CN218801753U - Servo cabin metalwork glues location structure - Google Patents
Servo cabin metalwork glues location structure Download PDFInfo
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- CN218801753U CN218801753U CN202223058927.XU CN202223058927U CN218801753U CN 218801753 U CN218801753 U CN 218801753U CN 202223058927 U CN202223058927 U CN 202223058927U CN 218801753 U CN218801753 U CN 218801753U
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- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
Abstract
The utility model discloses a servo cabin metalwork glues and glues location structure, including basic part and fixed jacket layer, be provided with connection structure on the fixed jacket layer, connection structure, include: inner plate, adhesion layer, top groove, opening and fixed part, the inner plate is fixed jacket layer inner wall, the adhesion layer is fixed the inner plate bottom surface and paste the connection and be in on the basis piece, the top groove is opened fixed jacket layer top, the opening is opened the top inslot, the fixed part sets up on the fixed jacket layer. The utility model discloses be provided with the fixed jacket layer of two semicircular structures, inside be provided with basic piece size assorted inner plating, the suit is on basic piece and through adhesion layer fixed position after the concatenation, and easy to assemble metalwork can play the effect of correcting the location, and after the installation was accomplished, can dismantle connection structure and separate and open and take off, convenient to use easy operation, the practicality is strong.
Description
Technical Field
The utility model belongs to the technical field of the location structure technique and specifically relates to a servo cabin metalwork glues and glues location structure is related to.
Background
At present, a cabin body made of composite materials is provided, and metal parts are needed to be adhered to the cabin body for assembling other parts. Compared with the traditional metal material, the composite material has the advantages of high specific strength, high specific modulus, anisotropy, fatigue resistance, corrosion resistance, designable performance, multiple functions and the like, and the application of the composite material plays a vital role in promoting the lightweight and high performance of aerospace equipment. The wide application of the composite material inevitably encounters the connection problem of the composite material and the metal which are two heterogeneous materials.
Through retrieval, the composite cabin and metal piece bonding and positioning device disclosed by the application number of CN201820923463.9 can quickly position the metal piece, can ensure the bonding precision and can ensure the form and position tolerance of the final product.
However, the above structure has the following disadvantages: the fixed cartridge of direct positioning can't be carried out according to the extrusion structure to the adjustment position that need relapse during the installation, needs loaded down with trivial details operation just to dismantle after the installation accessory and takes off, and the practicality is lower, and consequently inconvenient use is made the improvement to above-mentioned problem.
SUMMERY OF THE UTILITY MODEL
In order to achieve the purpose, the technical scheme adopted by the utility model is that the utility model provides a servo cabin metal piece bonding and positioning structure, which comprises a base piece and a fixed jacket layer, wherein the fixed jacket layer is provided with a connecting structure;
the connection structure includes: the inner layer plate, the adhesion layer, the top groove, the notch and the fixing part are arranged on the outer side of the inner layer plate;
the inner plate is fixed jacket layer inner wall, the adhesion layer is fixed inner plate bottom surface and paste the connection and be in on the basis piece, the top groove is opened fixed jacket layer top, the opening is opened in the top groove, the fixed part sets up on the fixed jacket layer.
Further, the fixing portion includes: the device comprises a fixing block, a limiting groove, a through hole, a screw, a fixing nut and a screwing block;
the fixed block is fixed jacket layer outer wall, the spacing groove is opened fixed block side end face, the through-hole is opened the spacing inslot, the screw rod suit is in the through-hole, fixing nut revolves soon to be connected screw rod both ends and suit are in the spacing inslot, it fixes to revolve wrong the piece on the screw rod.
Preferably, the screwing block adopts a hexagonal structure.
Preferably, the fixing sleeve layer and the inner plate are both in a semicircular structure.
Preferably, the whole fixed sleeve layer is in a truncated cone-shaped structure with a narrow top and a wide bottom after being spliced.
Compared with the prior art, the utility model discloses an advantage lies in with positive effect, is provided with two semicircular structure's fixed jacket layer, inside be provided with basic piece size assorted inner plate, the suit is on basic piece and through adhesion layer fixed position after the concatenation, and the effect of correcting the location can be played to the easy to assemble metalwork, and after the installation was accomplished, detachable connection structure separated to open and taken off, convenient to use easy operation, and the practicality is strong.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive labor.
Fig. 1 is a schematic structural view of a positioning structure for adhering a metal piece in a servo compartment according to this embodiment;
FIG. 2 is a sectional top view of a metal part bonding and positioning structure of a servo compartment provided in this embodiment;
shown in the figure: 1. a base member; 2. fixing the jacket layer; 3. an inner layer board; 4. an adhesion layer; 5. a top groove; 6. opening the gap; 7. a fixed block; 8. a limiting groove; 9. a through hole; 10. a screw; 11. fixing a nut; 12. and (5) screwing the block.
