CN213353363U - Integral forming die for composite material structure of unmanned aerial vehicle - Google Patents
Integral forming die for composite material structure of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN213353363U CN213353363U CN202022165246.8U CN202022165246U CN213353363U CN 213353363 U CN213353363 U CN 213353363U CN 202022165246 U CN202022165246 U CN 202022165246U CN 213353363 U CN213353363 U CN 213353363U
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- fixedly connected
- mould
- bed die
- aerial vehicle
- unmanned aerial
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- 239000002131 composite material Substances 0.000 title claims description 11
- 229920003023 plastic Polymers 0.000 claims abstract description 21
- 239000004033 plastic Substances 0.000 claims abstract description 21
- 239000000463 material Substances 0.000 claims abstract description 5
- 238000001746 injection moulding Methods 0.000 claims description 16
- 238000007789 sealing Methods 0.000 claims description 6
- 238000000465 moulding Methods 0.000 abstract description 11
- 238000002347 injection Methods 0.000 abstract description 9
- 239000007924 injection Substances 0.000 abstract description 9
- 230000005540 biological transmission Effects 0.000 abstract description 5
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 238000007493 shaping process Methods 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000005266 casting Methods 0.000 abstract description 2
- 238000006748 scratching Methods 0.000 abstract description 2
- 230000002393 scratching effect Effects 0.000 abstract description 2
- 238000009434 installation Methods 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
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- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle combined material structure whole forming die, including mount, last mould, bed die, push pedal and link gear, sliding connection has one to go up mould and a bed die in the mount, it is located the top of bed die to go up the mould, bed die upper end central point puts and has seted up a groove of moulding plastics, the groove bottom of moulding plastics just is located and has seted up a mounting hole in the bed die, mount lower extreme central point puts a support column of fixedly connected with, the utility model discloses the beneficial effect who reaches is: through link gear's drive gear transmission, can make mould casting shaping back, go up mould and bed die and move to opposite direction simultaneously to make the push pedal push away the unmanned aerial vehicle shell after the shaping from moulding plastics the inslot, made things convenient for injection mold's drawing of patterns, when having avoided scratching out with the finished product that moulds plastics the inslot with the hand, caused the damaged condition of finished product easily, not only improved the security of unmanned aerial vehicle shell production, improved the efficiency of drawing of patterns moreover.
Description
Technical Field
The utility model relates to a forming die, in particular to whole forming die of unmanned aerial vehicle combined material structure belongs to unmanned aerial vehicle production mould technical field.
Background
The unmanned aerial vehicle mould is an injection mould of processing unmanned aerial vehicle plastic casing, injects liquid combined material into the inslot of moulding plastics through the pipe of moulding plastics, takes out after cooling again, accomplishes the processing to unmanned aerial vehicle shell.
However, in the actual operation process, because the groove of moulding plastics is airtight space in the mould, lead to in drawing of patterns process, can only pull out the finished product in the inslot of moulding plastics through the manual work, not only operate slower, often can cause the broken problem of mould moreover.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to overcome prior art's defect, provide an unmanned aerial vehicle combined material structure whole forming die.
In order to solve the technical problem, the utility model provides a following technical scheme:
the utility model relates to an integral forming die for an unmanned aerial vehicle composite material structure, which comprises a fixed frame, an upper die, a lower die, a push plate and a linkage mechanism, wherein the fixed frame is internally and slidably connected with the upper die and the lower die, the upper die is positioned above the lower die, the central position of the upper end of the lower die is provided with an injection groove, the bottom of the injection groove is provided with an installation hole in the lower die, the central position of the lower end of the fixed frame is fixedly connected with a support column, the upper end of the support column is fixedly connected with the push plate corresponding to the installation hole, the push plate is clamped in the installation hole, the two sides of the fixed frame and the connection parts of the two ends of the upper die and the lower die are respectively provided with a slide groove, the two ends of the upper die and the lower die are respectively and fixedly connected with a slide block, the slide blocks are respectively and, go up mould upper end fixedly connected with two sets of pneumatic cylinders, it is two sets of the equal fixed connection in mount upper end in pneumatic cylinder upper end.
