Wing vibration reduction protection transportation device

Abstract

The invention provides a wing vibration reduction protection transportation device, and relates to the technical field of wing transportation. The transportation frame is detachably arranged in the box body, a containing space is formed in the transportation frame, and the containing space is used for containing the wings; the vibration reduction mechanism is arranged at the bottom of the containing space and connected with the transportation frame through an elastic component, the upper side of the vibration reduction mechanism is used for placing the wings, and fixing components are arranged at the two ends of the vibration reduction mechanism and used for fixing the wings; the problems that in the prior art, unmanned aerial vehicle wings with large sizes are large in transportation size, high in protection requirement and inconvenient to transport are solved.

Description

Technical Field

[0001] The present invention belongs to the technical field of wing transportation, and more specifically, relates to a wing vibration reduction and protection transportation device. Background Art

[0002] With the continuous development of solar drone technology, special needs for the use of drones have emerged one after another. The present invention is designed according to the special needs of a certain type of solar drone for long-distance transfer. The drone has a large wingspan and needs to be transported in sections during long-distance transfer. Considering that the impact load and transportation vibration load that the solar drone wings can withstand are relatively low, a shock-absorbing and protective transportation device needs to be designed. Summary of the invention

[0003] The purpose of the present invention is to provide a wing vibration reduction protection transportation device to address the deficiencies in the prior art, so as to solve the problems in the prior art of large-sized UAV wings having large transportation volume, high protection requirements and inconvenient transportation.

[0004] In order to achieve the above object, the present invention provides a wing vibration reduction and protection transportation device, comprising:

[0005] Box;

[0006] A transport rack, the transport rack is detachably arranged in the box, and a receiving space is formed inside the transport rack, and the receiving space is used to receive the wing;

[0007] A vibration-damping mechanism is arranged at the bottom of the accommodating space and connected to the transport frame through an elastic component. The upper side of the vibration-damping mechanism is used to place the wing. Fixing components are arranged at both ends of the vibration-damping mechanism, and the fixing components are used to fix the wing.

[0008] Optionally, the box body is a rectangular box, and box doors are respectively provided at both ends of the box body.

[0009] Optionally, a lock is provided on the inner wall of the box body, and the lock is detachably connected to the transport rack.

[0010] Optionally, casters are provided at the bottom of the transport frame.

[0011] Optionally, the casters are connected to the transport frame via a lifting mechanism.

[0012] Optionally, the transport rack includes a rectangular frame and a trapezoidal frame arranged on both sides of the long sides of the rectangular frame, and the lifting mechanism and the casters are arranged on the outside of the rectangular frame and do not protrude from the trapezoidal frame.

[0013] Optionally, the box body is a thermal insulation box.

[0014] Optionally, at least two transport racks are provided, and at least two transport racks are stacked and can be placed in the box.

[0015] Optionally, the vibration reduction mechanism includes a base frame, a plurality of mounting plates are arranged on the upper side of the base frame, a conformable sponge is arranged on the upper side of the mounting plate, the upper surface of the conformable sponge cooperates with the lower wing surface of the wing, and the base frame is connected to the bottom of the transport frame through the elastic component.

[0016] Optionally, the fixing component includes a base, the base is connected to the base frame, a lower holding ring and an upper holding ring are provided on the upper side of the base, the upper holding ring and the lower holding ring are connected to form a complete holding ring structure, and the wing is fixed by the holding ring structure.

[0017] The present invention provides a wing vibration reduction and protection transportation device, which has the beneficial effects of: the wing vibration reduction and protection transportation device comprises a box body, a transportation frame and a vibration reduction mechanism, the wing can be placed on the upper side of the vibration reduction mechanism and placed in the accommodating space in the transportation frame, and the elastic component between the vibration reduction mechanism and the transportation frame is used to reduce the vibration of the wing, thereby reducing the vibration impact suffered by the wing during transportation, and at the same time, the transportation frame loaded with the wing is placed in the box body and can be protected by the box body, thereby protecting the wing during transportation.

[0018] Other features and advantages of the present invention will be described in detail in the following detailed description. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] The above and other objects, features and advantages of the present invention will become more apparent through a more detailed description of exemplary embodiments of the present invention in conjunction with the accompanying drawings, wherein like reference numerals generally represent like components throughout the exemplary embodiments of the present invention.

[0020] Figure 1 A schematic structural diagram of a box of a wing vibration reduction and protection transportation device according to an embodiment of the present invention is shown.

[0021] Figure 2 A schematic diagram of the main structure of a transport frame of a wing vibration reduction and protection transport device according to an embodiment of the present invention is shown.

[0022] Figure 3 A schematic diagram of the structure of a transport frame of a wing vibration reduction and protection transport device according to an embodiment of the present invention is shown in a top view.

[0023] Figure 4 A schematic structural diagram of a three-layer transport frame of a wing vibration reduction and protection transport device according to an embodiment of the present invention is shown.

