CN215969649U - Precision fine-adjustment device for aerospace composite material mold - Google Patents
Precision fine-adjustment device for aerospace composite material mold Download PDFInfo
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- CN215969649U CN215969649U CN202122173874.5U CN202122173874U CN215969649U CN 215969649 U CN215969649 U CN 215969649U CN 202122173874 U CN202122173874 U CN 202122173874U CN 215969649 U CN215969649 U CN 215969649U
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Abstract
The utility model discloses a precision fine-adjustment device for an aerospace composite material die, and relates to the technical field of aerospace composite material dies. Including base and adjusting device, the fixed adjusting device that is provided with in top of base, the inside activity of base is provided with the backup pad, the fixed regulation pole that is provided with in top of backup pad, the one end of adjusting the pole runs through to adjusting device's bottom and extends to adjusting device's inside, the fixed regulating plate that is provided with in one end of adjusting the pole, the bottom activity of backup pad is provided with the connecting rod, the relation of connection of backup pad and connecting rod is articulated, the one end activity of connecting rod is provided with the slider. Through setting up sleeve and threaded rod, the second motor drives the threaded rod and rotates, and the pivoted threaded rod drives the stripper plate of sleeve one end and carries out horizontal migration, presss from both sides tightly the both sides of mould to carry out the regulation of horizontal direction, adjustable mould horizontal direction's loss of precision and deformation to the mould.
Description
Technical Field
The utility model relates to the technical field of aerospace composite material dies, in particular to a precision fine adjustment device for an aerospace composite material die.
Background
The aerospace composite material is a high-performance new material system applied to aerospace craft, which is compounded by two or more than two heterogeneous, special-shaped and heterogeneous materials through a special molding process, and the compounding aims to improve the performance of the material or enable the material to meet a certain special physical performance requirement.
When the traditional composite material die is used, certain deformation is caused due to the fact that production circulation of high temperature and high pressure is frequently generated, so that the quality of the die is reduced, the adjusting range of the existing die precision adjusting mechanism is limited, and multiple accurate adjustment in the horizontal direction and the vertical direction of the die is difficult to realize.
SUMMERY OF THE UTILITY MODEL
The utility model provides a precision fine-adjustment device for an aerospace composite material die, which has the advantages of horizontal and vertical adjustment and solves the problem of die deformation.
In order to realize the purpose of adjusting in the horizontal and vertical directions, the utility model provides the following technical scheme: a precision fine-tuning device for an aerospace composite material die, which comprises a base and an adjusting device, the top of the base is fixedly provided with an adjusting device, the inside of the base is movably provided with a supporting plate, the top of the supporting plate is fixedly provided with an adjusting rod, one end of the adjusting rod penetrates through the bottom of the adjusting device and extends into the adjusting device, one end of the adjusting rod is fixedly provided with an adjusting plate, the bottom of the supporting plate is movably provided with a connecting rod, the supporting plate is hinged with the connecting rod, one end of the connecting rod is movably provided with a sliding block, the connecting rod is hinged with the sliding block, one side of the sliding block is fixedly provided with a transmission cylinder, a nut seat is fixedly arranged inside the transmission cylinder, the inner wall of the nut seat is connected with a screw rod through threads, one end of the screw rod is provided with a first motor, and two sides inside the adjusting device are both movably provided with extrusion plates.
As a preferred technical scheme of the utility model, sliding sleeves are fixedly arranged on both sides of the supporting plate, and sliding rods are movably arranged on the inner walls of the sliding sleeves.
As a preferable technical scheme of the utility model, a first protection pad is fixedly arranged at the top of the adjusting plate, and the first protection pad is connected with the adjusting plate in an adhesion manner.
As a preferable technical solution of the present invention, a second protection pad is fixedly disposed at one side of the compression plate.
As a preferred technical scheme of the utility model, the other side of the extrusion plate is fixedly provided with a sleeve, the inner wall of the sleeve is movably provided with a threaded rod, and one end of the threaded rod is provided with a second motor.
As a preferable technical scheme of the utility model, the inner side of the sleeve is provided with a thread groove, and the inner wall of the thread groove is in threaded connection with a threaded rod.
Compared with the prior art, the utility model provides a precision fine-tuning device for an aerospace composite material die, which has the following beneficial effects:
1. this precision micromatic setting for aerospace combined material mould, through setting up the backup pad, adjust the pole, the regulating plate, the connecting rod, the slider, the transmission section of thick bamboo, nut seat and lead screw, first motor drives the lead screw and rotates, the slider that utilizes the threaded connection of lead screw and nut seat to drive transmission section of thick bamboo one end carries out horizontal migration, the slider under the moving state changes the support angle of connecting rod, make the regulating plate of adjusting pole one end carry out vertical migration, thereby highly adjust the mould, accomplish the precision adjustment of vertical direction, make the completion production manufacturing work that the mould can be accurate.
