Cart for transporting large components of airplane

By designing a trolley for transporting large parts of aircraft including push and pulling devices, positioning units and locking units, the problem of inability to effectively push into the trailer and ensure stable connection in the prior art is solved, and convenient push into the transport bracket of large parts and stable connection between the trolley and the trailer is achieved.

CN222921601UActive Publication Date: 2025-05-30YUCHUANG INTELLIGENT TECH (SHANGHAI) CO LTD
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Patent Information

Application Number
CN202422643368.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-10-30
Publication Date
2025-05-30
Estimated Expiration
2034-10-30

AI Technical Summary

Technical Problem

There is a lack of effective carts in the prior art, and it is impossible to push the aircraft's large parts transport bracket from the cart into the trailer, and it is impossible to ensure a stable connection between the cart and the trailer.

Method used

A trolley for transporting large parts of an aircraft is designed, including a bracket, a push-pull device, a positioning unit and a locking unit. Push and pull devices are used to push and pull large parts transport brackets, and positioning units and locking units are used to ensure the correct position and stable connection of the cart and trailer.

Benefits of technology

Through the design of the push-pull device, the large-component transport bracket is easily pushed into the trailer. The positioning unit and the locking unit ensure the stable connection between the push-cart and the trailer, improving transportation efficiency and safety.

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  • Figure CN222921601U_ABST
    Figure CN222921601U_ABST
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Abstract

The utility model discloses a cart for transporting large components of an airplane. The cart comprises a bracket, a push-pull device, a positioning unit and a locking unit, the push-pull device is arranged on the bracket and is used for pushing and pulling the large component transportation bracket on the bracket; the positioning unit is arranged on the bracket and is used for positioning the bracket and the trailer when the bracket is connected with the trailer; the locking unit is arranged on the bracket and is used for locking and connecting the bracket and the trailer; the trailer is an aircraft large component transportation trailer. According to the utility model, the large component transportation bracket and the large component can be conveniently loaded on a trailer together.
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Description

Technical Field

[0001] The utility model belongs to the technical field of transportation machinery, and particularly relates to a trolley for transporting large aircraft components. Background Art

[0002] Chinese Utility Model Patent CN219468545U discloses a bracket for transporting an aircraft tail fin. The aircraft tail fin can be installed on the transport bracket and then placed in a trailer for transportation. However, it is found during implementation that there is currently no good transport trolley to carry a large component transport bracket such as the bracket for transporting an aircraft tail fin to the side of the trailer and to load the large component transport bracket together with the large component into the trailer. Content of the Utility Model

[0003] The technical problem to be solved by the utility model is to provide a trolley for transporting large aircraft components, which is convenient for loading the large component transport bracket together with the large component into the trailer in view of the above-mentioned deficiencies in the prior art.

[0004] To solve the above technical problem, the technical scheme adopted by the utility model is: a trolley for transporting large aircraft components, including a bracket, a pushing and pulling device, a positioning unit and a locking unit;

[0005] The pushing and pulling device is arranged on the bracket and is used for pushing and pulling the large component transport bracket on the bracket;

[0006] The positioning unit is arranged on the bracket and is used for position positioning when the bracket is connected to the trailer;

[0007] The locking unit is arranged on the bracket and is used for locking and connecting the bracket and the trailer;

[0008] The trailer is a trailer for transporting large aircraft components.

[0009] For the above-mentioned trolley for transporting large aircraft components, the positioning unit is a trolley guide rod, and a positioning hole for inserting the trolley guide rod is formed in the trailer.

[0010] For the above-mentioned trolley for transporting large aircraft components, the locking unit is a pin cylinder, and a pin hole for pin-connecting the pin cylinder is formed in the trailer.

[0011] For the above-mentioned trolley for transporting large aircraft components, limiting rods are arranged on the front side, rear side and left side of the bracket, the positioning unit and the locking unit are both arranged on the right side of the bracket, and the telescopic direction of the pushing and pulling device is the left-right direction.

[0012] For the above-mentioned trolley for transporting large aircraft components, it further includes a trolley body and a lifting mechanism. The bracket is located above the trolley body, and a lifting mechanism is installed between the bracket and the trolley body. The lifting mechanism is used for lifting the bracket.