[0024] Figure 5A schematic structural diagram of a chassis of a wing vibration reduction and protection transportation device according to an embodiment of the present invention is shown.

[0025] Figure 6 A schematic diagram of the installation of a mounting plate of a wing vibration reduction and protection transportation device according to an embodiment of the present invention is shown.

[0026] Figure 7 A schematic structural diagram of a conformable sponge for a wing vibration reduction and protection transportation device according to an embodiment of the present invention is shown.

[0027] Figure 8 A schematic structural diagram of a fixing component of a wing vibration reduction and protection transportation device according to an embodiment of the present invention is shown.

[0028] Description of reference numerals:

[0029] 1. Box body; 2. Transport rack; 3. Box door; 4. Bottom plate lock; 5. Side wall lock; 6. Casters; 7. Rectangular frame; 8. Trapezoidal frame; 9. Base frame; 10. Mounting plate; 11. Conformal sponge; 12. Base; 13. Lower holding ring; 14. Upper holding ring. DETAILED DESCRIPTION

[0030] The preferred embodiments of the present invention will be described in more detail below. Although the preferred embodiments of the present invention are described below, it should be understood that the present invention can be implemented in various forms and should not be limited by the embodiments set forth herein. On the contrary, these embodiments are provided to make the present invention more thorough and complete, and to fully convey the scope of the present invention to those skilled in the art.

[0031] like Figures 1 to 8 As shown, the present invention provides a wing vibration reduction and protection transportation device, comprising:

[0032] Box 1;

[0033] A transport rack 2, which is detachably disposed in the box body 1, and an accommodation space is formed inside the transport rack 2, and the accommodation space is used to accommodate the wing;

[0034] The vibration-damping mechanism is arranged at the bottom of the accommodating space and is connected to the transport frame 2 through an elastic component. The upper side of the vibration-damping mechanism is used to place the wing. Fixed components are arranged at both ends of the vibration-damping mechanism, and the fixed components are used to fix the wing.

[0035] Specifically, in order to solve the problems in the prior art that large-sized UAV wings have large transportation volume, high protection requirements, and are inconvenient to transport; the wing vibration reduction and protection transportation device provided by the present invention has a box 1, a transport frame 2 and a vibration reduction mechanism. The wing can be placed on the upper side of the vibration reduction mechanism and placed in the accommodating space in the transport frame 2. The elastic components between the vibration reduction mechanism and the transport frame 2 are used to reduce the vibration of the wing to reduce the vibration impact during the transportation of the wing. At the same time, the transport frame 2 loaded with the wing is placed in the box 1, which can be protected by the box 1 to protect the wing during transportation.

[0036] Optionally, the box body 1 is a rectangular box, and box doors 3 are respectively provided at both ends of the box body 1.

[0037] Specifically, the doors 3 at both ends of the box body 1 can be opened and closed so that the transport rack 2 can enter and exit the box body 1 .

[0038] Optionally, a lock is provided on the inner wall of the box body 1 , and the lock is detachably connected to the transport frame 2 .

[0039] Specifically, when the transport rack 2 is placed in the box body 1 , the lock buckles on the inner wall of the box body 1 can be connected with the transport rack 2 to fix the transport rack 2 in the box body 1 .

[0040] In this embodiment, the lock buckle may be a lock plate with a lock hole connected to the inner wall of the box body 1 , and the lock plate may be fastened to the transport frame 2 via a connecting plate using bolt fasteners.

[0041] In this embodiment, the lock includes a bottom plate lock 4 and a side wall lock 5 .

[0042] Optionally, casters 6 are provided at the bottom of the transport frame 2 .

[0043] Specifically, the provision of the casters 6 can facilitate the movement of the transport rack 2 , thereby facilitating the transport rack 2 to enter and exit the box body 1 .

[0044] Optionally, the caster 6 is connected to the transport frame 2 via a lifting mechanism.

[0045] Specifically, the casters 6 are liftable, which not only facilitates the adjustment of the height of the transport rack 2 , but also enables the heights of both ends of the transport rack 2 to be adjusted when the transport rack 2 is moved out of the box 1 .

[0046] In this embodiment, the lifting mechanism includes a hydraulic cylinder that can be manually operated.

[0047] Optionally, the transport rack 2 includes a rectangular frame 7 and a trapezoidal frame 8 arranged on both sides of the long sides of the rectangular frame 7 , and the lifting mechanism and the casters 6 are arranged on the outside of the rectangular frame 7 and do not protrude from the trapezoidal frame 8 .

[0048] Specifically, the caster 6 is connected to the outer side of the rectangular frame 7 through a lifting mechanism, so that when two transport frames 2 are stacked, the caster 6 and the lifting mechanism do not mechanically interfere with the rectangular frame 7 below, and the caster 6 can also be configured to be fully retracted to the upper side of the bottom surface of the rectangular mining machine.

[0049] Optionally, the box body 1 is a heat-insulating box.

[0050] Specifically, the box body 1 adopts a heat-insulating box with heat-insulating functions, which can further improve the protection effect on the wing.

