CN212473904U - Oil-electricity hybrid's transportation unmanned aerial vehicle - Google Patents

Oil-electricity hybrid's transportation unmanned aerial vehicle Download PDF

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CN212473904U
CN212473904U CN202021242769.1U CN202021242769U CN212473904U CN 212473904 U CN212473904 U CN 212473904U CN 202021242769 U CN202021242769 U CN 202021242769U CN 212473904 U CN212473904 U CN 212473904U
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groups
rods
positioning
aerial vehicle
unmanned aerial
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CN202021242769.1U
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张瑞峰
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Shenzhou Huayi Agricultural Technology Co ltd
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Shenzhou Huayi Agricultural Technology Co ltd
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Abstract

The utility model discloses a hybrid's transportation unmanned aerial vehicle, an organism, the link, four dead levers of group, four fixed sleeves of group, hold the case, two sets of side layer boards, two sets of first telescopic links, four locating levers of group, four reference columns of group, four positioning spring of group, four threaded rods of group, four telescopic sleeve of group and two sets of side shield, the bottom of organism is connected with the top of link, the bottom of link is connected with the top of holding the case, it holds the chamber to hold the incasement, the one end of two sets of first telescopic links respectively with the antetheca and the back wall connection that hold the chamber, the other end of two sets of first telescopic links is connected with the outside of two sets of side layer boards respectively, two sets of fixed sleeve's top all is connected with the bottom that holds the case, four dead levers of group all include folding rod and extension rod, four. The utility model discloses, can be applicable to the transportation of length no room that is greater than express delivery box or express delivery storehouse, reduced transportation unmanned aerial vehicle's use limitation.

