CN219928347U - Fixed wing unmanned aerial vehicle fixing device and storage and transportation device - Google Patents
Fixed wing unmanned aerial vehicle fixing device and storage and transportation device Download PDFInfo
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- CN219928347U CN219928347U CN202321432520.0U CN202321432520U CN219928347U CN 219928347 U CN219928347 U CN 219928347U CN 202321432520 U CN202321432520 U CN 202321432520U CN 219928347 U CN219928347 U CN 219928347U
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- 238000004806 packaging method and process Methods 0.000 abstract description 6
- 230000007704 transition Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 229920001821 foam rubber Polymers 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a fixed wing unmanned aerial vehicle fixing device and a storage and transportation device, and relates to the technical field of unmanned aerial vehicle packaging and transportation. The utility model solves the technical problems of lower packaging reliability and troublesome disassembly and assembly of the fixed wing unmanned aerial vehicle during transition transportation. The fixed wing unmanned aerial vehicle fixing device comprises a first limiting piece, a second limiting piece, a buffer cushion and at least one main body frame; the main body frame comprises a plurality of placing chambers which are respectively matched with the fuselage, the propeller, the first tail wing, the second tail wing, the third tail wing and the wings; the front end and/or the rear end of the fuselage, the first tail wing, the second tail wing, the third tail wing and the wings are/is provided with a first limiting part, and are/is fixed by a second limiting part along the circumference of the first limiting part, and the joint of the first limiting part and the main body frame is provided with a buffer pad. The fixed wing unmanned aerial vehicle is classified and stored, and operating personnel can conveniently and rapidly install and detach. Therefore, the fixed wing unmanned aerial vehicle fixing device disclosed by the utility model is simple in structure, high in reliability, high in transportation efficiency and convenient to use and maintain.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle packaging and transportation, and particularly relates to a fixed wing unmanned aerial vehicle fixing device and a storage and transportation device.
Background
The fixed wing unmanned aerial vehicle has the unique advantages of long endurance time, high speed, large load and the like. For example, in the field of inspection, the fixed-wing unmanned aerial vehicle is also a sharp tool for remotely inspecting circuits and pipelines in remote areas. If the fixed wing unmanned aerial vehicle flies according to the set route, the route of tens or even hundreds of kilometers can be patrolled at one time, and the fixed wing unmanned aerial vehicle is used for patrolling and checking, so that the working efficiency is improved, and the burden of patrolling personnel is reduced.
However, most of existing fixed wing unmanned aerial vehicles adopt packaging box transfer transportation, so that not only are the fixing modes complex, the packaging reliability and the safety are low, but also the disassembly and assembly are relatively troublesome, and time and labor are wasted.
Disclosure of Invention
The embodiment of the utility model provides the fixed wing unmanned aerial vehicle fixing device and the storage and transportation device, which solve the technical problems of lower packaging reliability and troublesome disassembly and assembly of the fixed wing unmanned aerial vehicle in the prior art during transition transportation.
In a first aspect, an embodiment of the present utility model provides a fixed wing unmanned aerial vehicle fixing device, including a first limiting member, a second limiting member, a cushion pad, and at least one main body frame; the main body frame comprises a plurality of placing chambers which are respectively matched with the fuselage, the propeller, the first tail wing, the second tail wing, the third tail wing and the wings; the fuselage, the first fin, the second fin, the third fin and the front end and/or the rear end of the wing are/is provided with first locating parts, and are fixed by second locating parts along the circumference thereof, and the buffer pad is arranged at the joint of the buffer pad and the main body frame.
With reference to the first aspect, in one possible implementation manner, the main body frame includes three layers of subframes; the middle part of the first layer of the subframe is provided with the placing cavity for placing the airframe, and two sides of the first layer of the subframe are respectively provided with the placing cavity for placing the propeller and the first tail wing; the second layer of the subframe is provided with the placing cavity for placing the second tail wing along the length direction of the subframe, and is provided with the placing cavity for placing the third tail wing along the width direction of the subframe; and the subframe of the third layer is provided with the placing cavity for placing the wing.
With reference to the first aspect, in one possible implementation manner, the first layer of the subframe is located at a lower layer, the second layer of the subframe is located at a middle layer, and the third layer of the subframe is located at an upper layer.
With reference to the first aspect, in one possible implementation manner, the placement chambers for placing the first tail wing and the second tail wing are all L-shaped structures.