Detailed Description
In order to make the above objects, features and advantages of the present invention more clearly understood, the present invention will be further described with reference to the accompanying drawings and examples. It should be noted that the embodiments and features of the embodiments of the present application may be combined with each other without conflict.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, however, the present invention may be practiced in other ways than those specifically described herein, and therefore the present invention is not limited to the limitations of the specific embodiments of the present disclosure.
In the embodiment, as can be seen from fig. 1-2 in the specification, the adhering and positioning structure for the metal piece of the servo cabin comprises a base piece 1 and a fixed sleeve layer 2, wherein a connecting structure is arranged on the fixed sleeve layer 2;
the connection structure includes: the inner layer plate 3, the adhesion layer 4, the top groove 5, the notch 6 and the fixing part;
inner plate 3 is fixed 2 inner walls on fixed jacket layer, adhesion layer 4 is fixed 3 bottom surfaces of inner plate and paste the connection and be in on the basis spare 1, top groove 5 is opened fixed 2 tops on the jacket layer, opening 6 is in top groove 5, the fixed part sets up fixed jacket layer 2 is last.
The fixing portion includes: the device comprises a fixing block 7, a limiting groove 8, a through hole 9, a screw rod 10, a fixing nut 11 and a screwing block 12;
From the above, it can be seen that: the screwing block 12 is of a hexagonal structure, and is convenient to screw by using a wrench.
From the above, it can be seen that: the fixed jacket layer 2 and the inner-layer plate 3 are both of a semicircular structure, and the cross section of the spliced inner-layer plate is of an annular structure, so that the sheathing effect is achieved.
From the above, it can be seen that: the whole round platform shape structure that is narrow on the top wide down after the fixed jacket layer 2 concatenation, the bottom sprag is more stable.
It is important to point out that, in the specific implementation process, the connected fixing sleeve layer 2 is sleeved on the base member 1 and is adhered and fixed through the adhesion layer 4 on the bottom surface of the inner plate 3, then an external member is installed, after the correction and installation are completed, the screwing block 12 is screwed, the fixing screw cap 11 is detached and taken out from the two ends of the screw rod 10, and then the fixing sleeve layer 2 is detached.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in other forms, and any person skilled in the art may use the above-mentioned technical contents to change or modify the equivalent embodiment into equivalent changes and apply to other fields, but any simple modification, equivalent change and modification made to the above embodiments according to the technical matters of the present invention will still fall within the protection scope of the technical solution of the present invention.
Claims (5)
1. A servo cabin metal piece bonding and positioning structure comprises a base piece (1) and a fixed sleeve layer (2), and is characterized in that a connecting structure is arranged on the fixed sleeve layer (2);
the connection structure includes: the inner layer plate (3), the adhesion layer (4), the top groove (5), the notch (6) and the fixing part;
inner plate (3) are fixed jacket layer (2) inner wall, adhesion layer (4) are fixed inner plate (3) bottom surface and paste and connect in on basic piece (1), top groove (5) are opened fixed jacket layer (2) top, opening (6) are in top groove (5), the fixed part sets up on fixed jacket layer (2).
2. The adhesion positioning structure for the metal piece of the servo cabin as claimed in claim 1, wherein the fixing portion comprises: the device comprises a fixing block (7), a limiting groove (8), a through hole (9), a screw (10), a fixing nut (11) and a screwing block (12);
fixed block (7) are fixed jacket layer (2) outer wall, spacing groove (8) are opened fixed block (7) side end face, open through-hole (9) in spacing groove (8), screw rod (10) suit is in through-hole (9), fixing nut (11) are twisted and are connected screw rod (10) both ends and suit are in spacing groove (8), it fixes to twist piece (12) on screw rod (10).
3. The servo cabin metal piece bonding and positioning structure is characterized in that the screwing block (12) is of a hexagonal structure.
4. The bonding and positioning structure for the metal pieces of the servo cabin according to claim 1, wherein the fixing sleeve layer (2) and the inner plate (3) are both of a semicircular structure.
5. The bonding and positioning structure for the metal piece of the servo cabin as claimed in claim 1, wherein the fixing sleeve layer (2) is integrally in a truncated cone shape with a narrow top and a wide bottom after being spliced.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223058927.XU CN218801753U (en) | 2022-11-17 | 2022-11-17 | Servo cabin metalwork glues location structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223058927.XU CN218801753U (en) | 2022-11-17 | 2022-11-17 | Servo cabin metalwork glues location structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218801753U true CN218801753U (en) | 2023-04-07 |
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ID=87037695
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223058927.XU Active CN218801753U (en) | 2022-11-17 | 2022-11-17 | Servo cabin metalwork glues location structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218801753U (en) |
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2022
- 2022-11-17 CN CN202223058927.XU patent/CN218801753U/en active Active
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