Part transfer device for aircraft production

Abstract

The utility model discloses a part transfer device for aircraft production, which comprises a split-flow conveying assembly, a transfer distribution assembly is arranged on one side of the split-flow conveying assembly, and a feeding assembly is arranged on one side of the transfer distribution assembly; the feeding assembly comprises a fifth belt conveyor; the transfer distribution assembly comprises a third shell arranged on one side of the fifth belt conveyor, a hydraulic cylinder is fixedly connected to the bottom of the third shell, a sliding groove is formed in the inner side of the third shell, a second shell is slidably connected to the inner side of the third shell, and a fourth belt conveyor is arranged on the inner side of the second shell. The flow dividing conveying assembly comprises a first shell arranged on one side of the third shell, and a first belt conveyor, a second belt conveyor and a third belt conveyor are arranged in the first shell. According to the device, the phenomenon that the aircraft parts are blocked in the conveying process can be avoided without adjusting the conveying speed of the fifth belt conveyor, and the production efficiency of the aircraft parts is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft parts production, in particular to a parts transfer device for aircraft production. Background Art

[0002] An aircraft is a device that flies within the atmosphere or in space outside the atmosphere (space); aircraft are divided into three categories: aircraft, spacecraft, rockets and missiles; those that fly within the atmosphere are called aircraft, such as balloons, airships, airplanes, etc.; they rely on the static buoyancy of the air or the aerodynamic force generated by the relative movement of the air to take off and fly.

[0003] During the production process of aircraft, the parts of the aircraft need to be produced one by one and then assembled. During the production process of aircraft parts, a transfer device is needed to transport and transfer the aircraft parts. Since the speed of the transfer device is mostly fixed, during the process of transporting aircraft parts, if the output of aircraft parts is too large, the speed of the transfer device is prone to mismatch, which can easily cause transportation congestion. The speed of the transfer device needs to be adjusted again. The adjustment process is rather cumbersome and requires downtime, which affects production efficiency and needs to be improved. Utility Model Content

[0004] The utility model aims to provide a parts transfer device for aircraft production, so as to solve the problem that the transfer device proposed in the above background technology is difficult to adjust the transport speed and easily causes transportation congestion.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a parts transfer device for aircraft production, comprising a diversion conveying component, a transfer distribution component is provided on one side of the diversion conveying component, and a feeding component is provided on one side of the transfer distribution component;

[0006] The feeding assembly includes a fifth belt conveyor;

[0007] The transfer distribution assembly includes a third housing arranged on one side of the fifth belt conveyor, the inner side of the third housing is slidably connected with the second housing, and the inner side of the second housing is provided with the fourth belt conveyor;

[0008] The diversion conveying assembly comprises a first shell arranged on one side of the third shell, and a first belt conveyor, a second belt conveyor and a third belt conveyor are arranged inside the first shell.

[0009] Preferably, a hydraulic cylinder is fixedly connected to the bottom of the third shell, a slide groove is provided on the inner side of the third shell, openings are provided at both ends of the third shell, and the third shell is a right-angled "U"-shaped structure when viewed from the side.

[0010] Preferably, both ends of the second shell are provided with sliders, and one end of the slider is inserted into a slide groove on the inner side of the third shell.

[0011] Preferably, a second motor is fixedly connected to one end of the second housing, and a shaft of the second motor is connected to a shaft at one end of the fourth belt conveyor.

[0012] Preferably, a second belt conveyor is arranged at the bottom of the first belt conveyor, and a third belt conveyor is arranged at the bottom of the second belt conveyor.

[0013] Preferably, a driving belt is sleeved on the shaft at one end of the first belt conveyor and the third belt conveyor, a first motor is fixedly connected to the outer wall of the first shell, the shaft of the first motor is connected to the shaft at one end of the second belt conveyor, and one end of the driving belt on the first belt conveyor and the third belt conveyor is sleeved on the shaft of the first motor.

[0014] Preferably, the outer wall of the fifth belt conveyor is provided with a fourth shell, and the fourth shell is rotatably connected to the fifth belt conveyor.

[0015] Compared with the prior art, the beneficial effects of the utility model are:

[0016] (1) The device can avoid congestion during the transportation of aircraft parts without adjusting the conveying speed of the fifth belt conveyor, thereby improving the production efficiency of aircraft parts.