As a preferred technical scheme of the utility model, link gear includes support frame, fixed rotating shaft, linkage gear, hydraulic stem and connecting block, the support frame is provided with two pairs, two pairs equal swivelling joint has two fixed rotating shafts and vertical distribution about and between the support frame, two linkage gear of the equal fixedly connected with of fixed rotating shaft intermediate position, linkage gear all meshes the connection, two on the fixed rotating shaft and be located hydraulic stem of the equal fixedly connected with in linkage gear both sides, the slider outside and the equal fixedly connected with connecting block in the corresponding position of hydraulic stem, the hydraulic stem is kept away from the equal swivelling joint of fixed rotating shaft one end on the connecting block.
As a preferred technical scheme of the utility model, a fixing bearing of support frame and the equal fixedly connected with of fixed rotating shaft junction, the inboard equal fixed connection of fixing bearing inner circle is in fixed rotating shaft, the equal fixed connection in the fixing bearing inner circle outside is in the support frame.
As a preferred technical scheme of the utility model, sealed pad of push pedal outside fixedly connected with, sealed pad outside and mounting hole lateral wall contact mutually.
As an optimal technical scheme of the utility model, the pipe of moulding plastics of fixedly connected with in the support column, mould plastics and manage the upper end and pass the support column and the push pedal is located the tank bottom portion of moulding plastics, mould plastics and manage and keep away from the solenoid valve that the groove one end of moulding plastics passed support column and fixedly connected with.
As a preferred technical scheme of the utility model, a spacing hole has all been seted up in bed die upper end four corners, go up the mould lower extreme and with a gag lever post of the equal fixedly connected with in spacing hole corresponding position.
The utility model discloses the beneficial effect who reaches is: through link gear's drive gear transmission, can make mould casting shaping back, go up mould and bed die and move to opposite direction simultaneously to make the push pedal push away the unmanned aerial vehicle shell after the shaping from moulding plastics the inslot, made things convenient for injection mold's drawing of patterns, when having avoided scratching out with the finished product that moulds plastics the inslot with the hand, caused the damaged condition of finished product easily, not only improved the security of unmanned aerial vehicle shell production, improved the efficiency of drawing of patterns moreover.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a schematic diagram of a front urgent structure of the present invention;
FIG. 2 is a schematic side view of the present invention;
fig. 3 is a schematic view of the top-down appearance structure of the lower mold of the present invention;
fig. 4 is a schematic side sectional structure view of the linkage mechanism of the present invention.
In the figure: 1. a fixed mount; 2. an upper die; 3. a lower die; 4. mounting holes; 5. pushing the plate; 6. a gasket; 7. a chute; 8. a slider; 9. a linkage mechanism; 91. a support frame; 92. fixing the rotating shaft; 93. a linkage gear; 94. fixing the bearing; 95. a hydraulic lever; 96. connecting blocks; 10. injection molding a groove; 11. a support pillar; 12. injection molding a tube; 13. an electromagnetic valve; 14. a limiting hole; 15. a limiting rod; 16. and a hydraulic cylinder.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.
Examples
As shown in figures 1-4, the utility model provides an integral forming mold of an unmanned aerial vehicle composite material structure, which comprises a fixing frame 1, an upper mold 2, a lower mold 3, a push plate 5 and a linkage mechanism 9, wherein the fixing frame 1 is internally connected with the upper mold 2 and the lower mold 3 in a sliding way, the upper mold 2 is positioned above the lower mold 3, the central position of the upper end of the lower mold 3 is provided with an injection molding groove 10, the bottom of the injection molding groove 10 is provided with a mounting hole 4 in the lower mold 3, the central position of the lower end of the fixing frame 1 is fixedly connected with a support column 11, the upper end of the support column 11 is fixedly connected with the push plate 5 corresponding to the mounting hole 4, the push plate 5 is clamped in the mounting hole 4, the connecting parts of the two sides of the fixing frame 1 and the two ends of the upper mold 2 and the lower mold 3 are both provided with, the equal sliding connection of slider 8 is in corresponding spout 7, and link gear 9 sets up in 1 both sides of mount and is located between mould 2 and the bed die 3, goes up two sets of pneumatic cylinders 16 of 2 upper ends fixedly connected with of mould, and the equal fixed connection in 1 upper end of mount in 16 upper ends of two sets of pneumatic cylinders has not only improved the security of unmanned aerial vehicle shell production, has improved the efficiency of drawing of patterns moreover.
