112589901 B CN112589901 B CN 112589901B
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China
Prior art keywords
air suction
bed body
thermal control
control multilayer
machine head
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CN202011364162.5A
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CN112589901A (en
Inventor
王哲
傅浩
范子琦
彭鹤
于洋
武婷婷
边玉川
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Beijing Institute of Spacecraft Environment Engineering
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Beijing Institute of Spacecraft Environment Engineering
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Priority to CN202011364162.5A priority Critical patent/CN112589901B/en
Publication of CN112589901A publication Critical patent/CN112589901A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D11/00Combinations of several similar cutting apparatus
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D7/00Details of apparatus for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
    • B26D7/01Means for holding or positioning work
    • B26D7/018Holding the work by suction
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D7/00Details of apparatus for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
    • B26D7/27Means for performing other operations combined with cutting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D11/00Combinations of several similar cutting apparatus
    • B26D2011/005Combinations of several similar cutting apparatus in combination with different kind of cutters, e.g. two serial slitters in combination with a transversal cutter
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/10Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working

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  • Life Sciences & Earth Sciences (AREA)
  • Forests & Forestry (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Cutting Processes (AREA)

Abstract

The application provides a spacecraft thermal control multilayer multifunctional cutting device which comprises a bed body, wherein a machine head, an air suction system, a positioning projection device and an electric control system are arranged on the bed body; the machine head can slide in the guide rail on the surface of the bed body; the machine head comprises a hob actuating mechanism, a vibrating knife actuating mechanism, a stamping knife mechanism, an ink jet mechanism, a line drawing mechanism and a double-sided tape pasting mechanism; the air suction system is arranged in the bed body, the surface of the bed body is provided with a plurality of air suction areas corresponding to the air suction system, and each air suction area is provided with a plurality of air suction holes; the positioning projection device is arranged above the bed body and comprises a plurality of projectors, and all the projectors work together to project the heat control multilayer; the electric control system is in signal connection with the machine head, the air suction system and the positioning projection device. The beneficial effect of this application is: the equipment automatically cuts and shapes the material core and the surface film in the thermal control multilayer manufacturing process, marks and punches the material core and automatically pastes the double-sided adhesive tape, has high automation degree, improves the working efficiency, and has better processing quality and consistency.

