CN217343011U - Titanium plate integrated into one piece structure - Google Patents
Titanium plate integrated into one piece structure Download PDFInfo
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- CN217343011U CN217343011U CN202221942847.8U CN202221942847U CN217343011U CN 217343011 U CN217343011 U CN 217343011U CN 202221942847 U CN202221942847 U CN 202221942847U CN 217343011 U CN217343011 U CN 217343011U
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
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Abstract
The utility model provides a titanium plate integrated forming structure, which comprises a plurality of groups of forming units formed by continuously bending plates, wherein the forming units are sequentially stacked along the same horizontal plane to form the integrated forming structure; every two adjacent groups of the forming units are fixedly connected; each group of forming units comprises a plurality of continuous annular units which are stacked along the same horizontal plane; the annular unit is of a closed annular body structure, and a hollow cavity is arranged inside the annular body; every two adjacent annular units are fixedly connected. The utility model is used for it is extravagant, improve shaping efficiency and shaping intensity to reduce panel clout.
Description
Technical Field
The utility model relates to a titanium panel shaping technical field, concretely relates to titanium panel integrated into one piece structure.
Background
The titanium plate forming structure is widely applied to the fields of military industry, aerospace, biological refrigeration, electronic equipment and the like. At present, common titanium plate forming structures have honeycomb structures and cylindrical tank body structures, all need to be cut by titanium plates to prepare single shape units and then combined and spliced, the production process is relatively complex, and the waste of excess material cost is high. In addition, a plurality of shape units are spliced into a combined structure, so that the bonding strength of the combined structure is easily reduced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a titanium plate material integrated into one piece structure for it is extravagant, improve shaping efficiency and shaping intensity to reduce panel clout. The specific technical scheme is as follows:
an integrated forming structure of a titanium plate comprises a plurality of groups of forming units which are formed by continuously bending the plate, wherein all the forming units are sequentially stacked along the same horizontal plane to form the integrated forming structure; every two adjacent groups of the forming units are fixedly connected;
each group of forming units comprises a plurality of continuous annular units which are stacked along the same horizontal plane; the annular unit is of a closed annular body structure, and a hollow cavity is arranged inside the annular body; every two adjacent annular units are fixedly connected.
In some embodiments, the structural dimensions of each two adjacent sets of the shaped units are the same or different.
In some embodiments, a filler layer is disposed in each of the annular cells; the filling layer is arranged in a hollow cavity of an annular body of the annular unit.
In some embodiments, the filler layer comprises any one of a polyurethane layer and an aluminum silicate ceramic layer.
In some embodiments, the sheet material is a titanium sheet material.
In some embodiments, the titanium plate has a width of 10 to 30mm and a thickness of 0.3 to 3 mm.
Use the technical scheme of the utility model, following beneficial effect has at least:
(1) the utility model discloses in titanium plate integrated into one piece structure stacks gradually the setting through each constitutive unit by panel bending forming along same horizontal plane and constitutes the integrated into one piece structure, has reduced that the panel clout is extravagant, simultaneously, is also convenient for improve shaping efficiency. Every adjacent two sets of be fixed connection between the shaping unit, and be fixed connection between every two adjacent annular units, be convenient for improve shaping intensity.
(2) The utility model discloses in titanium sheet material integrated into one piece structure, the panel of adoption are the titanium sheet material, can satisfy the demand to the material lightweight. Simultaneously, according to the actual use scene, the utility model discloses the titanium sheet bending that can select different thickness and width makes titanium sheet integrated into one piece structure.
(3) The utility model discloses in adopt every adjacent two sets of the structure size of shaping unit is the same or different, is convenient for satisfy actual shaping demand.
(4) The utility model discloses in through setting up the filling layer, be used for satisfying titanium panel integrated into one piece structure heat preservation thermal-insulated demand.
In addition to the above-described objects, features and advantages, the present invention has other objects, features and advantages. The present invention will be described in further detail with reference to the drawings.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the invention and do not constitute a limitation on the invention. In the drawings:
fig. 1 is a schematic structural view of an integral forming structure of a titanium plate in embodiment 1 of the present invention (a filling layer is not shown in the figure, the arrow direction indicates the bending forming direction of the plate, and only a part of the forming structure is shown);
fig. 2 is a schematic structural view of an integral forming structure of a titanium plate in embodiment 2 of the present invention (a filling layer is not shown in the figure, the arrow direction indicates the bending forming direction of the plate, and only a part of the forming structure is shown);
FIG. 3 is a schematic perspective view of the titanium plate of FIG. 1 (only the first and second forming units are shown);
FIG. 4 is a schematic perspective view of the titanium plate integrally formed structure in FIG. 2 (only the first set of forming units are shown);
wherein, 1, titanium plate.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art all belong to the protection scope of the present invention.
