CN114526667A

CN114526667A - Aviation aluminum product testing arrangement

Info

Publication number: CN114526667A
Application number: CN202210183059.3A
Authority: CN
Inventors: 严泽玉; 张勤; 张烽
Original assignee: Suzhou Tengyida Precision Machinery Co ltd
Current assignee: Suzhou Tengyida Precision Machinery Co ltd
Priority date: 2022-02-27
Filing date: 2022-02-27
Publication date: 2022-05-24

Abstract

The invention relates to the technical field of aluminum product production devices, and discloses an aviation aluminum product testing device which comprises a base, wherein a placing table is fixedly arranged in the middle of the surface of one side of the base, clamping components distributed around the placing table are arranged on the surface of one side of the base, a support with an opening pointing to the U-shaped structure of the base is fixedly arranged on the base, a moving component is arranged on the support and comprises a rotating plate, and a testing component is arranged on the rotating plate. Compared with the prior art, the invention has the beneficial effects that: can carry out comprehensive test to the surface of aluminium product, improve the area of test, and can turn over automatically in the testing process, avoid artifical upset aluminium product, can avoid artifical clamping once more to produce the influence to the test result when improving test speed and efficiency, improve the accuracy of test result, be favorable to the use.

Description

Aviation aluminum product testing arrangement

Technical Field

The invention relates to the technical field of aluminum product production devices, in particular to an aviation aluminum product testing device.

Background

The aluminum product is a general name of living goods and industrial goods which are processed by adopting aluminum alloy as a main raw material, the aluminum alloy is a general name of aluminum-based alloy, main alloy elements comprise copper, silicon, magnesium, zinc and manganese, secondary alloy elements comprise nickel, iron, titanium, chromium, lithium and the like, the aluminum alloy has low density but higher strength which is close to or more than that of high-quality steel, and can be processed into various sections with good plasticity, has excellent electrical conductivity, thermal conductivity and corrosion resistance, is widely used industrially, and is second only to steel in use amount.

The aluminum product needs to be tested for the flatness of the surface of the aluminum product before use, the conventional testing device can only carry out single-side detection on the aluminum product when in use, and the aluminum product needs to be clamped again when another surface is detected, so that the manual workload is increased, the manual secondary clamping can influence the testing result, and the accuracy of the testing result is reduced.

Disclosure of Invention

The invention aims to provide an aviation aluminum product testing device to solve the problems in the background technology.

In order to achieve the purpose, the invention provides the following technical scheme:

the utility model provides an aviation aluminum product testing arrangement, includes the base, and base one side surface middle part fixed mounting has places the platform, base one side surface is provided with around placing the clamping component that the platform distributes, and fixed mounting has the support of the U type structure of the directional base of opening on the base, be provided with on the support and remove the subassembly, remove the subassembly and include the rotor plate, be provided with test component on the rotor plate.

As a further scheme of the invention: the clamping assembly comprises first telescopic pieces, the first telescopic pieces are fixedly mounted on the base and provided with a plurality of groups, the first telescopic pieces are located on two sides of the placing table, the output ends of the first telescopic pieces are fixedly mounted with side plates, and the side plates are jointly provided with clamping frames of frame-shaped structures.

As a further scheme of the invention: the clamping frame is characterized in that connecting columns are fixedly mounted at two ends of the clamping frame, one end, far away from the clamping frame, of each connecting column is rotatably connected with the corresponding side plate, and one end of one connecting column is fixedly connected with a first rotating power part on the corresponding displacement side plate.

As a further scheme of the invention: the inner side of the clamping frame is fixedly provided with a plurality of groups of second telescopic pieces which are distributed at intervals, and the output end of each second telescopic piece is fixedly provided with a clamping plate.

As a further scheme of the invention: the moving assembly comprises a sliding block, the sliding block is slidably mounted on the support, a third telescopic piece is fixedly connected to the side face of the sliding block, and one end, far away from the sliding block, of the third telescopic piece is fixedly connected with the support.

As a further scheme of the invention: and a second rotary power part is fixedly arranged on the surface of the sliding block close to the base, and an output shaft of the second rotary power part is fixedly connected with the rotating plate.

As a further scheme of the invention: the test assembly comprises a slide bar, the slide bar is provided with a plurality of groups and is slidably mounted on a rotating plate, the slide bar penetrates through the rotating plate and is fixedly mounted with a mounting plate together with one end of the slide bar close to the base, and the mounting plate is rotatably mounted with a ball close to the surface of the base.

As a further scheme of the invention: the test assembly further comprises a pressure detection piece which is fixedly installed on the rotating plate and located between the sliding rods, an elastic piece is fixedly installed on the surface, close to the base, of the pressure detection piece, and one end, far away from the pressure detection piece, of the elastic piece is fixedly connected with the installation plate.

Compared with the prior art, the invention has the beneficial effects that: can carry out comprehensive test to the surface of aluminium product, improve the area of test, and can turn over automatically in the testing process, avoid artifical upset aluminium product, can avoid artifical clamping once more to produce the influence to the test result when improving test speed and efficiency, improve the accuracy of test result, be favorable to the use.