[0017] (2) The device is provided with a first belt conveyor, a second belt conveyor and a third belt conveyor, and a transfer distribution assembly is provided on one side of the first belt conveyor, the second belt conveyor and the third belt conveyor, so that after the aircraft parts are transported to the fourth belt conveyor of the transfer distribution assembly via the fifth belt conveyor, the fourth belt conveyor can be raised and lowered to correspond to any position of the first belt conveyor, the second belt conveyor and the third belt conveyor, so that the aircraft parts are transported to the top of the first belt conveyor, the second belt conveyor or the third belt conveyor, thereby achieving the purpose of diverting and transporting the aircraft parts. There is no need to stop the machine to adjust the speed of the fifth belt conveyor, and congestion in the transportation of aircraft parts can be avoided.

[0018] (3) The device is provided with a hydraulic cylinder at the bottom of the third shell, which can push the second shell to automatically rise and fall inside the third shell, so that the height of the fourth belt conveyor inside the second shell corresponds to the first belt conveyor, the second belt conveyor or the third belt conveyor. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 This is a schematic diagram of the structure of a parts transfer device for aircraft production according to the utility model;

[0020] Figure 2 It is a top view of a flow distribution and conveying assembly of a parts transfer device for aircraft production according to the utility model;

[0021] Figure 3 It is a top view of a transfer distribution component of a parts transfer device for aircraft production according to the utility model;

[0022] Figure 4 This is a top sectional view of a third shell of a parts transfer device for aircraft production according to the utility model.

[0023] In the figure: 1. diversion conveying assembly; 11. first shell; 12. first belt conveyor; 13. second belt conveyor; 14. third belt conveyor; 15. first motor; 16. driving belt; 2. transfer distribution assembly; 21. second shell; 22. fourth belt conveyor; 23. hydraulic cylinder; 24. third shell; 25. second motor; 26. slider; 3. feeding assembly; 31. fifth belt conveyor; 32. fourth shell. DETAILED DESCRIPTION

[0024] 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.

[0025] See also Figure 1-4 , the utility model provides a technical solution: a parts transfer device for aircraft production, comprising a diversion conveying component 1, a transfer distribution component 2 is arranged on one side of the diversion conveying component 1, and a feeding component 3 is arranged on one side of the transfer distribution component 2;

[0026] The feeding assembly 3 includes a fifth belt conveyor 31; a fourth housing 32 is provided on the outer wall of the fifth belt conveyor 31, and the fourth housing 32 is rotatably connected to the fifth belt conveyor 31; a shaft at one end of the fifth belt conveyor 31 of this structure is also connected to a first motor 15 for driving the fifth belt conveyor 31 to operate; the movement direction of the device is that the parts are transported to the diversion conveying assembly 1 through the fifth belt conveyor 31; the driving device of the device is controlled by PLC during the installation process;

[0027] The transfer distribution component 2 includes a third shell 24 arranged on one side of the fifth belt conveyor 31, a hydraulic cylinder 23 is fixedly connected to the bottom of the third shell 24, one end of the hydraulic cylinder 23 is connected to the bottom of the second shell 21, a slide groove is provided on the inner side of the third shell 24, and openings are provided at both ends of the third shell 24. The third shell 24 is a right-angle "U"-shaped structure when viewed from the side; this structure can drive the second shell 21 to achieve automatic lifting through the hydraulic cylinder 23; the second shell 21 is slidably connected to the inner side of the third shell 24, and sliders 26 are provided at both ends of the second shell 21, and one end of the slider 26 is inserted in the slide groove on the inner side of the third shell 24; this structure can improve the second shell 21 during the sliding and lifting process by providing the slider 26 Stability; a second motor 25 is fixedly connected to one end of the second housing 21, and the shaft of the second motor 25 is connected to the shaft of one end of the fourth belt conveyor 22; this structure can drive the fourth belt conveyor 22 to move through the second motor 25, so that the fourth belt conveyor 22 drives the aircraft parts on the top of the fourth belt conveyor 22 to be transported to the first belt conveyor 12, the second belt conveyor 13 or the third belt conveyor 14; the fourth belt conveyor 22 is arranged on the inner side of the second housing 21; by openings at the front and rear ends of the third housing 24, the fifth belt conveyor 31 can be arranged at both ends of the third housing 24, so that the parts are conveniently transported from the two ends of the third housing 24 to the fourth belt conveyor 22;

