CN220626552U - Multimode airborne avionics tester convenient to install - Google Patents

Abstract

The utility model discloses a multimode airborne avionics tester convenient to install, which comprises a bottom plate, wherein the upper surface of the bottom plate is fixedly connected with a positioning seat, the inside of the positioning seat is clamped with a clamping column, the upper surface of the clamping column is fixedly connected with a positioning plate, the upper surface of the positioning plate is fixedly connected with a tester body, the upper surface of the bottom plate is provided with symmetrical positioning grooves, the bottom surface of the positioning plate is fixedly connected with symmetrical support columns, the bottom ends of the two support columns are fixedly connected with first magnet sheets, and the inner bottom wall of each positioning groove is fixedly connected with a second magnet sheet. This device is through the inside of going into the card post card positioning seat, reaches the effect to the preliminary location of tester body, utilizes the cooperation of support column and constant head tank, makes things convenient for the staff tester to fix a position, through the mutual attraction of first magnet piece and second magnet piece, can make the support column stable, further makes things convenient for the staff to install the tester body.

Description

Multimode airborne avionics tester convenient to install

Technical Field

The utility model relates to the field of multimode electromechanical testers, in particular to a multimode airborne avionic tester convenient to install.

Background

In the multi-mode wire stretcher, the wire continuously passes through the dies continuously and simultaneously during drawing, a winch is arranged between every two dies, the wire is wound on the dies with a certain number of turns, and thereby drawing force is established. According to the relation between the motion speed of the wire and the winch during drawing, the multimode continuous wire stretcher can be divided into a sliding multimode continuous wire stretcher and a non-sliding multimode continuous wire stretcher.

The multimode airborne avionics tester is characterized in that a tester is required to be used for testing before the multimode machine runs, most of the existing multimode airborne avionics tester is installed and fixed through a plurality of bolts when installed, the installation and the disassembly are troublesome, the working efficiency of workers is reduced, and therefore, the multimode airborne avionics tester convenient to install is provided for solving the problems.

Disclosure of Invention

The utility model aims to provide a multimode airborne avionic tester convenient to install, so as to solve the problems in the background technology.

In order to achieve the above purpose, the present utility model provides the following technical solutions:

the utility model provides a multimode airborne avionics tester convenient to installation, includes the bottom plate, the last fixed surface of bottom plate is connected with the positioning seat, the inside joint of positioning seat has the card post, the last fixed surface of card post is connected with the locating plate, the last fixed surface of locating plate is connected with the tester body, symmetrical constant head tank has been seted up to the upper surface of bottom plate, the bottom surface fixedly connected with symmetrical support column of locating plate, two equal fixedly connected with first magnet piece in bottom of support column, every the equal fixedly connected with second magnet piece of inner bottom wall of constant head tank, the through-hole has been seted up to the front of positioning seat, the screw hole has been seted up in the front of card post, the inner wall threaded connection of screw hole has positioning screw.

In a further embodiment, the front end of the positioning screw is fixedly connected with a rotating block, and the outer surface of the rotating block is fixedly connected with a symmetrical rotating rod.

In a further embodiment, the front and rear sides of the clamping column are fixedly connected with fixed curved bars, and the top ends of the two fixed curved bars are fixedly connected with the bottom surface of the positioning plate.

In a further embodiment, a side surface of the first magnet piece and a side surface of the second magnet piece, which are close to each other, are heteropolar surfaces, and threads matched with the outer surface of the positioning screw rod of the inner wall of the threaded hole are formed.

In a further embodiment, the outer surface of the bottom plate is fixedly connected with supporting legs which are arranged at equal intervals, and the bottom end of each supporting leg is fixedly connected with an anti-slip seat.

In a further embodiment, a positioning rod is fixedly connected to a side surface of each supporting leg, which is close to each other, and the top end of each positioning rod is fixedly connected to the bottom surface of the bottom plate.

Compared with the prior art, the utility model has the beneficial effects that:

this device is through the inside of going into the positioning seat to card post card, reaches the effect to the preliminary location of tester body, utilizes the cooperation of support column and constant head tank, makes things convenient for the staff tester to fix a position, through the mutual attraction of first magnet piece and second magnet piece, can make the support column stable, easy operation, further makes things convenient for the staff to install the tester body, rotates positioning screw through rotatory piece, reaches the effect to card post fastening, strengthens the stability of tester body, improves staff's work efficiency.

Drawings

Fig. 1 is a schematic perspective view of a multimode airborne avionics tester for ease of installation.

FIG. 2 is a cross-sectional view of a front view of a base plate in a multimode airborne avionics tester for ease of installation.

FIG. 3 is a cross-sectional view of a side view of a positioning socket in a multimode airborne avionics tester for ease of installation.

FIG. 4 is an enlarged schematic view of the multimode airborne avionics tester of FIG. 3 at A for ease of installation.

In the figure: 1. a bottom plate; 2. a positioning seat; 3. a clamping column; 4. a positioning plate; 5. a tester body; 6. a support column; 7. a positioning groove; 8. a first magnet piece; 9. a second magnet piece; 10. a through hole; 11. a threaded hole; 12. positioning a screw; 13. a rotating block; 14. a rotating rod; 15. fixing the bent rod; 16. support legs; 17. an antiskid base; 18. and a positioning rod.

Detailed Description

In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first", "a second", etc. may explicitly or implicitly include one or more such feature. In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more.

In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art in a specific case.

