Limiting transportation device for flight part production

Abstract

The utility model discloses a limiting transportation device for flight part production, which comprises a device base, a pair of device side plates, a plurality of carrying pulleys and a pair of stable auxiliary box bodies, the pair of stable auxiliary box bodies are connected with the pair of device side plates through coordinated transportation limiting structures correspondingly, the multiple carrying pulleys are installed at the bottom of the device base correspondingly, and surface auxiliary attaching assemblies are installed in the pair of stable auxiliary box bodies correspondingly. The utility model relates to the technical field of part limiting transportation, and the device enables the covering limiting baffle to be matched with a pair of stable auxiliary box bodies by coordinating the transportation limiting structure, so that flying parts are limited and fixed in multiple directions, semi-finished products and finished products are conveniently and protectively transported, and the subsequent processing is safe and convenient.

Description

Technical Field

[0001] The utility model relates to the technical field of part limit transportation, in particular to a limit transportation device for the production of flight parts. Background Art

[0002] The limit transportation device is a device used in the production of flight parts. It can position and transport parts during the production process and ensure their accuracy and stability. The following is a description of a possible limit transportation device for the production of flight parts; the device consists of a conveying table, a transmission mechanism, a limit device, and a control system. The conveying table is usually designed as a plane, on which a limit device and a fixture are installed. The transmission mechanism includes a motor and a gear system for controlling the movement of the conveying table. The limit device usually includes limiters in the horizontal and vertical directions to ensure that the parts do not deviate or deform during transportation. The control system can control the movement of the conveying table and the actions of the limit device through programming to achieve automated production; when the production of flight parts is required, workers place the parts on the fixture and then fix the fixture on the conveying table. With the start of the transmission mechanism, the conveying table begins to move, transporting the parts to the processing position of the next process. At the same time, the limit device can ensure that the parts do not have errors or deformations during transportation, thus ensuring the production accuracy and quality; however, most transportation devices or conveying flatbed trucks are difficult to fix irregular raw materials. Simply using auxiliary fixing methods such as ropes or belts is still prone to slippage and other situations, resulting in damage or deformation of the raw materials. In response to the above problems, there may already be technical solutions in the prior art, but this case wants to provide an alternative or replacement technical solution. Summary of the Utility Model

[0003] To achieve the above objectives, the utility model is realized through the following technical solutions: A limit transportation device for the production of flight parts, comprising: a device base, a pair of device side plates, a plurality of handling pulleys, and a pair of stable auxiliary boxes. The pair of device side plates are respectively installed on the device base. The pair of stable auxiliary boxes are respectively connected to the pair of device side plates through a coordinated transportation limit structure. The plurality of handling pulleys are respectively installed at the bottom of the device base. Surface auxiliary fitting components are respectively installed in the pair of stable auxiliary boxes;

[0004] The coordinated transportation limit structure includes: a pair of longitudinal alignment modules, a pair of module coordinated threaded rods, a pair of module adjustment motors, a covering limit baffle, a pair of baffle traction connecting columns, a pair of baffle driving air pumps, an air pump bearing module, a transverse displacement threaded rod, and a transverse driving motor;

[0005] A pair of the module position - adjusting motors are respectively installed inside a pair of the device side plates, and a pair of the module position - adjusting motors are respectively connected to a pair of the module cooperating threaded rods. A pair of the longitudinal alignment modules are respectively installed on a pair of the module cooperating threaded rods, and a pair of the longitudinal alignment modules are respectively connected to a pair of the stable auxiliary boxes. A pair of the baffle traction connecting columns are respectively connected to the covering limit baffle through rotating shafts, and a pair of the baffle traction connecting columns are respectively connected to a pair of the baffle driving air pumps through rotating shafts. A pair of the baffle driving air pumps are respectively installed on the air pump bearing module. The transverse displacement threaded rod is installed inside the device base, and the transverse displacement threaded rod is connected to the transverse driving motor. A module sliding groove is opened on the side wall of the device base, and the air pump bearing module is installed on the transverse displacement threaded rod through the module sliding groove.

[0006] It should be noted that in the above, a long - strip or plate - shaped flying part workpiece is placed on the bottom of the device base. The transverse driving motor drives the transverse displacement threaded rod to rotate, so that the air pump bearing module slides horizontally. After stopping at an appropriate position, the pair of baffle driving air pumps are driven to expand and contract, so that the baffle traction connecting columns drive the covering limit baffle to gradually fit the surface of the part, completing the preliminary limiting operation. Then, the pair of module position - adjusting motors are driven, so that the pair of module cooperating threaded rods rotate respectively, and then the corresponding pair of longitudinal alignment modules slide to appropriate positions, so that the pair of stable auxiliary boxes slide down until they fit the surface of the workpiece, completing the second thorough limiting operation. After the limiting and fixing are completed, the workpiece is properly transported through four handling pulleys.