[0013] For the cart for transporting large aircraft components described above, the lifting mechanism includes screw jacks installed at the four corners of the bracket. The four screw jacks are sequentially connected by a synchronous shaft in a driving manner, and at least one of the screw jacks is equipped with a driving motor.

[0014] The utility model has the following advantages compared with the prior art:

[0015] 1. By setting the pushing and pulling device, the utility model facilitates pushing the large component transportation bracket from the cart onto the trailer.

[0016] 2. By setting the positioning unit and the locking unit, the utility model facilitates connecting the cart and the trailer at a suitable position, which is reliable and stable.

[0017] The technical solution of the utility model will be further described in detail below with reference to the drawings and embodiments. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic structural diagram of the utility model.

[0019] Figure 2 It is Figure 1 a partial schematic diagram of

[0020] Figure 3 It is a schematic diagram before the transfer of the large component transportation bracket.

[0021] Figure 4 It is a schematic diagram after the transfer of the large component transportation bracket.

[0022] DESCRIPTION OF THE REFERENCE NUMERALS:

[0023] 1 - bracket; 2 - pushing and pulling device; 3 - positioning unit;

[0024] 4 - locking unit; 5 - large component transportation bracket; 6 - trailer;

[0025] 7 - cart body; 8 - lifting mechanism; 8-1 - screw jack;

[0026] 8-2 - synchronous shaft; 8-3 - motor. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0027] As Figure 1 — Figure 2 shown, a cart for transporting large aircraft components includes a bracket 1, a pushing and pulling device 2, a positioning unit 3 and a locking unit 4;

[0028] The pushing and pulling device 2 is arranged on the bracket 1 and is used for pushing and pulling the large component transportation bracket 5 on the bracket 1;

[0029] The positioning unit 3 is arranged on the bracket 1 and is used for positioning the position when the bracket 1 is connected to the trailer 6;

[0030] The locking unit 4 is arranged on the bracket 1 and is used for locking and connecting the bracket 1 and the trailer 6;

[0031] The trailer 6 is an aircraft large-component transport trailer 6.

[0032] It should be noted that the pushing and pulling device 2 is a pushing and pulling oil cylinder, and can also be an electric cylinder, a pneumatic cylinder or a lead screw nut mechanism with pushing and pulling functions, etc.;

[0033] The pushing and pulling device 2 is installed in the middle of the bracket 1. The pushing and pulling device 2 has two functions: the end of the pushing and pulling oil cylinder is connected to the connecting ear plate of the trailer 6, and the oil cylinder is contracted, so that the trolley is pulled towards the trailer 6 to realize the docking of the trailer 6 and the trolley; then the end of the pushing and pulling oil cylinder is connected to the ear plate of the large-component transport bracket 5, and through the pushing or pulling of the oil cylinder, the large-component transport bracket 5 is moved towards the trailer 6 or the trolley direction to complete the transfer of the large-component transport bracket 5.

[0034] In this embodiment, the positioning unit 3 is a trolley guide rod, and a positioning hole for inserting the trolley guide rod is provided on the trailer 6.

[0035] The structure of the trailer can refer to another patent for an aircraft large-component transport trailer structure applied simultaneously.

[0036] It should be noted that the number of the trolley guide rods is two, and the front end of the trolley guide rod is a frustum structure.

[0037] In this embodiment, the locking unit 4 is a pin oil cylinder, and a pin hole for pin-connecting the pin oil cylinder is provided on the trailer 6. The locking unit 4 can also be a pin electric cylinder, a pin pneumatic cylinder or a manual pin, etc.;

[0038] It should be noted that the left side wall of the trailer 6 has a hollow structure. During actual use, the pin oil cylinder can extend into the hollow structure, and the telescopic end of the pin oil cylinder extends upward and penetrates into the pin hole on the trailer 6, so as to realize the locking connection between the bracket 1 and the trailer 6.

[0039] In this embodiment, limiting rods are arranged on the front side, rear side and left side of the bracket 1. The positioning unit 3 and the locking unit 4 are both arranged on the right side of the bracket 1, and the telescopic direction of the pushing and pulling device 2 is the left-right direction.