Drawings

Fig. 1 is a front view of an aviation aluminum product testing device.

Fig. 2 is an enlarged view at a1 in fig. 1.

Fig. 3 is a schematic structural diagram of a clamping frame in an aviation aluminum product testing device.

Wherein: 1. a base; 2. a placing table; 3. a clamping frame; 4. a first electric telescopic rod; 5. a side plate; 6. connecting columns; 7. a first motor; 8. a second electric telescopic rod; 9. a splint; 10. a support; 11. a slider; 12. a second motor; 13. a rotating plate; 14. a slide bar; 15. mounting a plate; 16. a ball bearing; 17. a spring; 18. a pressure sensor; 19. a third electric telescopic rod; 20. a clamping assembly; 21. a moving assembly; 22. and testing the assembly.

Detailed Description

It should be noted that the embodiments and features of the embodiments may be combined with each other without conflict.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used only for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.

In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.

The present invention will be described in detail below with reference to the embodiments with reference to the attached drawings.

Referring to fig. 1 to 3, a structure diagram of an aviation aluminum product testing device provided in an embodiment of the present invention includes a base 1, a placing table 2 is fixedly installed in a middle portion of a surface of one side of the base 1, clamping assemblies 20 distributed around the placing table 2 are disposed on a surface of one side of the base 1, a support 10 having a U-shaped structure with an opening pointing to the base 1 is fixedly installed on the base 1, a moving assembly 21 is disposed on the support 10, the moving assembly 21 includes a rotating plate 13, and a testing assembly 22 is disposed on the rotating plate 13.

In practical application, the embodiment of the invention places an aluminum product on the placing table 2, then clamps the aluminum product through the clamping assembly 20, drives the aluminum product to move upwards through the clamping assembly 20 after clamping, makes the aluminum product contact with the testing assembly 22 and applies a certain initial pressure to the testing assembly 22, then drives the testing assembly 22 to make comprehensive rolling contact with the aluminum product through the moving assembly 21, the testing assembly 22 judges whether the surface flatness of the aluminum product meets the requirement by detecting the pressure value between the aluminum product and the testing assembly 22, after one side surface test is completed, drives the aluminum product to be far away from the testing assembly 22 through the clamping assembly 20, then turns the aluminum product 180 degrees through the clamping assembly 20, the other surface of the aluminum product can be tested by repeating the steps, thereby realizing comprehensive testing of the surface of the aluminum product and avoiding manual turning of the aluminum product, the test efficiency and the accuracy of the test result are improved, and the use is facilitated.

As shown in fig. 1 and 3, as a preferred embodiment of the present invention, the clamping assembly 20 includes first telescopic members, the first telescopic members are fixedly mounted on the base 1 and are provided with a plurality of sets, the first telescopic members are located on two sides of the placing table 2, the output ends of the first telescopic members are fixedly mounted with side plates 5, and the side plates 5 are provided with clamping frames 3 of a frame structure.

The connecting columns 6 are fixedly mounted at two ends of the clamping frame 3, one end, far away from the clamping frame 3, of each connecting column 6 is rotatably connected with the corresponding side plate 5, and one end of one group of connecting columns 6 is fixedly connected with a first rotating power part on the corresponding displacement side plate 5.

The inner side of the clamping frame 3 is fixedly provided with a plurality of groups of second telescopic pieces which are distributed at intervals, and the output end of each second telescopic piece is fixedly provided with a clamping plate 9.

The embodiment of the utility model provides an when in actual application, thereby it is the same with the central height of aluminium products to drive 3 rebound of clamping frame through first extensible member and make 3 central height of clamping frame and the inboard center height that moves, it can press from both sides tightly aluminium products to drive splint 9 through the second extensible member at last to move to the inboard from making splint 9, later drive aluminium products through first extensible member and rise and contact with test component 22, can drive clamping frame 3 through first rotatory power spare and rotate, thereby make aluminium products upset 180 degrees, thereby can test the another side.

In an example of the present invention, the first extensible member and the second extensible member are the first electric telescopic rod 4 and the second electric telescopic rod 8 respectively, and certainly, other components such as a hydraulic cylinder which can actively change the length can be provided, the clamping frame 3 can be driven by the first electric telescopic rod 4 to perform height adjustment, the clamping plate 9 can be driven by the second electric telescopic rod 8 to clamp the aluminum product, the first rotary power member is the first motor 7, and certainly, other components which can output rotary power such as a hydraulic motor can be provided, and the clamping frame 3 can be driven by the first motor 7 to rotate.

As shown in fig. 1 and fig. 2, as a preferred embodiment of the present invention, the moving assembly 21 includes a sliding block 11, the sliding block 11 is slidably mounted on the bracket 10, and a third telescopic member is fixedly connected to a side surface of the sliding block 11, and one end of the third telescopic member, which is far away from the sliding block 11, is fixedly connected to the bracket 10.

The surface of the sliding block 11 close to the base 1 is fixedly provided with a second rotating power piece, and an output shaft of the second rotating power piece is fixedly connected with the rotating plate 13.

