CN212019802U - Civil aviation wing assembly welding equipment - Google Patents

Abstract

The utility model discloses a civil aviation wing subassembly welding equipment, including the welding bench, install welding manipulator on electronic slide rail and the electronic slide rail in the upper end of welding bench, welding manipulator's below is equipped with carries thing board and carries the below of thing board and be bilateral symmetry and be equipped with two sets of lift electric telescopic handle, and is two sets of lift electric telescopic handle's upper end all with the lower extreme fixed connection who carries the thing board, the left and right sides that carries the thing board is the symmetry and is fixed with all be fixed with the rotating electrical machines on block and two sets of blocks. A civil aviation wing subassembly welding equipment, do the wing subassembly respectively through pressing from both sides tight piece and extrusion piece and carry out vertical and transverse orientation for the wing subassembly is stable to be fixed on standard welding position, convenient operation is simple and swift, is equipped with U type cushion in the U die cavity of pressing from both sides tight piece, is equipped with the elastic extrusion pad on the extrusion piece, carries out pressure buffering through U type cushion and elastic extrusion pad to the wing subassembly, prevents that the wing subassembly from being crushed.

Description

Civil aviation wing assembly welding equipment

Technical Field

The utility model relates to a welding equipment field, in particular to civil aviation wing subassembly welding equipment.

Background

The wing is one of the important parts of the airplane, is arranged on the airplane body, has the main function of generating lift force, can be provided with an ammunition cabin and an oil tank, can store a landing gear in flight, is also provided with a flap for improving the takeoff and landing performance and an aileron for transverse operation of the airplane, is also provided with a device for increasing the lift force such as a slat and the like on the front edge of the wing, has the function of generating the lift force to support the airplane to fly in the air, and has certain stabilizing and operating functions.

The existing rectangular wing assembly needs to be fixed when being welded, and the existing fixing mechanism is troublesome to operate and poor in fixing effect, so that a civil aviation wing assembly welding device is provided.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a civil aviation wing subassembly welding equipment can effectively solve the problem in the background art.

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

the utility model provides a civil aviation wing subassembly welding equipment, includes the welding bench, install welding manipulator on electronic slide rail and the electronic slide rail in the upper end of welding bench, welding manipulator's below is equipped with the below of carrying thing board and carrying the thing board and is bilateral symmetry and is equipped with two sets of lift electric telescopic handle, and is two sets of lift electric telescopic handle's upper end all with the lower extreme fixed connection who carries the thing board, it all is fixed with the rotating electrical machines on block and two sets of blocks to carry the left and right sides of thing board to be the symmetry and be fixed with, and is two sets of the output shaft of rotating electrical machines and turning block fixed connection and turning block are located the inner chamber of block and rotate rather than being connected, clamping mechanism and extrusion mechanism are installed to.

Preferably, clamping mechanism is including pressing from both sides tight motor, press from both sides tight motor and fix the inner chamber at the turning block, and press from both sides tight motor's output shaft and the left end fixed connection who presss from both sides tight lead screw, the right-hand member that presss from both sides tight lead screw rotates with the inner chamber wall of turning block to be connected, and presss from both sides to be all fixed with on the tight lead screw that is bilateral symmetry and is equipped with two sets of traveling nuts and press from both sides tight block, two sets of the one end of pressing from both sides tight lead screw is.

Preferably, the inner cavity of the clamping block is provided with a U-shaped clamping cavity, and a U-shaped elastic cushion matched with the U-shaped clamping cavity is fixed in the inner cavity of the U-shaped clamping cavity.

Preferably, extrusion mechanism is including extrusion electric telescopic handle, extrusion electric telescopic handle fixes the inner chamber at the turning block, and extrusion electric telescopic handle's output shaft runs through the turning block and extends to its outside and stripper plate fixed connection, one of stripper plate keeping away from extrusion electric telescopic handle is served and is fixed with the elasticity extrusion pad.

Preferably, the carrier plate has a width less than the width of the wing assembly.

Preferably, the welding bench is fixedly provided with a controller, and the electric slide rail, the welding manipulator, the lifting electric telescopic rod, the rotating motor, the clamping motor and the extrusion electric telescopic rod are all electrically connected with the controller.

Compared with the prior art, the utility model discloses following beneficial effect has:

1. the wing assembly fixing device is provided with the clamping mechanism and the extruding mechanism, the wing assembly is sent into the space between the two groups of clamping blocks on the same side by the aid of the extruding electric telescopic rod, and then the wing assembly is longitudinally and transversely positioned by the aid of the clamping blocks and the extruding block respectively, so that the wing assembly is stably fixed on a standard welding position, and the wing assembly fixing device is convenient, simple and fast to operate.