Four corners of the upper end of the lower die 3 are respectively provided with a limiting hole 14, the lower end of the upper die 2 and the position corresponding to the limiting hole 14 are respectively and fixedly connected with a limiting rod 15, the accuracy of the pressing between the upper die 2 and the lower die 3 can be effectively ensured, the inner part of the supporting column 11 is fixedly connected with an injection molding pipe 12, the upper end of the injection molding pipe 12 passes through the supporting column 11 and the push plate 5 is positioned at the bottom of the injection molding groove 10, one end of the injection molding pipe 12 far away from the injection molding groove 10 passes through the supporting column 11 and is fixedly connected with an electromagnetic valve 13, liquid plastic can be injected into the injection molding groove 10 through the injection molding pipe 12, the outer side of the push plate 5 is fixedly connected with a sealing gasket 6, the outer side of the sealing gasket 6 is contacted with the side wall of the mounting hole 4, the sealing gasket 6 can ensure the sealing performance of, two fixed rotating shafts 92 are rotatably connected between two pairs of supporting frames 91 and vertically distributed, a linkage gear 93 is fixedly connected between the middle positions of the two fixed rotating shafts 92, the linkage gear 93 is meshed and connected, a hydraulic rod 95 is fixedly connected on the two fixed rotating shafts 92 and on the two sides of the linkage gear 93, a connecting block 96 is fixedly connected on the outer side of the sliding block 8 corresponding to the hydraulic rod 95, one end of the hydraulic rod 95 far away from the fixed rotating shafts 92 is rotatably connected on the connecting block 96, a fixed bearing 94 is fixedly connected at the joint of the supporting frames 91 and the fixed rotating shafts 92, the inner side of the inner ring of the fixed bearing 94 is fixedly connected on the fixed rotating shafts 92, the outer side of the inner ring and the outer ring of the fixed bearing 94 are, through the transmission of the transmission gear 93 of the linkage mechanism 9, the upper die 2 and the lower die 3 can move in opposite directions simultaneously after the die is cast.
Specifically, the whole device is connected with an external power supply, then the electromagnetic valve 13 is opened, so that liquid composite plastic is injected into the injection groove 10 through the injection pipe 12, after the composite plastic in the injection groove 10 is cooled and formed, the electromagnetic valve 13 is closed, then the electromagnetic valve 13 is opened, so that the output end of the hydraulic cylinder 16 is contracted and moved upwards, the sliding blocks 8 on the two sides of the upper mold 2 are driven to move upwards, the connecting blocks 96 on the two sides of the upper mold 2 are driven to move upwards, finally, the hydraulic rods 95 and the fixed rotating shaft 92 are driven to rotate, the hydraulic rods 95 on the two sides of the lower mold 3 are driven to rotate through the transmission of the linkage gear 93, so that the connecting blocks 96 and the sliding blocks 8 on the two sides of the lower mold 3 are driven to move downwards, finally, the lower mold 3 is lowered, the formed unmanned aerial vehicle shell is pushed out of the injection groove 10 by the push plate 5, the operation is simple, and the condition that the finished product is damaged when the finished product is demoulded is avoided.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle combined material structure whole forming die, a serial communication port, including mount (1), last mould (2), bed die (3), push pedal (5) and link gear (9), sliding connection has one to go up mould (2) and a bed die (3) in mount (1), it is located the top of bed die (3) to go up mould (2), bed die (3) upper end central point puts and has seted up one and moulds plastics groove (10), mould plastics groove (10) bottom and be located bed die (3) and seted up one mounting hole (4), mount (1) lower extreme central point puts support column (11) of fixedly connected with, support column (11) upper end and push pedal (5) of the corresponding position fixedly connected with of mounting hole (4), push pedal (5) joint is in mounting hole (4), mount (1) both sides and last mould (2) and bed die (3) both ends junction have all seted up one and have seted up one push pedal (5), push pedal (5) joint, mount (1 Spout (7), go up slider (8) of the equal fixedly connected with in mould (2) and bed die (3) both ends, the equal sliding connection of slider (8) is in corresponding spout (7), link gear (9) set up in mount (1) both sides and are located between mould (2) and bed die (3), go up two sets of pneumatic cylinders (16) of mould (2) upper end fixedly connected with, two sets of pneumatic cylinder (16) upper end equal fixed connection is in mount (1) upper end.
