Aviation part plane detection device

Abstract

The utility model discloses a plane detection device for aviation parts, relates to the field of aviation parts, solves the problem that the conventional device is difficult to monitor the plane of a transmitted part according to corresponding specifications according to requirements, and adopts the following scheme that the plane detection device comprises a detection frame and a transmission assembly on the outer side of the detection frame, a display screen and a measuring light curtain are fixedly mounted at the top of the detection frame; a side table located on the outer side of the top face of the conveying assembly is arranged in the detection frame. An adjusting assembly is fixedly mounted at the top of the side table and comprises a lower driving assembly and an upper driving assembly which are sleeved in a sliding manner; according to the plane detection device for the aeronautical parts, through the arrangement of each assembly in the adjusting assembly on the detection frame, a micro motor and an electric cylinder seat in the adjusting assembly can be arranged to drive a suction cup seat to the position above the parts on the conveying assembly, and a micro air pump drives the suction cup seat to suck the parts and adjust the parts to the corresponding positions; and the upper display screen and the measuring light curtain are matched to carry out plane detection on parts below.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation parts, in particular to a plane detection device for aviation parts. Background Art

[0002] Aviation materials are the material guarantee for the development and production of aviation products, and are also the technical basis for aviation products to achieve the performance, service life and reliability that people expect. Due to the basic status of aviation materials and their increasing contribution to aviation products, aviation materials have become one of the three major aviation key technologies alongside aviation engines and information technology. Because aviation is so important, aviation material testing is also extremely strict. When testing aviation materials, flatness testing devices are used;

[0003] After searching, the application with patent application number CN202320831320.6 discloses a plane detection device for aviation parts, including two square plates, the inner wall of each of the square plates is threadedly connected with a threaded shaft, the ends of the two threaded shafts close to each other are fixedly connected with an extrusion plate, and the upper surface of each square plate is fixedly connected with a rectangular plate, and the front of one of the rectangular plates is fixedly connected with two groups of first long plates, and the left side of each group of first long plates is provided with two circular through holes, and the side of each group of first long plates away from each other is provided with a slide groove, and the inside of each slide groove is slidably connected with a slider, and the side of each group of sliders away from each other is fixedly connected with a second long plate, and the back of another rectangular plate is fixedly connected with a telescopic rod; the utility model makes the area of ​​the first long plate overlap with the second long plate by sliding the slider inside the slide groove, so as to effectively avoid the problem that the plane detection device is not easy to carry due to its large size;

[0004] The above application document realizes the detection of parts by setting up a single measuring light curtain detection component. However, in the process of parts production, it is necessary to perform planar detection on the same parts, and how to perform unified detection efficiently becomes a problem that needs to be solved urgently.

[0005] Therefore, we propose a plane detection device for aviation parts. Utility Model Content

[0006] In view of the deficiencies of the prior art, the utility model provides an aviation component plane detection device, which solves the problem that the prior devices are difficult to monitor the corresponding specifications of the plane of the transmitted component according to the requirements.

[0007] To achieve the above objectives, the utility model is implemented through the following technical solutions: an aviation component plane detection device, including a detection frame and a transmission component on its outer side, a display screen is fixedly installed on the top of the detection frame, and a measuring light curtain connected to the display screen is also installed on the detection frame;

[0008] The detection frame is provided with a side platform located outside the top surface of the conveying component;

[0009] An adjustment assembly is fixedly installed on the top of the side platform, and the adjustment assembly includes a lower drive assembly and an upper drive assembly of a sliding sleeve;

[0010] The main body of the lower driving assembly is a micro motor fixedly mounted on the top of the side platform, and the top end of the micro motor is fixedly connected to the bottom slide;

[0011] The main body of the upper driving component is an electric cylinder seat, the outer end of the output shaft of the electric cylinder seat is fixedly connected to a top slide, a micro air pump is fixedly installed on the top of the top slide, and a suction cup seat for the output end of the micro air pump is provided at the bottom of the top slide.

[0012] Preferably, the conveying assembly is provided with a belt group driven by a driving roller, and components distributed at intervals and located below the suction cup seat are placed on the top surface of the belt group;

[0013] Among them, the setting of the belt group can output multiple groups of parts, and combined with the setting of the upper detection frame and the adjustment components thereon, corresponding plane monitoring of multiple groups of parts can be performed.