2. This precision micromatic setting for aerospace combined material mould, through setting up sleeve and threaded rod, the second motor drives the threaded rod and rotates, and the pivoted threaded rod drives the stripper plate of sleeve one end and carries out horizontal migration, presss from both sides tightly the both sides of mould to carry out the regulation of horizontal direction, adjustable mould horizontal direction's precision loss and deformation to the mould.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a structural elevation view of the present invention;
FIG. 3 is a schematic view of the sleeve structure of the present invention;
FIG. 4 is an enlarged view of part A of the present invention;
fig. 5 is a schematic view of an adjusting plate according to the present invention.
In the figure: 1. a base; 101. an adjustment device; 102. a mold; 2. a support plate; 201. adjusting a rod; 202. an adjusting plate; 203. a first protection pad; 204. a connecting rod; 205. a slider; 206. a transmission cylinder; 207. a nut seat; 208. a screw rod; 209. a first motor; 210. a sliding sleeve; 211. a slide bar; 3. a pressing plate; 301. a second protection pad; 302. a sleeve; 303. a threaded rod; 304. a second motor.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, the utility model discloses a precision fine-tuning device for an aerospace composite material mold, which comprises a base 1 and an adjusting device 101, wherein the adjusting device 101 is fixedly arranged at the top of the base 1, a supporting plate 2 is movably arranged inside the base 1, an adjusting rod 201 is fixedly arranged at the top of the supporting plate 2, one end of the adjusting rod 201 penetrates through the bottom of the adjusting device 101 and extends into the adjusting device 101, an adjusting plate 202 is fixedly arranged at one end of the adjusting rod 201, a connecting rod 204 is movably arranged at the bottom of the supporting plate 2, the connecting relationship between the supporting plate 2 and the connecting rod 204 is hinged, a sliding block 205 is movably arranged at one end of the connecting rod 204, the connecting relationship between the connecting rod 204 and the sliding block 205 is hinged, a transmission cylinder 206 is fixedly arranged at one side of the sliding block 205, a nut seat 207 is fixedly arranged inside the transmission cylinder 206, the inner wall of the nut seat 207 is connected with a screw rod 208 in a threaded manner, one end of the screw rod 208 is provided with a first motor 209, and two sides inside the adjusting device 101 are both movably provided with the squeezing plates 3.
Specifically, sliding sleeves 210 are fixedly arranged on both sides of the supporting plate 2, and sliding rods 211 are movably arranged on the inner walls of the sliding sleeves 210.
In this embodiment, by providing the sliding sleeve 210 and the sliding rod 211, the moving tracks of the adjusting plate 202 and the adjusting rod 201 can be defined, so that the adjusting plate 202 can move vertically and stably.
Specifically, a first protection pad 203 is fixedly disposed on the top of the adjustment plate 202, and the connection relationship between the first protection pad 203 and the adjustment plate 202 is bonding.
In this embodiment, the bottom of the mold 102 can be protected by the first protection pad 203, so that the safety of the mold 102 is guaranteed.
Specifically, a second protection pad 301 is fixedly disposed on one side of the compression plate 3.
In this embodiment, the second protection pad 301 is provided to prevent the mold 102 from being damaged due to excessive clamping force, thereby protecting the mold 102.
Specifically, a sleeve 302 is fixedly arranged on the other side of the extrusion plate 3, a threaded rod 303 is movably arranged on the inner wall of the sleeve 302, and a second motor 304 is arranged at one end of the threaded rod 303.
In this embodiment, through setting up sleeve 302 and threaded rod 303, second motor 304 drives threaded rod 303 and rotates, and pivoted threaded rod 303 drives the stripper plate 3 of sleeve 302 one end and carries out horizontal migration, presss from both sides tight the both sides of mould 102 to carry out the regulation of horizontal direction to mould 102, the loss of precision and the deformation of adjustable mould 102 horizontal direction.
Specifically, a thread groove is formed on the inner side of the sleeve 302, and a threaded rod 303 is connected to the inner wall of the thread groove in a threaded manner.
In this embodiment, by providing the thread groove on the sleeve 302, the pressing plate 3 at one end of the sleeve 302 can be driven to move horizontally by the thread connection between the thread groove and the threaded rod 303.