The testing assembly 22 comprises a sliding rod 14, a plurality of groups of sliding rods 14 are arranged on the rotating plate 13 in a sliding mode, the sliding rods 14 penetrate through the rotating plate 13, a mounting plate 15 is fixedly mounted at one end, close to the base 1, of each sliding rod 14, and a ball 16 is rotatably mounted on the surface, close to the base 1, of each mounting plate 15.

The testing assembly 22 further comprises a pressure detecting member, the pressure detecting member is fixedly mounted on the rotating plate 13 and located between the sliding rods 14, an elastic member is fixedly mounted on the surface of the pressure detecting chamber close to the base 1, and one end of the elastic member far away from the pressure detecting member is fixedly connected with the mounting plate 15.

In practical application of the embodiment of the present invention, the first expansion piece drives the aluminum product to move upward and contact with the ball 16, and then the ball 16 is pushed to move upward and compress the elastic piece through the mounting plate 15, so that the pressure detection piece has a certain initial reading, the second power piece drives the rotation plate 13 to rotate back and forth in the range of the aluminum product, the rotation plate 13 rotates back and forth to drive the ball 16 to roll on the surface of the aluminum product, when the surface flatness of the aluminum product is low or the aluminum product is bent and deformed, the ball 16 rolls on the surface of the aluminum product to extend or continue to compress the elastic piece, so that the reading of the pressure detection piece changes, if the reading change range of the pressure detection piece is greater than a set threshold value, the aluminum product is unqualified, the third expansion piece can push the slider 11 to move, so that the slider 11 can drive the test component 22 to move, and then realize the comprehensive test to aluminium product surface, make aluminium product keep away from ball 16 after the single face test is accomplished, then drive aluminium product upset 180 degrees through first rotatory power spare, repeat above-mentioned step and can test the another side to avoided artifical upset aluminium product, improved the accuracy of efficiency of software testing and test result, be favorable to using.

In an example of the present invention, the second rotating power member is the second motor 12, certainly, other members capable of outputting rotating power such as a hydraulic motor can be used, the second motor 12 can drive the rotating plate 13 to rotate in a reciprocating manner, the third extensible member is the third electric telescopic rod 19, certainly, other members capable of actively changing the length such as a hydraulic cylinder can be used, the third electric telescopic rod 19 can drive the slider 11 to move, the elastic member is the spring 17, certainly, other members having elasticity such as a bouncing ball can be used, the pressure detecting member is the pressure sensor 18, and the pressure sensor 18 detects the pressure change of the rolling ball 16 on the aluminum product, so that the surface smooth length of the aluminum product can be reflected.

Although the preferred embodiments of the present patent have been described in detail, the present patent is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present patent within the knowledge of those skilled in the art.

Claims

1. The utility model provides an aviation aluminum product testing arrangement, includes the base, and base one side surface middle part fixed mounting has places the platform, its characterized in that, base one side surface is provided with around placing the clamping component that the platform distributes, and fixed mounting has the support of the U type structure of the directional base of opening on the base, be provided with the removal subassembly on the support, the removal subassembly includes the rotor plate, be provided with test assembly on the rotor plate.

2. The aviation aluminum product testing device of claim 1, wherein the clamping assembly comprises first telescopic members, the first telescopic members are fixedly mounted on the base and provided with multiple groups, the first telescopic members are located on two sides of the placing table, side plates are fixedly mounted at output ends of the first telescopic members, and clamping frames of frame-shaped structures are jointly arranged on the side plates.

3. The aviation aluminum product testing device of claim 2, wherein connecting columns are fixedly mounted at both ends of the clamping frame, one ends of the connecting columns, which are far away from the clamping frame, are rotatably connected with the side plates, and one ends of one group of the connecting columns are fixedly connected with first rotating power pieces on the displacement side plates.

4. The aviation aluminum product testing device of claim 3, wherein a plurality of groups of second telescopic members which are distributed at intervals are fixedly arranged on the inner side of the clamping frame, and a clamping plate is fixedly arranged at the output end of each second telescopic member.

5. The aviation aluminum product testing device of claim 1, wherein the moving assembly comprises a sliding block, the sliding block is slidably mounted on the support, a third telescopic member is fixedly connected to the side face of the sliding block, and one end, far away from the sliding block, of the third telescopic member is fixedly connected with the support.

6. The aviation aluminum product testing device of claim 5, wherein a second rotating power part is fixedly mounted on the surface of the sliding block close to the base, and an output shaft of the second rotating power part is fixedly connected with the rotating plate.

7. The aviation aluminum product testing device of claim 6, wherein the testing assembly comprises a plurality of sets of sliding rods which are slidably mounted on the rotating plate, the sliding rods penetrate through the rotating plate, one ends of the sliding rods, close to the base, are fixedly mounted with a mounting plate, and the surface of the mounting plate, close to the base, is rotatably mounted with a ball.

8. The aviation aluminum product testing device of claim 7, wherein the testing assembly further comprises a pressure detecting member, the pressure detecting member is fixedly mounted on the rotating plate and located between the sliding rods, an elastic member is fixedly mounted on the surface of the pressure detecting chamber close to the base, and one end of the elastic member far away from the pressure detecting member is fixedly connected with the mounting plate.