CN214604212U

CN214604212U - Strutting arrangement is used in aircraft model processing

Info

Publication number: CN214604212U
Application number: CN202120690746.5U
Authority: CN
Inventors: 张红武; 雷永胜
Original assignee: Xi'an Ruisheng Precision Machinery Co ltd
Current assignee: Xi'an Linglong Aircraft Parts Manufacturing Co ltd
Priority date: 2021-04-06
Filing date: 2021-04-06
Publication date: 2021-11-05
Anticipated expiration: 2031-04-06

Abstract

The utility model relates to a strutting arrangement is used in aircraft model processing, the on-line screen storage device comprises a base, base upper end overlap joint is equipped with the backup pad, a side end face that backup pad and base are close to each other is equipped with first connecting block and second connecting block respectively, one side of keeping away from first connecting block between backup pad and the base is equipped with first spout and second spout relatively, be equipped with elevating system between backup pad and the base, the bottom is equipped with first motor in the base cavity, the backup pad top is equipped with the swivel mount, swivel mount center pin lower extreme is connected with second motor output shaft, the fixed concave type revolving stage that is equipped with in swivel mount upper end, be equipped with fixture on the concave type revolving stage, elevating system includes two sets of alternately first branch and second branch. The utility model discloses support and fixed more stable, can adjust the height of aircraft and rotate the aircraft model according to actual processing needs when using, need not to fix again.

Description

Strutting arrangement is used in aircraft model processing

Technical Field

The utility model relates to an aircraft model processing technology field, in particular to strutting arrangement is used in aircraft model processing.

Background

The airplane is one of the greatest inventions of human beings, and realizes the dream that the human beings want to fly to the blue sky. With the development of time, the cognition level of people is continuously improved, more and more people love to collect airplane models, and the historical cultural value of the airplane models is unintentionally sublimated. Various airplane models are designed according to different requirements of people. At present, static aircraft model material has the multiple, has metal, plastics, resin and glass steel etc. and also divide into ten many centimetres, twenty many centimetres, thirty many centimetres, forty many centimetres and the model up to a meter more according to the proportion, in aircraft model course of working, need utilize strutting arrangement to fix the centre gripping to the fuselage, however current strutting arrangement simple structure is fixed, is difficult to fix the fuselage stably, is not convenient for go up and down and rotate according to the processing demand simultaneously, brings the inconvenience for aircraft model's processing.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a strutting arrangement is used in aircraft model processing to the strutting arrangement simple structure who mentions in the solution background art can not go up and down and rotate, the fixed unstability scheduling problem of fuselage.

In order to achieve the above object, the utility model adopts the following technical scheme:

the utility model provides a strutting arrangement is used in aircraft model processing, includes the base, base upper end overlap joint is equipped with the backup pad, a side end face that backup pad and base are close to each other is equipped with first connecting block and second connecting block respectively, the one side of keeping away from first connecting block between backup pad and the base is equipped with first spout and second spout relatively, be equipped with elevating system between backup pad and the base, the bottom is equipped with first motor in the base cavity, the backup pad lower extreme is equipped with the second motor, the backup pad top is equipped with the swivel mount, swivel mount center pin lower extreme is connected with second motor output shaft, the fixed concave type revolving stage that is equipped with in swivel mount upper end, be equipped with fixture on the concave type revolving stage.

Further, elevating system includes two sets of criss-cross first branch and second branch, first branch and second branch cross department rotate through the connecting piece and connect, first branch top and second branch bottom are articulated with first connecting block and second connecting block respectively, first branch bottom and second branch top respectively with first spout and second spout sliding connection, be equipped with two fixed blocks, two relatively on the base be equipped with the lead screw between the fixed block and rotate with two fixed blocks and be connected, the one end of lead screw is connected with the output shaft of first motor, run through on the lead screw and be equipped with the moving member, the moving member both ends are connected with two first branch bottoms respectively.

Further, fixture is including setting up the electric telescopic handle on two opposite faces of concave type revolving stage, electric telescopic handle keeps away from the one end of concave type revolving stage and is equipped with pressure sensor, pressure sensor keeps away from electric telescopic handle's one end and is equipped with the grip block.