Description

Multi-functional equipment of tailorring of spacecraft thermal control multilayer
Technical Field
The disclosure relates to the technical field of manufacturing of a thermal control multilayer of a spacecraft, in particular to a multifunctional cutting device for the thermal control multilayer of the spacecraft.
Background
The thermal control multilayer is a flexible product on the spacecraft, is arranged on the surfaces of the spacecraft and equipment, and directly influences the temperature control and on-orbit operation effects of the spacecraft. The original processing mode of the thermal control multilayer is a cutting mode of a triangular vibrating knife cutting and single punch, the problems that the edge of the thermal control multilayer is irregular after cutting, the single-layer film is cut, the edge is torn and cannot be used and the like exist, functions of automatic identification, double-sided tape pasting, projection positioning and the like do not exist, the processing of the identification pasting double-sided tape and the installation hole can only be manually carried out, the operation efficiency is low, and the processing quality and the consistency level are not high.
Disclosure of Invention
The utility model aims at the above problem, provide a multi-functional tailorring equipment of spacecraft thermal control multilayer.
In a first aspect, the application provides a spacecraft thermal control multilayer multifunctional cutting device which comprises a bed body, wherein a machine head, an air suction system, a positioning projection device and an electric control system are arranged on the bed body; the machine head is arranged on the surface of the bed body, a guide rail is arranged on the surface of the bed body, and a transmission mechanism is further arranged on the bed body and drives the machine head to slide along the guide rail; the machine head comprises a hobbing cutter actuating mechanism, a vibrating cutter actuating mechanism, a punching cutter mechanism, an ink-jet mechanism, a line drawing mechanism and a double-sided tape pasting mechanism; the hob actuating mechanism cuts and shapes the material by rolling and cutting the material; the vibrating knife actuating mechanism vibrates up and down to cut the material; the punching cutter mechanism is used for processing round holes in the materials; the ink-jet mechanism sprays dot-shaped ink for identification on the material; the line drawing mechanism draws a graph for identification on the material; the double-sided tape sticking mechanism is used for cutting double-sided tapes and sticking the cut tapes to corresponding positions of materials; the air suction system is arranged in the bed body, the surface of the bed body is provided with a plurality of air suction areas corresponding to the air suction system, and each air suction area is provided with a plurality of air suction holes; the positioning projection device is arranged above the bed body and comprises a plurality of projectors, and all the projectors work together to project the heat control multilayer; and the electric control system is in signal connection with the machine head, the air suction system and the positioning projection device.
According to the technical scheme provided by the embodiment of the application, the circular hob is installed on the hob executing mechanism, and the cutting edge of the circular hob rolls on the material to cut.
According to the technical scheme provided by the embodiment of the application, the straight blade is installed on the vibration knife executing mechanism, and the cutting edge of the straight blade vibrates up and down in the process of traveling to cut materials.
According to the technical scheme provided by the embodiment of the application, the circular punch is arranged on the punch executing mechanism, and the circular punch can rotate around the axis of the punch to process a circular hole in a material when the punch descends.
According to the technical scheme provided by the embodiment of the application, a waste collecting box is arranged above the stamping knife executing mechanism and used for absorbing waste materials after punching.
According to the technical scheme provided by the embodiment of the application, the guide rail comprises an X track and a Y track which are vertically arranged.
The invention has the beneficial effects that: the application provides a multi-functional tailorring equipment of spacecraft thermal control multilayer, place core material or surface film etc. materials that need in the spacecraft thermal control multilayer manufacture process on the surface of the bed body, adsorb the material to fix on the surface of the bed body through the induced draft system, the mobile aircraft nose carries on automatic tailoring shaping, marking, mounting hole punching and double-sided tape automatic sticking to core material and surface film after shaping through each organization in the aircraft nose, the degree of automation is high, has raised the working efficiency, the processing quality and conformance are better; all projectors in the projection positioning device work jointly, automatic splicing projection of large-size thermal control multilayer graphs is achieved, and meanwhile the mounting holes of the thermal control multilayer are positioned.
Drawings
Fig. 1 and 2 are schematic structural diagrams of a first embodiment of the present application;
FIG. 3 is a schematic structural diagram of a positioning projection apparatus according to a first embodiment of the present application;
FIG. 4 is a schematic structural diagram of a handpiece in a first embodiment of the present application;
the text labels in the figures are represented as: 1. a bed body; 2. positioning the projection device; 3. a machine head; 11. an air suction system; 12. a guide rail; 13. an electronic control system; 21. a projector; 22. a support; 31. a hob actuating mechanism; 32. a vibrating knife actuator; 33. a die cutter mechanism; 34. a double-sided tape sticking mechanism; 35. an ink jet mechanism; 36. drawing mechanism.
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.
Fig. 1 to 4 are schematic diagrams of an embodiment of the present application, which include a bed body 1, and a machine head 3, an air suction system 11, a positioning projection device 2, and an electric control system 13 are disposed on the bed body 1; the machine head 3 is arranged on the surface of the bed body 1, a guide rail 12 is arranged on the surface of the bed body 1, and a transmission mechanism is further arranged on the bed body 1 and drives the machine head 3 to slide along the guide rail 12. Preferably, the guide rail 12 includes an X-rail and a Y-rail that are vertically disposed. In this embodiment, the transmission mechanism drives the machine head 3 to slide in the X track or the Y track so as to process different positions of the material.
The air suction system 11 is arranged in the bed body 1, the surface of the bed body 1 corresponds to the air suction system 11 is provided with a plurality of air suction areas, each of which is provided with a plurality of air suction holes. In this embodiment, PVC material is laid on 1 surface of the bed body, for the material provides the processing mesa, and the material is placed on 1 surface of the bed body, and the fan of air suction system 11 adsorbs the material on the mesa through the hole of induced drafting, sets up a plurality of regions of induced drafting with 1 surface of the bed body, can specifically select the not regional region of induced drafting according to actual material size, or adsorb the regional combination of induced drafting in a plurality of regions.
The positioning projection device 2 is arranged above the bed body 1 and comprises a plurality of projectors 21, and the projectors 21 work jointly to project heat control layers. In this embodiment, each projector 21 is erected above the bed 1 through the bracket 22, and the position of the bracket 22 on the bed 1 and the height of the bracket 22 can be adjusted according to actual needs. In the embodiment, all projectors 21 work together to realize automatic splicing projection of large-size thermal control multilayer graphs, show the processing positions of the thermal control multilayer graphs, and are used for repositioning the thermal control multilayer after cutting, forming and enveloping and before processing mounting holes, and the positioning precision is better than 1 mm.
And the electric control system 13 is in signal connection with the machine head 3, the air suction system 11 and the positioning projection device 2. In this embodiment, the electronic control system 13 controls hardware such as the machine head 3 and the positioning projection device 2 to perform positioning and cutting tasks through programs, and can receive instructions through the operation panel and perform real-time feedback of execution conditions.
The machine head 3 comprises a hob actuating mechanism 31, a vibrating knife actuating mechanism 32, a stamping knife mechanism 33, an ink jet mechanism 35, a line drawing mechanism 36 and a double-sided tape pasting mechanism 34. The machine head 3 in this embodiment includes a plurality of mechanisms, and can perform a plurality of operations in a thermal control multilayer manufacturing process such as rolling cutting, straight cutting, line drawing, ink jet, double-sided adhesive tape pasting, and the like.
In this embodiment, the hob actuator 31 may be configured to mount a circular hob to perform rolling cutting on a material to cut and shape the material, the cutting edge is neat, and the cutting precision is better than 0.5 mm.
In this embodiment, the vibration knife actuator 32 may be provided with a straight blade, and the blade vibrates up and down during the movement to cut the material with a thickness of 30 units, and the cutting precision is better than 1 mm.
The die cutter mechanism 33 can be provided with round punches with different diameters, and the round punches rotate around the axes of the punches while descending to process round holes in materials. Preferably, a waste collecting box is arranged above the stamping knife executing mechanism and used for absorbing waste after punching.
The ink-jet mechanism 35 sprays dot-shaped ink for identification on the material; the drawing mechanism 36 draws a graphic for identification on the material.
The double-sided tape sticking mechanism 34 is used for cutting double-sided tapes and sticking the cut tapes to corresponding positions of materials, and the sticking position precision is superior to 1 mm.
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 (5)