Description

Oil-electricity hybrid's transportation unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a hybrid power's transportation unmanned aerial vehicle.
Background
The unmanned aerial vehicle is also called as unmanned aerial vehicle or remote control piloted aircraft, is an unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device, has the characteristics of high portability, flexible use and the like, is a hybrid unmanned aerial vehicle, is a novel dual-power unmanned aerial vehicle, has a power system consisting of two power systems of an electric drive and a conventional engine so as to realize the combination of good take-off and climbing performances, silence and ultra-long endurance, and introduces the unmanned aerial vehicle in the operation of various industries such as land measurement, agricultural plant protection, low-altitude logistics, deep forest fire prevention and the like along with the development of science and technology, wherein the low-altitude transportation unmanned aerial vehicle used in the low-altitude logistics industry mainly carries packages by the unmanned low-altitude aircraft operated by the radio remote control equipment and the self-contained program control device and automatically reaches the destination, and has the main advantages of improving the distribution efficiency, reduce the human cost, current low latitude transport unmanned aerial vehicle (express delivery unmanned aerial vehicle) all loads through setting up express delivery box, perhaps express delivery storehouse and treats the transportation express delivery, but because the space in express delivery box, express delivery storehouse is restricted, its parcel that is suitable for the rule (for example, rectangular bodily form) transports, and to long rod-shaped etc. then comparatively difficult is transported of the article that length is greater than express delivery box or express delivery storehouse.
Therefore, an oil-electricity hybrid transport unmanned aerial vehicle is provided.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a hybrid's transport unmanned aerial vehicle of oil electricity can be applicable to the transportation of length no room that is greater than express delivery box or express delivery storehouse, has reduced transport unmanned aerial vehicle's use limitation to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: an oil-electricity hybrid transportation unmanned aerial vehicle comprises a body, a connecting frame, four groups of fixing rods, four groups of fixing sleeves, a containing box, two groups of side supporting plates, two groups of first telescopic rods, four groups of positioning columns, four groups of positioning springs, four groups of threaded rods, four groups of telescopic sleeves and two groups of side baffle plates, wherein the bottom end of the body is connected with the top end of the connecting frame, the bottom end of the connecting frame is connected with the top end of the containing box, a containing cavity is arranged in the containing box, one end of each of the two groups of first telescopic rods is respectively connected with the front wall and the rear wall of the containing cavity, the other end of each of the two groups of first telescopic rods is respectively connected with the outer sides of the two groups of side supporting plates, the top ends of the two groups of fixing sleeves are respectively connected with the bottom end of the containing box, the four groups of, the outer sides of the four groups of the extension rods are respectively hinged with one end of each of the four groups of the folding rods, the other ends of the four groups of the folding rods are respectively connected with one end of each of the four groups of the positioning rods, positioning cavities are respectively formed in the four groups of the extension rods and one end of each of the four groups of the fixing sleeves, a plurality of groups of positioning holes are formed in the side walls of the four groups of the fixing sleeves, one ends of the four groups of the positioning springs are respectively connected with the side walls of the four groups of the positioning cavities, the other ends of the four groups of the positioning springs are respectively connected with one ends of the four groups of the positioning columns, the other ends of the four groups of the positioning columns respectively penetrate through the four groups of the extension rods and the four groups of the positioning holes, the side walls of the four groups of the telescopic sleeves are respectively connected with.
Preferably, the top ends of the four positioning rods are provided with buckles, the left part and the right part of the connecting frame are provided with two clamping seats, and the four groups of buckles are respectively matched with the four groups of clamping seats.
Preferably, the telescopic rod further comprises four groups of positioning sleeves, the four groups of positioning sleeves are respectively sleeved with the four groups of extension rods, and one ends of the four groups of positioning sleeves are respectively screwed with the four groups of fixing sleeves.
Preferably, the outer sides of the ends, connected with the four groups of folding rods, of the four groups of extension rods are provided with external threads, and the four groups of positioning sleeves are provided with internal threads.
Preferably, the storage box further comprises a lower top plate and a second telescopic rod, the top end of the second telescopic rod is connected with the upper wall of the containing cavity, and the bottom end of the second telescopic rod is connected with the top end of the lower top plate.
Preferably, the device also comprises four groups of turntables, and the top ends of the four groups of turntables are respectively connected with the bottom ends of the four groups of threaded rods.
Preferably, the two groups of side supporting plates, the two groups of side baffles and the lower top plate are provided with protective layers.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses, when loading the goods of shape rule, the user contracts the extension rod in the fixed sleeve, and upwards rotate the folding rod at the junction with the extension rod, connect locating lever and link, the user can drive the side layer board to move through adjusting first telescopic link according to the size of goods, thereby fix the goods in the front-back direction, the user can make the side layer board cling to the folding rod through rotating the threaded rod, the threaded rod and the telescopic sleeve relatively move, the threaded rod drives the side shield to move, thereby fix the goods in the left-right direction, when loading the goods of longer length, the user can rotate the folding rod into the state horizontal with the extension rod, then make the side shield cling to the folding rod through the threaded rod, the user inwards presses the locating column, make the locating column slide into the locating hole, pull out the extension rod according to the length of goods, then load the goods and hold the case back, inwards adjust the extension rod, make the locating lever hug closely with the left end and the right-hand member of goods to fixed with the goods, reached and to have been applicable to the transportation that length is greater than the nothing in express delivery box or express delivery storehouse, reduced transportation unmanned aerial vehicle's use limitation.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic sectional structure of the present invention;