2. A U-shaped elastic cushion is arranged in a U-shaped cavity of the clamping block, an elastic extrusion cushion is arranged on the extrusion block, and the U-shaped elastic cushion and the elastic extrusion cushion are used for carrying out pressure buffering on the wing assembly to prevent the wing assembly from being crushed.

Drawings

FIG. 1 is an overall structure diagram of the welding equipment for civil aviation wing components of the present invention;

FIG. 2 is a block structure diagram of the welding equipment for civil aviation wing components of the present invention;

FIG. 3 is a sectional top view of a block of the welding device for civil aviation wing assemblies of the present invention;

FIG. 4 is an enlarged view of the point A structure of the welding equipment for civil aviation wing assemblies of the present invention;

fig. 5 is the utility model discloses a clamp block left side view of civil aviation wing subassembly welding equipment.

In the figure: 1. a welding table; 2. an electric slide rail; 3. welding a manipulator; 4. a block body; 5. a loading plate; 6. lifting the electric telescopic rod; 7. rotating the block; 8. a rotating electric machine; 9. a clamping mechanism; 91. clamping the motor; 92. clamping the screw rod; 93. moving the nut; 94. a clamping block; 10. an extrusion mechanism; 101. extruding the electric telescopic rod; 102. a pressing plate; 103. an elastic pressing pad; 11. a U-shaped clamping cavity; 12. and a controller.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; 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 in specific cases to those skilled in the art.

As shown in fig. 1-5, a civil aviation wing subassembly welding equipment, including welding bench 1, install electric slide rail 2 and electric slide rail 2 on the upper end of welding bench 1 and install welding manipulator 3, the below of welding manipulator 3 is equipped with carries thing board 5 and carries the below of thing board 5 and is bilateral symmetry and is equipped with two sets of lift electric telescopic handle 6, the upper end of two sets of lift electric telescopic handle 6 all with the lower extreme fixed connection who carries thing board 5, it all is fixed with rotating electrical machines 8 on 4 and two sets of blocks 4 to carry the left and right sides of thing board 5 to be the symmetry fixed with block 4, the output shaft of two sets of rotating electrical machines 8 and the inner chamber that 7 fixed connection of turning block and 7 are located block 4 and rotate rather than being connected, clamping mechanism 9 and extrusion mechanism 10 are installed to the inner chamber of turning block 7.

The clamping mechanism 9 comprises a clamping motor 91, the clamping motor 91 is fixed in an inner cavity of the rotating block 7, an output shaft of the clamping motor 91 is fixedly connected with the left end of a clamping screw rod 92, the right end of the clamping screw rod 92 is rotatably connected with the wall of the inner cavity of the rotating block 7, two groups of moving nuts 93 are symmetrically arranged on the clamping screw rod 92 in a left-right mode, clamping blocks 94 are fixed on the two groups of moving nuts 93, one ends, far away from the clamping screw rod 92, of the two groups of clamping blocks 94 penetrate through the rotating block 7 and extend to the outside of the rotating block, and the two groups of clamping blocks 94 are driven to clamp and fix two ends of the wing assembly through.

The inner cavity of the clamping block 94 is provided with a U-shaped clamping cavity 11, a U-shaped elastic cushion matched with the U-shaped clamping cavity 11 is fixed in the inner cavity of the U-shaped clamping cavity 11, two ends of the wing assembly are respectively located in the two groups of U-shaped clamping cavities 11 to longitudinally fix the wing assembly, and the pressure of the clamping plate on the wing assembly is buffered through the U-shaped elastic cushion to prevent the wing assembly from being damaged due to extrusion.

The extrusion mechanism 10 comprises an extrusion electric telescopic rod 101, the extrusion electric telescopic rod 101 is fixed in an inner cavity of the rotating block 7, an output shaft of the extrusion electric telescopic rod 101 penetrates through the rotating block 7 and extends to the outside of the rotating block and is fixedly connected with an extrusion plate 102, an elastic extrusion pad 103 is fixed on one end, far away from the extrusion electric telescopic rod 101, of the extrusion plate 102, the two ends of the extrusion electric telescopic rod 101 and the two ends of the wing assembly are in contact extrusion through the two groups of extrusion mechanisms 10, and therefore the wing assembly is transversely extruded and fixed.

The width of the carrier plate 5 is smaller than that of the wing assembly, so that the clamping mechanism 9 can clamp the wing assembly conveniently.