[0051] Optionally, at least two transport racks 2 are provided, and at least two transport racks 2 are stacked and can be placed in the box body 1 .

[0052] Specifically, the stacked transport racks 2 can effectively utilize the space in the box 1 and improve the transport efficiency.

[0053] In this embodiment, if Figure 4 As shown, three transport racks 2 are provided to form three-layer stacked transport racks 2 .

[0054] Optionally, the vibration reduction mechanism includes a base frame 9, a plurality of mounting plates 10 are arranged on the upper side of the base frame 9, a conformable sponge 11 is arranged on the upper side of the mounting plate 10, the upper surface of the conformable sponge 11 cooperates with the lower wing surface of the wing, and the base frame 9 is connected to the bottom of the transport frame 2 through an elastic component.

[0055] Specifically, the base frame 9 is connected to the bottom of the transport frame 2 through an elastic component, so that the entire base frame 9 is suspended on the transport frame 2, and a conformable sponge 11 is installed on the mounting plate 10 above the base frame 9. The upper surface of the conformable sponge 11 coincides with the lower wing surface of the wing, and the conformable sponge 11 is arranged to support the wing.

[0056] In this embodiment, the elastic component is a spring.

[0057] In this embodiment, the base frame 9 includes three longitudinal beams and two transverse beams, which are welded to form a U-shaped structure. A plurality of mounting plates 10 are arranged at intervals on the upper side of the two longitudinal beams for mounting conformable sponges 11. The conformable sponges 11 coincide with the lower wing surface of the wing to achieve elastic support for the wing, and the wing is fixed by fixing components on both sides.

[0058] Optionally, the fixing component includes a base 12, which is connected to the base frame 9. A lower holding ring 13 is provided on the upper side of the base 12, and an upper holding ring 14 is detachably connected to the upper side of the lower holding ring 13. The upper holding ring 14 is connected to the lower holding ring 13 to form a complete holding ring structure, and the wing is fixed by the holding ring structure.

[0059] Specifically, the fixing component is located at the left and right ends of the base frame 9, and fixes the wing section of the wing in the form of a ring; a lower ring 13 is integrally formed on the upper side of the base 12 of the fixing component, and an upper ring 14 can be fastened to the lower ring 13 by bolts, and the base 12 can be fixed to the base frame 9 by bolts.

[0060] The embodiments of the present invention have been described above, and the above description is exemplary, not exhaustive, and is not limited to the disclosed embodiments. Many modifications and changes will be apparent to those skilled in the art without departing from the scope and spirit of the described embodiments.

Claims

1. A wing vibration reduction and protection transport device, characterized in that: include: Box; A transport rack, the transport rack is detachably arranged in the box, and a receiving space is formed inside the transport rack, and the receiving space is used to receive the wing; A vibration-damping mechanism is arranged at the bottom of the accommodating space and connected to the transport frame through an elastic component. The upper side of the vibration-damping mechanism is used to place the wing. Fixing components are arranged at both ends of the vibration-damping mechanism, and the fixing components are used to fix the wing.

2. The wing vibration reduction and protection transportation device according to claim 1, characterized in that: The box body is a rectangular box, and box doors are respectively arranged at two ends of the box body.

3. The wing vibration reduction and protection transportation device according to claim 1, characterized in that: The inner wall of the box body is provided with a lock buckle, and the lock buckle is detachably connected to the transport rack.

4. The wing vibration reduction and protection transportation device according to claim 1, characterized in that: Casters are arranged at the bottom of the transport frame.

5. The wing vibration reduction and protection transportation device according to claim 4, characterized in that: The caster is connected to the transport frame through a lifting mechanism.

6. The wing vibration reduction and protection transportation device according to claim 5, characterized in that: The transport rack comprises a rectangular frame and a trapezoidal frame arranged on both sides of the long sides of the rectangular frame, and the lifting mechanism and the casters are arranged on the outside of the rectangular frame and do not protrude from the trapezoidal frame.

7. The wing vibration reduction and protection transportation device according to claim 1, characterized in that: The box body is a heat-insulating box.

8. The wing vibration reduction and protection transportation device according to claim 1, characterized in that: At least two transport racks are provided, and at least two transport racks are stacked and can be placed in the box.

9. The wing vibration reduction and protection transportation device according to claim 1, characterized in that: The vibration reduction mechanism includes a base frame, a plurality of mounting plates are arranged on the upper side of the base frame, a conformable sponge is arranged on the upper side of the mounting plates, the upper surface of the conformable sponge cooperates with the lower wing surface of the wing, and the base frame is connected to the bottom of the transport frame through the elastic component.

10. The wing vibration reduction and protection transportation device according to claim 9, characterized in that: The fixing component includes a base, which is connected to the base frame. A lower holding ring and an upper holding ring are provided on the upper side of the base. The upper holding ring and the lower holding ring are connected to form a complete holding ring structure, and the wing is fixed by the holding ring structure.

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