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-4, in the utility model, a multimode airborne avionics tester convenient to install comprises a bottom plate 1, wherein the upper surface of the bottom plate 1 is fixedly connected with a positioning seat 2, the inside of the positioning seat 2 is clamped with a clamping column 3, the upper surface of the clamping column 3 is fixedly connected with a positioning plate 4, the upper surface of the positioning plate 4 is fixedly connected with a tester body 5, the upper surface of the bottom plate 1 is provided with symmetrical positioning grooves 7, the bottom surface of the positioning plate 4 is fixedly connected with symmetrical support columns 6, the bottom ends of the two support columns 6 are fixedly connected with first magnet sheets 8, the inner bottom wall of each positioning groove 7 is fixedly connected with second magnet sheets 9, the front surface of the positioning seat 2 is provided with a through hole 10, the front surface of the clamping column 3 is provided with a threaded hole 11, and the inner wall of the threaded hole 11 is in threaded connection with a positioning screw 12.

The front end fixedly connected with rotatory piece 13 of locating screw 12, the surface fixedly connected with symmetrical rotary rod 14 of rotatory piece 13, the equal fixedly connected with fixed curved bar 15 in front and back two sides of card post 3, the top of two fixed curved bars 15 all is the bottom surface fixed connection with locating plate 4, a side that first magnet piece 8 and second magnet piece 9 are close to each other is the heteropolar, the screw thread rather than the surface looks adaptation of locating screw 12 has been seted up to the inner wall of screw hole 11, through the cooperation of rotatory piece 13 and rotary rod 14, make things convenient for the staff to rotate locating screw 12, improve staff's work efficiency, utilize fixed curved bar 15 to support the locating plate 4 and consolidate, increase the stability of tester body 5.

The supporting legs 16 are fixedly connected with the outer surface of the bottom plate 1, the bottom ends of the supporting legs 16 are fixedly connected with the anti-slip seats 17, one side surface, close to each other, of each supporting leg 16 is fixedly connected with the locating rod 18, the top end of each locating rod 18 is fixedly connected with the bottom surface of the bottom plate 1, the device can be stably placed through the cooperation of the supporting legs 16 and the anti-slip seats 17, sliding of the device is avoided, the effect of reinforcing the supporting legs 16 is achieved through the locating rods 18, and the stability of the device is improved.

The working principle of the utility model is as follows:

when the tester is used, the tester is communicated with a corresponding power supply, then the tester is stably placed at a proper position through the cooperation of the supporting legs 16 and the anti-skid seat 17, when the tester body 5 is required to be installed, the clamping columns 3 are clamped into the positioning seat 2, the preliminary positioning effect of the tester body 5 is achieved, the two supporting columns 6 are clamped into the positioning groove 7 respectively, then the supporting columns 6 are stable through the mutual attraction of the first magnet sheet 8 and the second magnet sheet 9, the tester body 5 is further conveniently installed by workers, the positioning screw 12 is rotated through the rotating block 13, the fastening effect of the clamping columns 3 is achieved, and the stability of the tester body 5 is enhanced.

It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present disclosure describes embodiments, not every embodiment is provided with a separate embodiment, and that this description is provided for clarity only, and that the disclosure is not limited to the embodiments described in detail below, and that the embodiments described in the examples may be combined as appropriate to form other embodiments that will be apparent to those skilled in the art.

Claims (6)

1. Multimode airborne avionics tester convenient to installation, its characterized in that: including bottom plate (1), the upper surface fixedly connected with positioning seat (2) of bottom plate (1), the inside joint of positioning seat (2) has draw-in column (3), the upper surface fixedly connected with locating plate (4) of draw-in column (3), the upper surface fixedly connected with tester body (5) of locating plate (4), symmetrical constant head tank (7) have been seted up to the upper surface of bottom plate (1), the bottom surface fixedly connected with symmetrical support column (6) of locating plate (4), two equal fixedly connected with first magnet piece (8) in bottom of support column (6), every the equal fixedly connected with second magnet piece (9) of interior bottom wall of constant head tank (7), through-hole (10) have been seted up in the front of positioning seat (2), threaded hole (11) have been seted up in the front of draw-in column (3), the inner wall threaded connection of screw hole (11) has positioning screw (12).

2. A multimode airborne avionics tester convenient to install as in claim 1, wherein: the front end of the positioning screw rod (12) is fixedly connected with a rotating block (13), and the outer surface of the rotating block (13) is fixedly connected with a symmetrical rotating rod (14).

3. A multimode airborne avionics tester convenient to install as in claim 1, wherein: the front surface and the rear surface of the clamping column (3) are fixedly connected with fixed curved bars (15), and the top ends of the two fixed curved bars (15) are fixedly connected with the bottom surface of the positioning plate (4).

4. A multimode airborne avionics tester convenient to install as in claim 1, wherein: one side surface of the first magnet sheet (8) and one side surface of the second magnet sheet (9) which are close to each other are different pole surfaces, and threads matched with the outer surface of the positioning screw rod (12) of the inner wall of the threaded hole (11) are formed.

5. A multimode airborne avionics tester convenient to install as in claim 1, wherein: the outer surface of the bottom plate (1) is fixedly connected with supporting legs (16) which are arranged at equal intervals, and the bottom end of each supporting leg (16) is fixedly connected with an anti-slip seat (17).

6. A multimode airborne avionics tester convenient to install as in claim 5, wherein: one side surface of each supporting leg (16) which is close to each other is fixedly connected with a positioning rod (18), and the top end of each positioning rod (18) is fixedly connected with the bottom surface of the bottom plate (1).