[0007] Preferably, the surface auxiliary fitting assembly includes: a pair of box body displacement rotating shafts, several fitting limit blocks, and a pair of box - internal filling air bags;

[0008] A pair of the box body displacement rotating shafts are respectively installed on a pair of the longitudinal alignment modules, and a pair of the box body displacement rotating shafts are respectively connected to a pair of the stable auxiliary boxes. A pair of the box - internal filling air bags are respectively installed inside a pair of the stable auxiliary boxes;

[0009] It should be noted that in the above, after a pair of stable auxiliary boxes fit the surface of the flying part workpiece, the box - internal filling air bags are started. The box - internal filling air bags push several fitting limit blocks one by one and fit the surface of the flying part workpiece, so that the surface of the workpiece is properly fixed.

[0010] Preferably, a maintenance opening is provided on the device side plate;

[0011] Preferably, a maintenance opening is provided on the device base;

[0012] Preferably, an adjustment and maintenance opening is provided on the stable auxiliary box;

[0013] Preferably, an anti-slip pad is provided on the covering limit baffle. Beneficial effects

[0014] The utility model provides a limit transportation device for the production of flight components. It has the following beneficial effects. Compared with the prior art, this limit transportation device for the production of flight components coordinates the transportation limit structure, enabling the covering limit baffle to cooperate with a pair of stable auxiliary boxes to limit and fix the flight components in multiple directions, facilitating the protective transportation of semi-finished and finished products, and making subsequent processing safe and convenient. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a front view sectional structure schematic diagram of the limit transportation device for the production of flight components described in the utility model.

[0016] Figure 2 It is a side view structure schematic diagram of the limit transportation device for the production of flight components described in the utility model.

[0017] Figure 3 It is a schematic diagram of the stable auxiliary box of the limit transportation device for the production of flight components described in the utility model.

[0018] In the figure: 1, device base; 2, device side plate; 3, handling pulley; 4, stable auxiliary box; 5, longitudinal alignment module; 6, module coordination threaded rod; 7, module position adjustment motor; 8, covering limit baffle; 9, baffle traction connecting column; 10, baffle driving air pump; 11, air pump bearing module; 12, transverse displacement threaded rod; 13, transverse driving motor; 14, box body displacement rotating shaft; 15, fitting limit block; 16, box inner filling airbag. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0019] Based on the embodiments in the utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the utility model.

[0020] Through those skilled in the art, all electrical components in this case are connected to their adapted power supplies through wires, and appropriate controllers and encoders should be selected according to the actual situation to meet the control requirements. For the specific connection and control sequence, reference should be made to the sequence of the electrical components working successively in the following working principle to complete the electrical connection. The detailed connection means are well-known techniques in the art. The following mainly introduces the working principle and process, and no further description of electrical control will be made. Embodiment

[0021] The following specifically describes the present novel in conjunction with the drawings, as Figures 1-3As shown in the figure, a limiting transportation device for the production of flight parts includes: a device base 1, a pair of device side plates 2, a plurality of handling pulleys 3, and a pair of stable auxiliary boxes 4. The pair of device side plates 2 are respectively installed on the device base 1. The pair of stable auxiliary boxes 4 are respectively connected to the pair of device side plates 2 through a coordinated transportation limiting structure. The plurality of handling pulleys 3 are respectively installed at the bottom of the device base 1. Surface auxiliary fitting components are respectively installed in the pair of stable auxiliary boxes 4. The coordinated transportation limiting structure includes: a pair of longitudinal alignment modules 5, a pair of module coordinated threaded rods 6, a pair of module positioning motors 7, a covering limiting baffle 8, a pair of baffle traction connecting columns 9, a pair of baffle driving air pumps 10, an air pump bearing module 11, a transverse displacement threaded rod 12, and a transverse driving motor 13. The pair of module positioning motors 7 are respectively installed in the pair of device side plates 2, and the pair of module positioning motors 7 are respectively connected to the pair of module coordinated threaded rods 6. The pair of longitudinal alignment modules 5 are respectively installed on the pair of module coordinated threaded rods 6, and the pair of longitudinal alignment modules 5 are respectively connected to the pair of stable auxiliary boxes 4. The pair of baffle traction connecting columns 9 are respectively connected to the covering limiting baffle 8 through rotating shafts, and the pair of baffle traction connecting columns 9 are respectively connected to the pair of baffle driving air pumps 10 through rotating shafts. The pair of baffle driving air pumps 10 are respectively installed on the air pump bearing module 11. The transverse displacement threaded rod 12 is installed in the device base 1, and the transverse displacement threaded rod 12 is connected to the transverse driving motor 13. A module sliding groove is opened on the side wall of the device base 1. The air pump bearing module 11 is installed on the transverse displacement threaded rod 12 through the module sliding groove. The surface auxiliary fitting component includes: a pair of box body displacement rotating shafts 14, a plurality of fitting limiting blocks 15, and a pair of box body filling air bags 16. The pair of box body displacement rotating shafts 14 are respectively installed on the pair of longitudinal alignment modules 5, and the pair of box body displacement rotating shafts 14 are respectively connected to the pair of stable auxiliary boxes 4. The pair of box body filling air bags 16 are respectively installed in the pair of stable auxiliary boxes 4.