[0014] Preferably, a semicircular groove is provided at the top of the outer end surface of the bottom slide, and a slide card having a size matching the semicircular groove is fixedly installed at the bottom of the outer end of the top slide;

[0015] The bottom slide and the top slide can be driven by the upper drive assembly to adjust the lateral position of the suction cup seat, so as to adjust the position of the component to be tested accordingly.

[0016] Preferably, the top slide is slidably mounted on the bottom slide, and the thickness of the outer end plates of the top slide and the bottom slide are both half the thickness of the top plate;

[0017] Among them, the provision of the top slide and the bottom slide can increase its stability during adjustment.

[0018] Preferably, a slide column is fixedly mounted on the outer wall of the electric cylinder seat, and a slide groove matching the specifications of the slide column is opened on the top of the rear side surface of the side platform.

[0019] The utility model provides a plane detection device for aviation parts, which has the following beneficial effects:

[0020] The aircraft component plane detection device, through the setting of each component in the adjustment component on the detection frame, can drive the suction cup seat to the top of the component on the transmission component through the setting of the micro motor and the electric cylinder seat in the adjustment component, and the suction cup seat is driven by a micro air pump to adsorb the component and adjust it to the corresponding position, and cooperates with the upper display screen and the measuring light curtain to perform plane detection on the component below to ensure the detection accuracy, thereby solving the problem that the existing device is difficult to monitor the corresponding specifications of the plane of the transmitted component according to the demand. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 It is a structural schematic diagram of the utility model;

[0022] Figure 2 This is a schematic diagram of the structure of the detection frame of the utility model;

[0023] Figure 3 It is a structural schematic diagram of the adjustment component of the utility model;

[0024] Figure 4 It is a structural schematic diagram of the upper drive assembly of the utility model;

[0025] Figure 5 It is a structural schematic diagram of the lower drive assembly of the utility model.

[0026] In the figure: 1. detection frame; 11. side stage; 12. slide; 13. display screen; 14. measuring light curtain; 2. transmission component; 3. adjustment component; 31. lower drive component; 311. micro motor; 312. bottom slide; 32. upper drive component; 321. micro air pump; 322. suction cup seat; 323. electric cylinder seat; 324. slide column; 325. top slide. DETAILED DESCRIPTION

[0027] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0028] See also Figure 1-5The embodiment of the utility model provides a technical solution: a plane detection device for aviation parts, comprising a detection frame 1 and a transmission component 2 on its outer side, a display screen 13 is fixedly installed on the top of the detection frame 1, and a measuring light curtain 14 connected to the display screen 13 is also installed on the detection frame 1; a side platform 11 located on the outer side of the top surface of the transmission component 2 is arranged in the detection frame 1; an adjustment component 3 is fixedly installed on the top of the side platform 11, and the adjustment component 3 includes a lower drive component 31 and an upper drive component 32 of a sliding set; the main body of the lower drive component 31 is a micro motor 311 fixedly installed on the top of the side platform 11, and the top of the micro motor 311 is fixedly connected to a bottom slide 312; the main body of the upper drive component 32 is an electric cylinder seat 323, and the outer end of the output shaft of the electric cylinder seat 323 is fixedly connected to a top slide 325, a micro air pump 321 is fixedly installed on the top of the top slide 325, and a suction cup seat 322 for the output end of the micro air pump 321 is arranged at the bottom of the top slide 325;

[0029] Among them, the aircraft parts plane detection device, through the setting of each component in the adjustment component 3 on the detection frame 1, can drive the suction cup seat 322 to the top of the parts on the transmission component 2 by the setting of the micro motor 311 and the electric cylinder seat 323 in the adjustment component 3, and the suction cup seat 322 is driven by the micro air pump 321 to adsorb the parts and adjust them to the corresponding position, and cooperate with the upper display screen 13 and the measuring light curtain 14 to perform plane detection on the parts below to ensure the detection accuracy, thereby solving the problem that the existing device is difficult to monitor the corresponding specifications of the plane of the transmitted parts according to the needs.