The working principle and the using process of the utility model are as follows: when the die is used, the first motor 209 drives the screw rod 208 to rotate, the screw rod 208 is connected with the nut seat 207 through threads to drive the sliding block 205 at one end of the transmission cylinder 206 to move horizontally, the sliding block 205 in a moving state changes the supporting angle of the connecting rod 204, so that the adjusting plate 202 at one end of the adjusting rod 201 moves vertically, the height of the die 102 is adjusted, the second motor 304 drives the threaded rod 303 to rotate, the rotating threaded rod 303 drives the extrusion plate 3 at one end of the sleeve 302 to move horizontally, the two sides of the die 102 are clamped, and the die 102 is adjusted in the horizontal direction.
In summary, according to the precision fine-tuning device for the aerospace composite material mold, by arranging the sliding sleeve 210 and the sliding rod 211, the moving tracks of the adjusting plate 202 and the adjusting rod 201 can be limited, so that the adjusting plate 202 can stably and vertically move, by arranging the first protection pad 203, the bottom of the mold 102 can be protected, the safety of the mold 102 is guaranteed, by arranging the second protection pad 301, the damage of the mold 102 caused by excessive clamping force can be avoided, so as to protect the mold 102, by arranging the sleeve 302 and the threaded rod 303, the second motor 304 drives the threaded rod 303 to rotate, the rotating threaded rod 303 drives the extrusion plate 3 at one end of the sleeve 302 to horizontally move, and the two sides of the mold 102 are clamped, so that the mold 102 can be adjusted in the horizontal direction, the precision loss and deformation of the mold 102 in the horizontal direction can be adjusted, by arranging the threaded groove on the sleeve 302, the pressing plate 3 at one end of the sleeve 302 can be driven to move horizontally by the threaded connection of the threaded groove and the threaded rod 303.
It should be noted that, in this document, terms such as "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an aerospace precision micromatic setting for combined material mould, includes base (1) and adjusting device (101), its characterized in that: the top of the base (1) is fixedly provided with an adjusting device (101), a supporting plate (2) is movably arranged in the base (1), the top of the supporting plate (2) is fixedly provided with an adjusting rod (201), one end of the adjusting rod (201) penetrates through the bottom of the adjusting device (101) and extends into the adjusting device (101), one end of the adjusting rod (201) is fixedly provided with an adjusting plate (202), the bottom of the supporting plate (2) is movably provided with a connecting rod (204), the connecting relation between the supporting plate (2) and the connecting rod (204) is hinged, one end of the connecting rod (204) is movably provided with a sliding block (205), the connecting relation between the connecting rod (204) and the sliding block (205) is hinged, one side of the sliding block (205) is fixedly provided with a transmission cylinder (206), and a nut seat (207) is fixedly arranged in the transmission cylinder (206), the inner wall of the nut seat (207) is in threaded connection with a screw rod (208), one end of the screw rod (208) is provided with a first motor (209), and two sides inside the adjusting device (101) are both movably provided with the extrusion plates (3).
2. The precision fine-tuning device for the aerospace composite material mold as claimed in claim 1, wherein: sliding sleeves (210) are fixedly arranged on two sides of the supporting plate (2), and sliding rods (211) are movably arranged on the inner walls of the sliding sleeves (210).
3. The precision fine-tuning device for the aerospace composite material mold as claimed in claim 1, wherein: the top of the adjusting plate (202) is fixedly provided with a first protection pad (203), and the connection relation between the first protection pad (203) and the adjusting plate (202) is bonding.
4. The precision fine-tuning device for the aerospace composite material mold as claimed in claim 1, wherein: and a second protective pad (301) is fixedly arranged on one side of the extrusion plate (3).
5. The precision fine-tuning device for the aerospace composite material mold as claimed in claim 1, wherein: the other side of the extrusion plate (3) is fixedly provided with a sleeve (302), the inner wall of the sleeve (302) is movably provided with a threaded rod (303), and one end of the threaded rod (303) is provided with a second motor (304).
6. The precision fine-tuning device for the aerospace composite material mold as claimed in claim 5, wherein: the inner side of the sleeve (302) is provided with a thread groove, and the inner wall of the thread groove is connected with a threaded rod (303) in a threaded manner.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122173874.5U CN215969649U (en) | 2021-09-09 | 2021-09-09 | Precision fine-adjustment device for aerospace composite material mold |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122173874.5U CN215969649U (en) | 2021-09-09 | 2021-09-09 | Precision fine-adjustment device for aerospace composite material mold |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215969649U true CN215969649U (en) | 2022-03-08 |
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ID=80468583
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122173874.5U Active CN215969649U (en) | 2021-09-09 | 2021-09-09 | Precision fine-adjustment device for aerospace composite material mold |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215969649U (en) |
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2021
- 2021-09-09 CN CN202122173874.5U patent/CN215969649U/en active Active
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