[0022] According to the attached Figures 1-3It is obtained that the strip or plate-shaped flight component workpiece is placed on the bottom of the device base 1. The transverse drive motor 13 drives the transverse displacement threaded rod 12 to rotate, causing the air pump bearing module 11 to slide horizontally. After stopping at an appropriate position, the pair of baffle plates drive the air pump 10 to expand and contract, so that the baffle traction connecting column 9 drives the covering limit baffle 8 to gradually fit the surface of the component, completing the preliminary limit operation. Then, the pair of module position adjustment motors 7 are driven, causing the pair of module cooperation threaded rods 6 to rotate respectively, and further causing the corresponding pair of longitudinal alignment modules 5 to slide to an appropriate position, so that the pair of stable auxiliary boxes 4 slide down until they fit the surface of the workpiece, completing the second complete limit operation. After the limit fixation is completed, the workpiece is properly transported through the four handling pulleys 3; when the pair of stable auxiliary boxes 4 fit the surface of the flight component workpiece, the airbag filled in the box 16 is started, and the airbag filled in the box 16 pushes and fits each of the several fitting limit blocks 15 to the surface of the flight component workpiece, thus properly fixing the surface of the workpiece.

[0023] Although the embodiments of the present invention have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principle and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A limited transport device for the production of flight parts, comprising: A device base (1), a pair of device side panels (2), a plurality of transport pulleys (3) and a pair of stabilizing auxiliary boxes (4), characterized in that the pair of device side panels (2) are respectively mounted on the device base (1), the pair of stabilizing auxiliary boxes (4) are respectively connected to the pair of device side panels (2) via coordinated transport limiting structures, the plurality of transport pulleys (3) are respectively mounted on the bottom of the device base (1), and the pair of stabilizing auxiliary boxes (4) are respectively installed with surface auxiliary laminating components; The coordinated transport limiting structure comprises: a pair of longitudinal alignment modules (5), a pair of module cooperative threaded rods (6), a pair of module positioning motors (7), a covering limiting baffle (8), a pair of baffle traction connecting columns (9), a pair of baffle driving air pumps (10), an air pump bearing module (11), a lateral displacement threaded rod (12) and a lateral driving motor (13); A pair of module positioning motors (7) are respectively installed in a pair of device side panels (2), and the pair of module positioning motors (7) are respectively connected to a pair of module cooperative threaded rods (6), a pair of longitudinal alignment modules (5) are respectively installed on a pair of module cooperative threaded rods (6), and the pair of longitudinal alignment modules (5) are respectively connected to a pair of stable auxiliary boxes (4), a pair of baffle traction connecting columns (9) are respectively connected to the covering limit baffle (8) through a rotating shaft, and the ... The connecting column (9) is connected to a pair of the baffle driving air pumps (10) through a rotating shaft, and the pair of the baffle driving air pumps (10) are respectively installed on the air pump supporting module (11). The transverse displacement threaded rod (12) is installed in the device base (1), and the transverse displacement threaded rod (12) is connected to the transverse driving motor (13). A module slide groove is opened on the side wall of the device base (1), and the air pump supporting module (11) is installed on the transverse displacement threaded rod (12) through the module slide groove.

2. A position limiting and transporting device for producing flight parts according to claim 1, characterized in that: The surface auxiliary laminating component comprises: a pair of box displacement shafts (14), a plurality of laminating limit blocks (15) and a pair of box filling air bags (16); A pair of the box displacement shafts (14) are respectively mounted on a pair of the longitudinal alignment modules (5), and a pair of the box displacement shafts (14) are respectively connected to a pair of the stabilizing auxiliary boxes (4), and a pair of the box filling air bags (16) are respectively mounted in a pair of the stabilizing auxiliary boxes (4).

3. A limited transport device for producing flight parts according to claim 2, characterized in that: An inspection opening is provided on the device side panel (2).

4. A limited transport device for producing flight parts according to claim 3, characterized in that: An inspection opening is provided on the device base (1).

5. A position limiting and transporting device for producing flight parts according to claim 4, characterized in that: The auxiliary stabilizing box (4) is provided with an adjustment and maintenance opening.

6. A position limiting and transporting device for producing flight parts according to claim 5, characterized in that: An anti-slip pad is provided on the covering limit baffle (8).

Images