Furthermore, rubber pads are arranged on the opposite surfaces of the two clamping blocks.

Furthermore, the lower end of the base is provided with a universal wheel with a locking structure.

The utility model has the advantages that:

the utility model is provided with the lifting mechanism, which can adjust the height of the device according to the actual processing requirement, and can lower the supporting plate to the lowest when not in use, thereby saving the space occupation; the provided rotating mechanism can rotate the airplane model in the machining process, so that the airplane model does not need to be fixed again, the working procedures are reduced, and the working efficiency is improved; the electric telescopic rod is adopted to fix the airplane model and is provided with the pressure sensor, so that pressure can be sensitively sensed, and the airplane model is prevented from deforming due to overlarge pressure during fixing; the universal wheel with the locking structure is arranged at the bottom end of the device, so that the device can be conveniently moved and fixed, and manual carrying of the device is reduced.

Drawings

Fig. 1 is a schematic front view of the supporting device for processing an airplane model of the present invention;

FIG. 2 is a schematic view of the cross-sectional structure A-A of the supporting device for machining an airplane model of the present invention;

fig. 3 is the utility model relates to a supporting device's concave type revolving stage for aircraft model processing looks sideways at the structural sketch map.

Reference symbol comparison table:

the device comprises a base 1, a support plate 2, a first connecting block 3, a second connecting block 4, a first sliding groove 5, a second sliding groove 6, a first motor 7, a second motor 8, a rotating frame 9, a concave rotating table 10, an electric telescopic rod 11, a pressure sensor 12, a clamping block 13, a first supporting rod 14, a second supporting rod 15, a fixed block 16, a screw rod 17, a moving member 18 and a universal wheel 19.

Detailed Description

In order to make the content of the present invention more clearly understood, the technical solution in the embodiment of the present invention will be clearly and completely described below with reference to the attached drawings in the embodiment of the present invention. In which like parts are designated by like reference numerals. It should be noted that the terms "front," "back," "left," "right," "upper" and "lower" used in the following description refer to directions in the drawings, and the terms "inner" and "outer" refer to directions toward and away from, respectively, the geometric center of a particular component.

As shown in fig. 1-3, a supporting device for processing an airplane model comprises a base 1, a supporting plate 2 is lapped on the upper end of the base 1, a first connecting block 3 and a second connecting block 4 are respectively arranged on the side end surfaces of the supporting plate 2 and the base 1 which are close to each other, a first sliding groove 5 and a second sliding groove 6 are oppositely arranged on one side of the supporting plate 2 and the base 1 which is far away from the first connecting block 3, two groups of crossed first supporting rods 14 and second supporting rods 15 are arranged between the supporting plate 2 and the base 1, the crossed parts of the first supporting rods 14 and the second supporting rods 15 are rotatably connected through a bolt structure, the top ends of the first supporting rods 14 and the bottom ends of the second supporting rods 15 are respectively hinged with the first connecting block 3 and the second connecting block 4, the bottom ends of the first supporting rods 14 and the top ends of the second supporting rods 15 are respectively slidably connected with the first sliding groove 5 and the second sliding groove 6, two fixing blocks 16 are oppositely arranged on the base 1, a screw rod 17 is arranged between the two fixed blocks 16 and is rotationally connected with the two fixed blocks 16, one end of the screw rod 17 is connected with an output shaft of the first motor 7, a moving member 18 is arranged on the screw rod 17 in a penetrating way, two ends of the moving member 18 are respectively connected with the bottom ends of the two first supporting rods 14, a second motor 8 is arranged at the lower end of the supporting plate 2, a rotating frame 9 is arranged above the supporting plate 2, the lower end of the central shaft of the rotating frame 9 is connected with an output shaft of the second motor 8, a concave rotating platform 10 is fixedly arranged at the upper end of the rotating frame 9, electric telescopic rods 11 on two opposite surfaces of the concave rotating platform 10, one end of each electric telescopic rod 11, which is far away from the concave rotating platform 10, is provided with a pressure sensor 12, one end of each pressure sensor 12, which is far away from the corresponding hydraulic electric telescopic rod 11, is provided with a clamping block 13, and the opposite surfaces of the two clamping blocks 13 are both provided with rubber pads, the lower end of the base 1 is provided with a universal wheel 19 with a locking structure.