With reference to the first aspect, in one possible implementation manner, the placement chambers in which the first tail wing and the second tail wing are placed are disposed in parallel along a height direction of the main body frame.
With reference to the first aspect, in one possible implementation manner, the fixed wing unmanned aerial vehicle fixing device further includes a clamping piece; the clamping piece is arranged in the placing cavity for placing the propeller, and the propeller is clamped in the clamping piece.
With reference to the first aspect, in one possible implementation manner, the fixed wing unmanned aerial vehicle fixing device further includes a plurality of moving wheels; the movable wheels are detachably arranged at the bottom of the main body frame.
With reference to the first aspect, in one possible implementation manner, the fixed wing unmanned aerial vehicle fixing device further includes a fixing frame; the fixing frame is detachably connected to the top of the main body frame.
In a second aspect, an embodiment of the present utility model provides a storage and transportation device, including the fixed wing unmanned aerial vehicle fixing device according to the first aspect or any one of the possible implementation manners of the first aspect.
One or more technical solutions provided in the embodiments of the present utility model at least have the following technical effects:
the fixed wing unmanned aerial vehicle fixing device provided by the embodiment of the utility model comprises a first limiting piece, a second limiting piece, a buffer cushion and at least one main body frame. The main body frame comprises a plurality of placing chambers which are respectively matched with the fuselage, the propeller, the first tail wing, the second tail wing, the third tail wing and the wings. Each part of the fixed wing unmanned aerial vehicle is stored in a classified mode, so that operators can conveniently and rapidly install and detach the fixed wing unmanned aerial vehicle, and the fixed wing unmanned aerial vehicle can be quickly transferred into a use state from a transportation state. The first limiting piece and the second limiting piece can limit the displacement of each part of the fixed wing unmanned aerial vehicle, and the reliability and the safety of the fixed wing unmanned aerial vehicle in the storage and transportation process are improved. The cushion pad can prevent the parts of the fixed wing unmanned aerial vehicle from being worn. Therefore, the fixed wing unmanned aerial vehicle fixing device disclosed by the utility model is simple in structure, high in reliability, high in transportation efficiency and convenient to use and maintain.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed in the description of the embodiments of the present utility model will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present utility model, and other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic structural diagram of a fixing device for a fixed wing unmanned aerial vehicle according to an embodiment of the present utility model;
fig. 2 is a top view of a fixed wing unmanned aerial vehicle fixing device according to an embodiment of the present utility model;
fig. 3 is a front view of a fixed wing unmanned aerial vehicle fixing device according to an embodiment of the present utility model;
fig. 4 is a schematic structural diagram of a fixing manner of a machine body according to an embodiment of the present utility model.
Reference numerals: 1-a main body frame; 11a, 11b, 11c, 11d, 11e, 11 f-placement chamber; 12-subframes; 2-a first limiting piece; 3-a second limiting piece; 4-clamping pieces; 5-moving wheels; 6-cushion pad.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are some, but not all embodiments of the utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
In the description of the embodiments of the present utility model, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like indicate or are based on the orientation or positional relationship shown in the drawings, merely to facilitate description of the embodiments of the present utility model and simplify description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model. The terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. Furthermore, the terms "mounted," "connected," "coupled," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the embodiments of the present utility model will be understood by those of ordinary skill in the art according to specific circumstances.
As shown in fig. 1, 11a is a placing chamber for placing a wing, 11b is a placing chamber for placing a second tail wing, 11c is a placing chamber for placing a third tail wing, 11d is a placing chamber for placing a first tail wing, 11e is a placing chamber for placing a fuselage, and 11f is a placing chamber for placing a propeller.