1. The spacecraft thermal control multilayer multifunctional cutting equipment is characterized by comprising a bed body, wherein a machine head, an air suction system, a positioning projection device and an electric control system are arranged on the bed body;
the machine head is arranged on the surface of the bed body, a guide rail is arranged on the surface of the bed body, and a transmission mechanism is further arranged on the bed body and drives the machine head to slide along the guide rail;
the machine head comprises a hobbing cutter actuating mechanism, a vibrating cutter actuating mechanism, a punching cutter mechanism, an ink-jet mechanism, a line drawing mechanism and a double-sided tape pasting mechanism; the hob actuating mechanism cuts and shapes the material by rolling and cutting the material; the vibrating knife actuating mechanism vibrates up and down to cut the material; the punching cutter mechanism is used for processing round holes in the materials; the ink-jet mechanism sprays dot-shaped ink for identification on the material; the line drawing mechanism draws a graph for identification on the material; the double-sided tape sticking mechanism is used for cutting double-sided tapes and sticking the cut tapes to corresponding positions of materials;
a waste collecting box is arranged above the punching cutter mechanism and used for absorbing waste after punching;
the air suction system is arranged in the bed body, the surface of the bed body is provided with a plurality of air suction areas corresponding to the air suction system, and each air suction area is provided with a plurality of air suction holes; the air suction areas in different areas can be selected according to the actual material size, or the air suction areas in a plurality of areas are combined for adsorption;
the positioning projection device is arranged above the bed body and comprises a plurality of projectors, and all the projectors work together to project the heat control multilayer; all projectors work together to realize automatic splicing projection of large-size thermal control multilayer graphs, show the processing positions of the thermal control multilayer graphs and be used for repositioning the thermal control multilayer graphs before processing mounting holes after cutting, forming and enveloping the thermal control multilayer graphs;
and the electric control system is in signal connection with the machine head, the air suction system and the positioning projection device.
2. The spacecraft thermal control multilayer multifunctional cutting equipment according to claim 1, wherein a circular hob is installed on the hob executing mechanism, and the edge of the circular hob rolls on materials to cut.
3. The spacecraft thermal control multilayer multifunctional cutting equipment according to claim 1, wherein a straight blade is mounted on the vibrating blade actuator, and the blade edge of the straight blade vibrates up and down in the process of traveling to cut materials.
4. The spacecraft thermal control multilayer multifunctional cutting equipment according to claim 1, wherein a circular punch is mounted on the punch mechanism, and the punch can rotate around the axis of the punch to process a circular hole in a material while descending.
5. The spacecraft thermal control multilayer multifunctional trimming device according to any one of claims 1 to 4, wherein the guide rail comprises an X-orbit and a Y-orbit which are vertically arranged.
CN202011364162.5A 2020-11-27 2020-11-27 Multi-functional equipment of tailorring of spacecraft thermal control multilayer Active CN112589901B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011364162.5A CN112589901B (en) 2020-11-27 2020-11-27 Multi-functional equipment of tailorring of spacecraft thermal control multilayer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011364162.5A CN112589901B (en) 2020-11-27 2020-11-27 Multi-functional equipment of tailorring of spacecraft thermal control multilayer

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CN112589901A CN112589901A (en) 2021-04-02
CN112589901B true CN112589901B (en) 2022-07-05

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Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1460141A1 (en) * 1964-08-01 1968-12-19 Schubert & Salzer Maschinen Process and device for automatic cutting of textile materials
US3844461A (en) * 1973-04-09 1974-10-29 Gerber Scientific Instr Co Precise indexing apparatus and method
CN202297617U (en) * 2011-08-01 2012-07-04 东莞市爱玛数控科技有限公司 Sheet stock cutting device
TWI618131B (en) * 2013-08-30 2018-03-11 半導體能源研究所股份有限公司 Device for forming separation starting point, stack manufacturing apparatus, and method for forming separation starting point
CN207031880U (en) * 2017-06-02 2018-02-23 格柏(上海)工业数控设备有限公司 A kind of projection numerical control cutting
CN209289408U (en) * 2018-12-13 2019-08-23 上海伊斯曼电气股份有限公司 A kind of minitype cutting machine
CN209579691U (en) * 2019-02-28 2019-11-05 江苏摩臣智联科技股份有限公司 The shear of handset touch panel
CN210158122U (en) * 2019-05-05 2020-03-20 东莞市瀚通激光科技有限公司 Automatic line drawing and marking equipment based on visual recognition
CN210525306U (en) * 2019-09-16 2020-05-15 杭州临安镜胡纸业有限公司 Rewinding paper cutter

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