2. The integral forming die for the unmanned aerial vehicle composite material structure according to claim 1, the linkage mechanism (9) comprises a support frame (91), a fixed rotating shaft (92), a linkage gear (93), a hydraulic rod (95) and a connecting block (96), two pairs of the supporting frames (91) are arranged, two fixed rotating shafts (92) are respectively connected between the two pairs of the supporting frames (91) in a rotating way and vertically distributed, a linkage gear (93) is respectively fixedly connected at the middle position of each fixed rotating shaft (92), the linkage gears (93) are all in meshed connection, two hydraulic rods (95) are fixedly connected to the two fixed rotating shafts (92) and positioned at the two sides of the linkage gears (93), the outer side of the sliding block (8) is fixedly connected with a connecting block (96) at the position corresponding to the hydraulic rod (95), and one end of the hydraulic rod (95) far away from the fixed rotating shaft (92) is rotationally connected to the connecting block (96).
3. The integral forming mold for the composite material structure of the unmanned aerial vehicle as claimed in claim 2, wherein a fixing bearing (94) is fixedly connected to a joint of the supporting frame (91) and the fixing rotating shaft (92), inner sides of inner rings of the fixing bearing (94) are fixedly connected to the fixing rotating shaft (92), and outer sides of inner and outer rings of the fixing bearing (94) are fixedly connected to the inside of the supporting frame (91).
4. The integral forming mold for the composite material structure of the unmanned aerial vehicle as claimed in claim 1, wherein a sealing gasket (6) is fixedly connected to the outer side of the push plate (5), and the outer side of the sealing gasket (6) is in contact with the side wall of the mounting hole (4).
5. The integrated forming mold for the composite material structure of the unmanned aerial vehicle as claimed in claim 1, wherein an injection molding pipe (12) is fixedly connected in the support column (11), the upper end of the injection molding pipe (12) passes through the support column (11) and the push plate (5) and is located at the bottom of the injection molding groove (10), and one end of the injection molding pipe (12) far away from the injection molding groove (10) passes through the support column (11) and is fixedly connected with an electromagnetic valve (13).
6. The integral forming mold for the composite material structure of the unmanned aerial vehicle as claimed in claim 1, wherein four corners of the upper end of the lower mold (3) are respectively provided with a limiting hole (14), and a limiting rod (15) is fixedly connected to the lower end of the upper mold (2) and corresponds to the limiting hole (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022165246.8U CN213353363U (en) | 2020-09-27 | 2020-09-27 | Integral forming die for composite material structure of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022165246.8U CN213353363U (en) | 2020-09-27 | 2020-09-27 | Integral forming die for composite material structure of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213353363U true CN213353363U (en) | 2021-06-04 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022165246.8U Active CN213353363U (en) | 2020-09-27 | 2020-09-27 | Integral forming die for composite material structure of unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN213353363U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113997603A (en) * | 2021-11-17 | 2022-02-01 | 安徽皓翔航空科技有限公司 | Carbon fiber composite material U-shaped frame, U-shaped frame forming die and forming method |
-
2020
- 2020-09-27 CN CN202022165246.8U patent/CN213353363U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113997603A (en) * | 2021-11-17 | 2022-02-01 | 安徽皓翔航空科技有限公司 | Carbon fiber composite material U-shaped frame, U-shaped frame forming die and forming method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A Kind of Integrated Forming Mold for Composite Structure of Unmanned Aerial Vehicle Effective date of registration: 20230810 Granted publication date: 20210604 Pledgee: Pudong Development Bank of Shanghai Limited by Share Ltd. Xi'an branch Pledgor: XI'AN YALONG AVIATION ELECTROMECHANICAL CO.,LTD. Registration number: Y2023980051607 |
|
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 710089 No. 38, Hangkong 1st Road, National Aviation high tech industry base, Xi'an, Shaanxi Province Patentee after: Xi'an Yalong Aviation Electromechanical Co.,Ltd. Country or region after: China Address before: No.38, Hangkong 1st Road, Xi'an Aviation base, Shaanxi 710000 Patentee before: XI'AN YALONG AVIATION ELECTROMECHANICAL CO.,LTD. Country or region before: China |