[0040] In this embodiment, it further includes a trolley body 7 and a lifting mechanism 8. The bracket 1 is located above the trolley body 7, and a lifting mechanism 8 is installed between the bracket 1 and the trolley body 7. The lifting mechanism 8 is used for lifting the bracket 1.

[0041] In this embodiment, the lifting mechanism 8 includes screw jacks 8-1 installed at the four corners of the bracket 1. The four screw jacks 8-1 are sequentially connected by a synchronous shaft 8-2, and at least one of the screw jacks 8-1 is equipped with a driving motor 8-3.

[0042] It should be noted that the lifting of the bracket 1 is performed by the screw jacks 8-1. The four screw jacks 8-1 are driven by one motor 8-3, and the synchronous shaft 8-2 connects and synchronously drives the four screw jacks 8-1. When the bracket 1 approaches the trailer 6, the trolley guide rod on the trolley aligns with the positioning hole on the trailer 6. If the trailer 6 and the cargo plane of the bracket 1 are inconsistent due to the tire pressure of the trailer 6, the screw jacks 8-1 are used to adjust the height of the cargo plane of the bracket 1 so that the trolley guide rod aligns with the positioning hole. Then, the piston rod of the push-pull device 2 is extended, and the end of the piston rod is connected to the connecting ear plate of the trailer 6 with a pin. The push-pull device 2 is contracted, so that the trolley is pulled towards the trailer 6, realizing the docking of the trailer 6 and the trolley.

[0043] As Figure 3 and Figure 4 shown, when the present utility model is in use, it is positioned through the trolley guide rod and the trailer 6. Then, the end of the push-pull device 2 is connected to the connecting ear plate of the trailer 6, and the push-pull device 2 is contracted, so that the trolley is pulled towards the trailer 6, realizing the docking of the trailer 6 and the trolley. Then, the telescopic end of the pin cylinder extends upwards and penetrates into the pin hole on the trailer 6, thereby realizing the locking connection between the bracket 1 and the trailer 6. Finally, the end of the push-pull device 2 is connected to the ear plate of the large component transportation bracket 5, and the large component transportation bracket 5 is moved towards the trailer 6 through the push-pull device 2, completing the transfer of the large component transportation bracket 5.

[0044] The above is only a preferred embodiment of the present utility model, and does not impose any limitation on the present utility model. Any simple modification, change, and equivalent structural change made to the above embodiments according to the technical essence of the present utility model still fall within the protection scope of the technical solution of the present utility model.

Claims

1. A trolley for transporting large aircraft parts, characterized in that: It includes a bracket, a push-pull device, a positioning unit and a locking unit; The push-pull device is arranged on the bracket and is used to push and pull the large component transport bracket on the bracket; The positioning unit is arranged on the bracket and is used for positioning the bracket and the trailer when they are connected; The locking unit is arranged on the bracket and is used to lock and connect the bracket and the trailer; The trailer is a trailer for transporting large aircraft parts.

2. A trolley for transporting large aircraft parts according to claim 1, characterized in that: The positioning unit is a trolley guide rod, and a positioning hole for inserting the trolley guide rod is provided on the trailer.

3. A trolley for transporting large aircraft parts according to claim 1, characterized in that: The locking unit is a latch cylinder, and the trailer is provided with a latch hole for the latch cylinder to be pinned.

4. A trolley for transporting large aircraft parts according to claim 1, characterized in that: Limiting rods are arranged on the front side, the rear side and the left side of the bracket, the positioning unit and the locking unit are arranged on the right side of the bracket, and the telescopic direction of the push-pull device is the left-right direction.

5. A trolley for transporting large aircraft parts according to claim 1, characterized in that: It also includes a trolley body and a lifting mechanism. The bracket is located above the trolley body. The lifting mechanism is installed between the bracket and the trolley body, and the lifting mechanism is used to lift the bracket.

6. A trolley for transporting large aircraft parts according to claim 5, characterized in that: The lifting mechanism comprises screw lifts installed at four corners of the bracket, the four screw lifts are sequentially connected by a synchronous shaft, and at least one of the screw lifts is equipped with a driving motor.

Citation Information

Patent Citations

  • Bracket for transporting empennage of airplane

    CN219468545U