[0030] Embodiment 2:

[0031] A belt group driven by a driving roller is provided in the conveying component 2, and parts are placed on the top surface of the belt group in an interval distribution and located below the suction cup seat 322; wherein, the setting of the belt group can output multiple groups of parts, and cooperate with the setting of the upper detection frame 1 and the adjustment component 3 thereon, so as to perform corresponding plane monitoring on multiple groups of parts.

[0032] A semicircular groove is provided at the top of the outer end surface of the bottom slide 312, and a slide card with a specification matching the semicircular groove is fixedly installed at the bottom of the outer end of the top slide 325; wherein, the bottom slide 312 and the top slide 325 can be driven by the upper drive assembly 32 to adjust the lateral position of the suction cup seat 322, so as to facilitate the corresponding adjustment of the position of the parts to be tested.

[0033] The top slide 325 is slidably mounted on the bottom slide 312, and the thickness of the outer end plates of the top slide 325 and the bottom slide 312 are both half of the thickness of the top plate; wherein, the arrangement of the top slide 325 and the bottom slide 312 can increase their stability during adjustment.

[0034] A slide post 324 is fixedly mounted on the outer wall of the electric cylinder seat 323 , and a slide groove 12 matching the specification of the slide post 324 is opened on the top of the rear side surface of the side platform 11 .

[0035] The working principle and use process of the utility model are as follows: when the device is required to work, the transmission component 2 outputs the component to be detected. When it is under the measuring light curtain 14, the micro motor 311 drives the suction cup seat 322 to the top of the component, and then the electric cylinder seat 323 is opened to drive the suction cup seat 322 to the top of the center of the component. Finally, the micro air pump 321 is opened to use the suction cup seat 322 to absorb the component on the bottom side and place it at the center of the bottom side of the measuring light curtain 14 to ensure the accuracy of the detection result.

[0036] The above shows and describes the basic principles and main features of the utility model and the advantages of the utility model. For those skilled in the art, it is obvious that the utility model is not limited to the details of the above exemplary embodiments, and can be implemented in other specific forms without departing from the spirit or basic features of the utility model. Therefore, no matter from which point of view, the embodiments should be regarded as exemplary and non-restrictive. The scope of the utility model is limited by the attached claims rather than the above description, and it is intended to include all changes within the meaning and scope of the equivalent elements of the claims. Any figure mark in the claims should not be regarded as limiting the claims involved.

[0037] In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.

Claims

1. An aviation component plane detection device, comprising a detection frame (1) and a transmission assembly (2) outside the detection frame (1), a display screen (13) being fixedly mounted on the top of the detection frame (1), and a measuring light curtain (14) connected to the display screen (13) being also mounted on the detection frame (1); Features: The detection frame (1) is provided with a side platform (11) located outside the top surface of the transmission component (2); An adjustment component (3) is fixedly mounted on the top of the side platform (11), and the adjustment component (3) comprises a lower drive component (31) and an upper drive component (32) which are slidably mounted. The main body of the lower driving assembly (31) is a micro motor (311) fixedly mounted on the top of the side platform (11), and the top end of the micro motor (311) is fixedly connected to a bottom slide platform (312); The main body of the upper driving component (32) is an electric cylinder seat (323), the outer end of the output shaft of the electric cylinder seat (323) is fixedly connected to a top slide (325), a micro air pump (321) is fixedly installed on the top of the top slide (325), and a suction cup seat (322) which is the output end of the micro air pump (321) is arranged at the bottom of the top slide (325).

2. The aircraft component plane detection device according to claim 1, characterized in that: The conveying assembly (2) is provided with a belt group driven by a driving roller, and components distributed at intervals and located below the suction cup seat (322) are placed on the top surface of the belt group.

3. The plane detection device for aviation parts according to claim 1, characterized in that: A semicircular groove is formed at the top of the outer end surface of the bottom slide (312), and a slide card having a size matching the semicircular groove is fixedly mounted at the bottom of the outer end of the top slide (325).

4. The aircraft component plane detection device according to claim 3, characterized in that: The top slide (325) is slidably mounted on the bottom slide (312), and the thickness of the outer end plates of the top slide (325) and the bottom slide (312) are both half the thickness of the top plate.

5. The aircraft component plane detection device according to claim 4, characterized in that: A slide post (324) is fixedly mounted on the outer wall of the electric cylinder seat (323), and a slide groove (12) matching the specifications of the slide post (324) is provided on the top of the rear side surface of the side platform (11).

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