[0028] The diversion conveying assembly 1 includes a first shell 11 arranged on one side of the third shell 24, and a first belt conveyor 12, a second belt conveyor 13 and a third belt conveyor 14 are arranged inside the first shell 11; a second belt conveyor 13 is arranged at the bottom of the first belt conveyor 12, and a third belt conveyor 14 is arranged at the bottom of the second belt conveyor 13; this structure can divert and convey aircraft parts by arranging the first belt conveyor 12, the second belt conveyor 13 and the third belt conveyor 14, thereby not only avoiding congestion in the transportation process of aircraft parts, but also transporting aircraft parts to different processes for processing according to needs; the first shell 11 A driving belt 16 is sleeved on the shafts at one end of the belt conveyor 12 and the third belt conveyor 14, a first motor 15 is fixedly connected to the outer wall of the first shell 11, the shaft of the first motor 15 is connected to the shaft at one end of the second belt conveyor 13, and one end of the driving belt 16 on the first belt conveyor 12 and the third belt conveyor 14 is sleeved on the shaft of the first motor 15; with this structure, the first motor 15 can drive the second belt conveyor 13 to operate, and at the same time, the driving belt 16 can drive the first belt conveyor 12 and the third belt conveyor 14 to move synchronously, and the movement directions of the first belt conveyor 12, the second belt conveyor 13 and the third belt conveyor 14 are consistent.

[0029] Working principle: When the aircraft production parts transfer device is used, the aircraft parts are first transported to the fourth belt conveyor 22 inside the second housing 21 via the fifth belt conveyor 31. At this time, the hydraulic cylinder 23 pushes the second housing 21 and the fourth belt conveyor 22 to move upward, so that the height of the fourth belt conveyor 22 corresponds to the first belt conveyor 12, the second belt conveyor 13 or the third belt conveyor 14. When the height of the fourth belt conveyor 22 corresponds to the first belt conveyor 12, the second belt conveyor 13 or the third belt conveyor 14, the second motor 25 drives the fourth belt conveyor 22 to move upward. The fourth belt conveyor 22 is operated to move the aircraft parts on the fourth belt conveyor 22 to the first belt conveyor 12, the second belt conveyor 13 or the third belt conveyor 14 at the corresponding position, and then the fourth belt conveyor 22 moves downward to reset, and another aircraft part is conveyed to the top of the fourth belt conveyor 22 via the fifth belt conveyor 31. At this time, the fourth belt conveyor 22 rises and drives the aircraft parts to the first belt conveyor 12, the second belt conveyor 13 or the third belt conveyor 14 at different heights, and the aircraft parts are diverted for transportation to avoid congestion during the transportation of aircraft parts.

[0030] Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art may still modify the technical solutions described in the aforementioned embodiments, or make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention shall be included in the protection scope of the present invention.

Claims

1. A parts transfer device for aircraft production, characterized in that: It comprises a flow-dividing conveying component (1), a transfer distribution component (2) is arranged on one side of the flow-dividing conveying component (1), and a feeding component (3) is arranged on one side of the transfer distribution component (2); The feeding assembly (3) comprises a fifth belt conveyor (31); The transfer distribution component (2) comprises a third housing (24) arranged on one side of the fifth belt conveyor (31), the inner side of the third housing (24) is slidably connected to the second housing (21), and the inner side of the second housing (21) is provided with a fourth belt conveyor (22); The flow-dividing conveying assembly (1) comprises a first housing (11) arranged on one side of a third housing (24), and a first belt conveyor (12), a second belt conveyor (13) and a third belt conveyor (14) are arranged inside the first housing (11).

2. The aircraft production parts transfer device according to claim 1, characterized in that: The bottom of the third shell (24) is fixedly connected to a hydraulic cylinder (23); a slide groove is provided on the inner side of the third shell (24); openings are provided at both ends of the third shell (24); and the third shell (24) is a right-angled "U"-shaped structure when viewed from the side.

3. The aircraft production parts transfer device according to claim 1, characterized in that: Both ends of the second housing (21) are provided with sliding blocks (26), and one end of the sliding block (26) is inserted into a sliding groove on the inner side of the third housing (24).

4. The aircraft production parts transfer device according to claim 1, characterized in that: A second motor (25) is fixedly connected to one end of the second housing (21), and a shaft of the second motor (25) is connected to a shaft at one end of the fourth belt conveyor (22).

5. The aircraft production parts transfer device according to claim 1, characterized in that: A second belt conveyor (13) is arranged at the bottom of the first belt conveyor (12), and a third belt conveyor (14) is arranged at the bottom of the second belt conveyor (13).

6. The aircraft production parts transfer device according to claim 1, characterized in that: A driving belt (16) is sleeved on the shafts at one end of the first belt conveyor (12) and the third belt conveyor (14); a first motor (15) is fixedly connected to the outer wall of the first housing (11); the shaft of the first motor (15) is connected to the shaft at one end of the second belt conveyor (13); and one end of the driving belt (16) on the first belt conveyor (12) and the third belt conveyor (14) is sleeved on the shaft of the first motor (15).

7. The aircraft production parts transfer device according to claim 1, characterized in that: The outer wall of the fifth belt conveyor (31) is provided with a fourth outer shell (32), and the fourth outer shell (32) is rotatably connected to the fifth belt conveyor (31).

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