As shown in fig. 1 to 4, the fixing device for a fixed wing unmanned aerial vehicle provided by the embodiment of the utility model comprises a first limiting piece 2, a second limiting piece 3, a cushion pad 6 and at least one main body frame 1. The main body frame 1 includes a plurality of placement chambers 11e, 11f, 11d, 11b, 11c, 11a respectively adapted to the fuselage, the propeller, the first tail, the second tail, the third tail, and the wing. Each part of the fixed wing unmanned aerial vehicle is stored in a classified mode, and operators can install and detach each part rapidly, so that the fixed wing unmanned aerial vehicle can be transferred from a transportation state to a use state more rapidly. The front end and/or the rear end of the fuselage, the first tail wing, the second tail wing, the third tail wing and the wings are provided with first limiting pieces 2, and are fixed by second limiting pieces 3 along the circumferential direction, and buffer pads 6 are arranged at the joints of the fuselage, the first tail wing, the second tail wing, the third tail wing and the wings. The front end of fuselage, first fin, second fin, third fin and wing is provided with first locating part 2 or fuselage, first fin, second fin, third fin and the rear end of wing are provided with first locating part 2 or fuselage, first fin, second fin, third fin, the front end and the rear end of wing all are provided with first locating part 2. The first limiting piece 2 and the second limiting piece 3 can prevent each part of the fixed wing unmanned aerial vehicle from shifting, and reliability and safety of the fixed wing unmanned aerial vehicle in the storage and transportation process are improved. The cushion 6 prevents the components of the fixed wing drone from being worn. Specifically, the cushion pad 6 is a 10mm rubber foam pad. Therefore, the fixed wing unmanned aerial vehicle fixing device provided by the embodiment of the utility model has the advantages of simple structure, high reliability, simplicity and convenience in operation and transportation efficiency, and simplicity and convenience in use and maintenance.
As shown in fig. 4, specifically, the first limiting member 2 is a rubber pad, and the second limiting member 3 is a tightening strap. The tightening strap is fixed with the main body frame 1 through bolts.
As shown in fig. 1 and 3, the main body frame 1 includes three layers of subframes 12. The middle part of the first layer subframe 12 is provided with a placing cavity 11e for placing the airframe, and two sides of the first layer subframe are respectively provided with placing cavities 11f and 11d for placing the propeller and the first tail wing. The second-layer subframe 12 is provided with a placement chamber 11b for placing the second tail along its length direction and a placement chamber 11c for placing the third tail along its width direction. The third subframe 12 is provided with a placement chamber 11a in which the wing is placed. Specifically, two wings are placed on the placement chamber 11a rotationally symmetrically.
Further, the first sub-frame 12 is located at the lower layer, the second sub-frame 12 is located at the middle layer, and the third sub-frame 12 is located at the upper layer. The machine body is relatively heavy and is positioned at the lower layer, so that the whole device is more stable.
Further, the placement chamber 11e for placing the airframe is provided with a groove for accommodating the bottom of the airframe, so that the airframe can be placed in the placement chamber 11e more quickly. The subframe 12 located at the lower layer is provided with a plurality of beams in the width direction thereof and a support beam in the diagonal line thereof, so that the structure of the whole fixed wing unmanned aerial vehicle is more stable.
Further, two wings are placed on the upper layer, the root parts of the two wings are butted with the main body frame 1, and the two wings are fixed through bolts. The wing is limited up and down by the second limiting piece 3. Where the two wings contact the subframe 12, a cushion 6 is provided. Specifically, the cushion pad 6 is a 10mm rubber foam pad.
In one implementation manner of the embodiment of the present utility model, the placement chambers 11d and 11b for placing the first tail wing and the second tail wing are both L-shaped structures. The first fin and the second fin are L-shaped structures, and the placing chambers 11d and 11b for placing the first fin and the second fin are matched with the shapes of the first fin and the second fin, so that the structure of the whole device is more compact, and the space can be better utilized.
In one implementation of the embodiment of the present utility model, the placement chambers 11d, 11b in which the first and second tail wings are placed are arranged in parallel along the height direction of the main body frame 1. The fixed wing unmanned aerial vehicle fixing device provided by the embodiment of the utility model reasonably utilizes space, has a compact structure and is convenient to use.
As shown in fig. 3, the fixed wing unmanned aerial vehicle fixing device further comprises a clamping piece 4. The clamping piece 4 is arranged in a placing cavity 11f for placing the propeller, and the propeller is clamped in the clamping piece 4, so that the propeller can be limited.
With continued reference to fig. 3, the fixed wing drone fixture also includes a plurality of moving wheels 5. The plurality of moving wheels 5 are detachably arranged at the bottom of the main body frame 1. When the installer needs to move the fixed wing unmanned aerial vehicle fixing device, the labor can be saved, and the fixed wing unmanned aerial vehicle fixing device is convenient to use.
In an implementation manner of the embodiment of the utility model, the fixed wing unmanned aerial vehicle fixing device further comprises a fixing frame. The fixing frame is detachably connected to the top of the main body frame 1. If the main body frame 1 is provided with a plurality of, the fixing frame can prevent the parts of the fixed wing unmanned aerial vehicle on the uppermost layer from being damaged. Specifically, if the wing is placed on top of the main body frame 1, the height of the fixing frame is greater than the height of the wing, so that the upper main body frame 1 can be prevented from crushing the wing located in the lower main body frame 1. Therefore, the fixed wing unmanned aerial vehicle fixing device provided by the embodiment of the utility model is simple in structure, and the safety and reliability of the fixed wing unmanned aerial vehicle in the transportation process are improved.