Example 1:
referring to fig. 1 and 3, an integrally formed structure of titanium plate comprises a plurality of forming units formed by continuously bending a plate, wherein the forming units are sequentially stacked along the same horizontal plane to form an integrally formed structure; the contact parts between every two adjacent groups of the forming units are welded, so that the stability of the integrally formed structure is ensured;
each group of forming units comprises two continuous annular units which are stacked along the same horizontal plane; the annular unit is of a closed annular body structure, and a hollow cavity is arranged inside the annular body; the contact position between every two adjacent annular units is welded, so that the stability of the integrally formed structure is ensured.
According to the direction of bending and forming the plate, sequentially marking each forming unit as a first forming unit, a second forming unit until the last forming unit, and marking the last forming unit as an Nth forming unit, wherein the value of N is not less than 2.
The structural sizes (representing the annular body length and the annular body width of the annular body structure of each annular unit in each composition unit) of every two adjacent groups of the forming units are different. Specifically, the structural size of the odd-numbered forming units is larger than that of the even-numbered forming units, so that the requirement of using the odd-numbered forming units as the thermal insulation layer of the airplane shell is met.
It should be noted that the size difference between the structure size of the odd-numbered forming units and the structure size of the even-numbered forming units can be specifically adjusted according to different application scenarios.
A filling layer is arranged in each annular unit; the filling layer is arranged in a hollow cavity of an annular body of the annular unit.
The filling layer is an aluminum silicate ceramic layer.
The plate is a titanium plate 1.
The width of the titanium plate 1 is 10mm, and the thickness is 3 mm.
The titanium plate 1 integrally molded structure prepared in example 1 is applied to an aircraft casing, and is particularly used as a high-strength lightweight heat insulating layer.
Example 2:
referring to fig. 2 and 4, an integral forming structure of titanium plate includes a plurality of forming units formed by continuously bending a plate, wherein the forming units are sequentially stacked along a same horizontal plane to form an integral forming structure; the contact parts of every two adjacent groups of the forming units are welded, so that the stability of the integrally formed structure is ensured;
each group of the forming units comprises two continuous annular units which are stacked along the same horizontal plane; the annular unit is of a closed annular body structure, and a hollow cavity is arranged inside the annular body; the contact position between every two adjacent annular units is welded, so that the stability of the integrally formed structure is ensured.
The two adjacent groups of the forming units have the same structure size, so that the stability of the structure is improved conveniently, and the standardization of application in a specific scene is realized conveniently.
A filling layer is arranged in each annular unit; the filling layer is arranged in a hollow cavity of an annular body of the annular unit.
The filling layer is a polyurethane layer.
The plate is a titanium plate 1.
The width of the titanium plate 1 is 30mm, and the thickness of the titanium plate is 0.3 mm.
The titanium plate 1 integrally formed structure prepared in embodiment 1 is applied to a refrigeration heat-insulation shell, and is particularly used as a high-strength light heat-insulation layer.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. 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. An integrated forming structure for titanium plates is characterized by comprising a plurality of groups of forming units formed by continuously bending the plates, wherein all the forming units are sequentially stacked along the same horizontal plane to form the integrated forming structure; every two adjacent groups of the forming units are fixedly connected;
each group of forming units comprises a plurality of continuous annular units which are stacked along the same horizontal plane; the annular unit is of a closed annular body structure, and a hollow cavity is arranged inside the annular body; every two adjacent annular units are fixedly connected.
2. The titanium plate integral molding structure as claimed in claim 1, wherein the structural dimensions of each two adjacent sets of said molding units are the same or different.
3. The titanium plate integrated molding structure according to claim 1, wherein a filling layer is provided in each of the annular units; the filling layer is arranged in a hollow cavity of an annular body of the annular unit.
4. The titanium plate integrated structure according to claim 3, wherein said filler layer comprises any one of a polyurethane layer and an aluminum silicate ceramic layer.
5. The titanium plate integrated structure according to any one of claims 1 to 4, wherein said plate is a titanium plate.
6. The titanium plate integrated molding structure as claimed in claim 5, wherein the titanium plate has a width of 10-30mm and a thickness of 0.3-3 mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202221942847.8U CN217343011U (en) | 2022-07-27 | 2022-07-27 | Titanium plate integrated into one piece structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202221942847.8U CN217343011U (en) | 2022-07-27 | 2022-07-27 | Titanium plate integrated into one piece structure |
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CN217343011U true CN217343011U (en) | 2022-09-02 |
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CN202221942847.8U Active CN217343011U (en) | 2022-07-27 | 2022-07-27 | Titanium plate integrated into one piece structure |
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2022
- 2022-07-27 CN CN202221942847.8U patent/CN217343011U/en active Active
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