Fixed controller 12 that is equipped with on the welding bench 1, electric slide rail 2, welding manipulator 3, lift electric telescopic handle 6, rotating electrical machines 8, press from both sides tight motor 91 and extrusion electric telescopic handle 101 all with controller 12 electric connection, the controller 12 of being convenient for is to the control of each equipment.

It should be noted that the utility model relates to a civil aviation wing assembly welding device, when in use, the wing assembly is placed on the carrying plate 5, the left and right ends of the wing assembly are moved between two sets of clamping blocks 94 arranged on the left and right sides by the lifting electric telescopic rod 6, the clamping screw 92 is driven to rotate by the work of two sets of clamping motors 91, the clamping blocks 94 on the same side are driven by the moving nut 93 to clamp and fix the front and back ends of the wing assembly (namely, longitudinally clamp and fix), at the moment, the front and back ends of the wing assembly are respectively arranged in the U-shaped clamping cavities 11 of the two sets of clamping blocks 94 arranged on the front and back sides, and then the two ends of the wing assembly are extruded and fixed (namely, transversely fixed) by the two sets of extruding electric telescopic rods 101, so that the wing assembly is stably fixed on a standard welding position, the operation is simple and convenient, the wing assembly is welded, when the wing assembly needs to be overturned, the lifting electric telescopic rod 6 is restored to the original position, a sufficient overturning space is emptied for overturning of the wing assembly, and then the two groups of rotating motors 8 work simultaneously to drive the two groups of rotating blocks 7 to rotate, so that the wing assembly is overturned, and welding of the wing assembly is facilitated.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (6)

1. The utility model provides a civil aviation wing subassembly welding equipment, includes welding bench (1), its characterized in that: install welding machines hand (3) on electric slide rail (2) and electric slide rail (2) are installed to the upper end of welding bench (1), the below of welding machines hand (3) is equipped with carries thing board (5) and carries the below of thing board (5) and is bilateral symmetry and is equipped with two sets of lift electric telescopic handle (6), and is two sets of the upper end of lift electric telescopic handle (6) all with the lower extreme fixed connection who carries thing board (5), it is the symmetry and is fixed with all be fixed with rotating electrical machines (8) on block (4) and two sets of block (4) to carry the left and right sides of thing board (5), and is two sets of the output shaft and the turning block (7) fixed connection of rotating electrical machines (8) and turning block (7) are located the inner chamber of block (4) and rotate rather than and be connected, clamping mechanism (9) and extrusion mechanism (10) are installed to the inner chamber of turning block.

2. The civil aviation wing assembly welding device of claim 1, wherein: clamping mechanism (9) are including pressing from both sides tight motor (91), press from both sides tight motor (91) and fix the inner chamber at turning block (7), and press from both sides the output shaft of tight motor (91) and the left end fixed connection who presss from both sides tight lead screw (92), the right-hand member that presss from both sides tight lead screw (92) rotates with the inner chamber wall of turning block (7) to be connected, and presss from both sides tight lead screw (92) and goes up to be bilateral symmetry and be equipped with two sets of removal nuts (93) and all be fixed with and press from both sides tight piece (94), two sets of the one end of pressing from both sides tight lead screw (92) is kept away from to tight piece (.

3. The civil aviation wing assembly welding device of claim 2, wherein: the inner cavity of the clamping block (94) is provided with a U-shaped clamping cavity (11), and a U-shaped elastic pad matched with the U-shaped clamping cavity (11) is fixed in the inner cavity of the U-shaped clamping cavity (11).

4. The civil aviation wing assembly welding device of claim 1, wherein: extrusion mechanism (10) are including extrusion electric telescopic handle (101), the inner chamber at turning block (7) is fixed in extrusion electric telescopic handle (101), and the output shaft of extrusion electric telescopic handle (101) runs through turning block (7) and extends to its outside and stripper plate (102) fixed connection, stripper plate (102) are kept away from one of extrusion electric telescopic handle (101) and are served and be fixed with elasticity extrusion pad (103).

5. The civil aviation wing assembly welding device of claim 1, wherein: the width of the carrier plate (5) is smaller than the width of the wing assembly.

6. The civil aviation wing assembly welding device of any one of claims 1 to 4, wherein: the welding bench (1) is fixedly provided with a controller (12), and the electric sliding rail (2), the welding manipulator (3), the lifting electric telescopic rod (6), the rotating motor (8), the clamping motor (91) and the extrusion electric telescopic rod (101) are all electrically connected with the controller (12).

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