Further, the main body frame 1 may be a 316L stainless steel profile.
In addition, the embodiment of the utility model provides a storage and transportation device, which comprises the fixed wing unmanned aerial vehicle fixing device.
Specifically, the storage and transportation device of the embodiment of the present utility model can place two main body frames 1, and place up and down. The overall device dimensions were 5500mm x 2161mm x 2100mm. In transportation, the bottom of the main body frame 1 is detachably connected with the bottom plate of the storage and transportation device, so that the fixed wing unmanned aerial vehicle fixing device is safer and more reliable in transportation.
In this specification, each embodiment is described in a progressive manner, and the same or similar parts of each embodiment are referred to each other, and each embodiment is mainly described as a difference from other embodiments.
The above embodiments are only for illustrating the technical solution of the present utility model, and not for limiting the present utility model; although the utility model has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some or all of the technical features thereof can be replaced with equivalents; such modifications and substitutions do not depart from the spirit of the utility model.
Claims (9)
1. The fixed wing unmanned aerial vehicle fixing device is characterized by comprising a first limiting piece, a second limiting piece, a buffer cushion and at least one main body frame;
the main body frame comprises a plurality of placing chambers which are respectively matched with the fuselage, the propeller, the first tail wing, the second tail wing, the third tail wing and the wings;
the fuselage, the first fin, the second fin, the third fin and the front end and/or the rear end of the wing are/is provided with first locating parts, and are fixed by second locating parts along the circumference thereof, and the buffer pad is arranged at the joint of the buffer pad and the main body frame.
2. The fixed wing unmanned aerial vehicle fixation device of claim 1, wherein the main body frame comprises a three-layer subframe;
the middle part of the first layer of the subframe is provided with the placing cavity for placing the airframe, and two sides of the first layer of the subframe are respectively provided with the placing cavity for placing the propeller and the first tail wing;
the second layer of the subframe is provided with the placing cavity for placing the second tail wing along the length direction of the subframe, and is provided with the placing cavity for placing the third tail wing along the width direction of the subframe;
and the subframe of the third layer is provided with the placing cavity for placing the wing.
3. The fixed wing unmanned aerial vehicle of claim 2, wherein the first layer of subframes is positioned on a lower layer, the second layer of subframes is positioned on a middle layer, and the third layer of subframes is positioned on an upper layer.
4. A fixed wing unmanned aerial vehicle fixing device according to claim 2 or claim 3, wherein the placement chambers in which the first and second flight are placed are of L-shaped configuration.
5. The fixed wing unmanned aerial vehicle fixing device of claim 4, wherein the placement chamber in which the first tail and the second tail are placed is disposed in parallel along a height direction of the main body frame.
6. The fixed wing unmanned aerial vehicle fixation device of claim 1, further comprising a clip;
the clamping piece is arranged in the placing cavity for placing the propeller, and the propeller is clamped in the clamping piece.
7. The fixed wing unmanned aerial vehicle fixation device of claim 1, further comprising a plurality of moving wheels;
the movable wheels are detachably arranged at the bottom of the main body frame.
8. The fixed wing unmanned aerial vehicle fixation device of claim 1, further comprising a fixation frame;
the fixing frame is detachably connected to the top of the main body frame.
9. A storage and transportation device comprising a fixed wing unmanned aerial vehicle fixing device according to any of claims 1 to 8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321432520.0U CN219928347U (en) | 2023-06-07 | 2023-06-07 | Fixed wing unmanned aerial vehicle fixing device and storage and transportation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321432520.0U CN219928347U (en) | 2023-06-07 | 2023-06-07 | Fixed wing unmanned aerial vehicle fixing device and storage and transportation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219928347U true CN219928347U (en) | 2023-10-31 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321432520.0U Active CN219928347U (en) | 2023-06-07 | 2023-06-07 | Fixed wing unmanned aerial vehicle fixing device and storage and transportation device |
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| Country | Link |
|---|---|
| CN (1) | CN219928347U (en) |
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2023
- 2023-06-07 CN CN202321432520.0U patent/CN219928347U/en active Active
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