The utility model discloses at its during operation, can conveniently remove whole device through universal wheel 19, labour saving and time saving, locking mechanism can be fixed with the device, after removing the device to suitable position, according to the height that processing needs, start first motor 7 and rotate and drive the lead screw 17 that sets up between two fixed blocks 16 and rotate, moving member 18 on the lead screw 17 moves to the right, drive two first branch 14 bottoms at moving member 18 both ends and move to the right in second spout 6, two second branch 15 tops move to the right in first spout 5 simultaneously, the top of first branch 14 and the bottom of second branch 15 rotate on first connecting block 3 and second connecting block 4 respectively, backup pad 2 rises thereupon; placing the airplane model on the concave rotary table 10, starting the electric telescopic rod 11 to extend, extruding the clamping block 13 and the airplane model to generate pressure, and controlling the electric telescopic rod 11 to stop working after the pressure sensor 12 receives a certain pressure to fix the airplane model; when the airplane model needs to rotate in the machining process, the second motor 8 is started to rotate to drive the rotating frame 9 and the concave rotating platform 10 to rotate together.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not intended to limit the present invention, and all modifications, equivalents, improvements and the like that are made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims

1. The supporting device for processing the airplane model is characterized by comprising a base (1), wherein a supporting plate (2) is arranged at the upper end of the base (1) in a lap joint mode, a first connecting block (3) and a second connecting block (4) are respectively arranged on one side end face, close to each other, of the supporting plate (2) and the base (1), a first sliding groove (5) and a second sliding groove (6) are oppositely arranged on one side, far away from the first connecting block (3), between the supporting plate (2) and the base (1), a lifting mechanism is arranged between the supporting plate (2) and the base (1), a first motor (7) is arranged at the bottom in a cavity of the base (1), a second motor (8) is arranged at the lower end of the supporting plate (2), a rotating frame (9) is arranged above the supporting plate (2), the lower end of a central shaft of the rotating frame (9) is connected with an output shaft of the second motor (8), a concave rotating table (10) is fixedly arranged at the upper end of the rotating frame (9), the concave rotary table (10) is provided with a clamping mechanism.

2. The supporting device for processing the airplane model according to claim 1, wherein the lifting mechanism comprises two sets of first supporting rods (14) and second supporting rods (15) which are crossed, the crossed parts of the first supporting rods (14) and the second supporting rods (15) are rotatably connected through connecting pieces, the top ends of the first supporting rods (14) and the bottom ends of the second supporting rods (15) are respectively hinged with the first connecting block (3) and the second connecting block (4), the bottom ends of the first supporting rods (14) and the top ends of the second supporting rods (15) are respectively slidably connected with the first sliding chute (5) and the second sliding chute (6), two fixing blocks (16) are oppositely arranged on the base (1), a screw rod (17) is arranged between the two fixing blocks (16) and is rotatably connected with the two fixing blocks (16), one end of the screw rod (17) is connected with an output shaft of the first motor (7), the screw rod (17) is provided with moving parts (18) in a penetrating mode, and two ends of each moving part (18) are connected with the bottom ends of the two first supporting rods (14) respectively.

3. The supporting device for airplane model machining according to claim 1, wherein the clamping mechanism comprises an electric telescopic rod (11) arranged on two opposite surfaces of the concave rotary table (10), one end of the electric telescopic rod (11) far away from the concave rotary table (10) is provided with a pressure sensor (12), and one end of the pressure sensor (12) far away from the electric telescopic rod (11) is provided with a clamping block (13).

4. A support device for machining aircraft models, as in claim 3, characterized in that the opposite faces of the two blocks (13) are provided with rubber pads.

5. The supporting device for airplane model machining according to claim 1, characterized in that the lower end of the base (1) is provided with a universal wheel (19) with a locking structure.