fig. 3 is a schematic left-side sectional structure of the present invention;
fig. 4 is a schematic diagram of a partially enlarged structure at a position in fig. 3 according to the present invention.
In the figure: 1. a body; 2. a connecting frame; 3. fixing the sleeve; 4. a containing box; 5. a side fascia; 6. a first telescopic rod; 7. a positioning column; 8. a positioning spring; 9. a threaded rod; 10. a telescopic sleeve; 11. a side dam; 12. a folding bar; 13. an extension rod; 14. buckling; 15. a card holder; 16. a positioning sleeve; 17. a lower top plate; 18. a second telescopic rod; 19. a turntable; 20. a protective layer; 21. and (5) positioning the rod.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are used merely for convenience of description and for simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," 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; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1 to 4, the present invention provides a technical solution:
an oil-electricity hybrid transportation unmanned aerial vehicle is shown in figures 1-4, and comprises a machine body 1, a connecting frame 2, four groups of fixing rods, four groups of fixing sleeves 3, a containing box 4, two groups of side supporting plates 5, two groups of first telescopic rods 6, four groups of positioning rods 21, four groups of positioning columns 7, four groups of positioning springs 8, four groups of threaded rods 9, four groups of telescopic sleeves 10 and two groups of side baffles 11, wherein the bottom end of the machine body 1 is connected with the top end of the connecting frame 2, the bottom end of the connecting frame 2 is connected with the top end of the containing box 4, a containing cavity is arranged in the containing box 4, one ends of the two groups of first telescopic rods 6 are respectively connected with the front wall and the rear wall of the containing cavity, the other ends of the two groups of first telescopic rods 6 are respectively connected with the outer sides of the two groups of side supporting plates 5, the top ends of the, the four groups of fixing rods comprise folding rods 12 and extension rods 13, the four groups of extension rods 13 are respectively sleeved with four groups of fixing sleeves 3, the outer sides of the four groups of extension rods 13 are respectively hinged with one ends of the four groups of folding rods 12, the other ends of the four groups of folding rods 12 are respectively connected with one ends of four groups of positioning rods 21, one ends of the four groups of extension rods 13 respectively sleeved with the four groups of fixing sleeves 3 are respectively provided with a positioning cavity, the side walls of the four groups of fixing sleeves 3 are provided with a plurality of groups of positioning holes, one ends of four groups of positioning springs 8 are respectively connected with the side walls of the four groups of positioning cavities, the other ends of the four groups of positioning springs 8 are respectively connected with one ends of four groups of positioning columns 7, the other ends of the four groups of positioning columns 7 respectively penetrate through the four groups of extension rods 13 and the four groups of positioning holes, and the side, the top ends of the four groups of threaded rods 9 are respectively screwed and penetrate through the four groups of telescopic sleeves 10 to be respectively and rotatably connected with the front part and the rear part of the bottom ends of the two groups of side baffles 11;
specifically, as shown in fig. 1, the top ends of the four positioning rods 21 are provided with two sets of buckles 14, the left part and the right part of the connecting frame 2 are provided with two sets of clamping seats 15, and the four sets of buckles 14 are respectively matched with the four sets of clamping seats 15.
Through adopting above-mentioned technical scheme, folding rod 12 is foldable, and the user can cooperate through buckle 14 and cassette 15 to fix locating lever 21, has strengthened transportation unmanned aerial vehicle's stability.
Specifically, as shown in fig. 2, the telescopic rod further includes four sets of positioning sleeves 16, the four sets of positioning sleeves 16 are respectively sleeved with the four sets of extension rods 13, and one end of each of the four sets of positioning sleeves 16 is respectively screwed with the four sets of fixing sleeves 3.
Through adopting above-mentioned technical scheme, when folding rod 12 and extension rod 13 were in same straight line, the user with 16 suit of position sleeve at folding rod 12 and extension rod 13's junction, can prevent folding rod 12 and roll over downwards, influence the normal use of dead lever, strengthened transportation unmanned aerial vehicle's stability.
Specifically, as shown in fig. 2, the outer sides of the ends of the four groups of extension rods 13 connected to the four groups of folding rods 12 are provided with external threads, and the four groups of positioning sleeves 16 are provided with internal threads.
Through adopting above-mentioned technical scheme, the user can prevent that 16 take place to slide of position sleeve from causing folding rod 12 to roll over downwards through external screw thread and internal thread mesh mutually, has strengthened transportation unmanned aerial vehicle's reliability and security.
Specifically, as shown in fig. 2, the container further comprises a lower top plate 17 and a second telescopic rod 18, wherein the top end of the second telescopic rod 18 is connected with the upper wall of the containing cavity, and the bottom end of the second telescopic rod 18 is connected with the top end of the lower top plate 17.
Through adopting above-mentioned technical scheme, the user can drive down roof 17 through adjusting second telescopic link 18 and remove, and roof 17 can be fixed the goods with the lower part cooperation that holds case 4 in the upper and lower direction down, has strengthened transportation unmanned aerial vehicle's stability.
Specifically, as shown in fig. 1, the device further comprises four groups of rotating discs 19, and the top ends of the four groups of rotating discs 19 are respectively connected with the bottom ends of the four groups of threaded rods 9.
Through adopting above-mentioned technical scheme, the user can drive threaded rod 9 through rotating carousel 19 and rotate to control side shield 11's removal has strengthened transportation unmanned aerial vehicle's convenience.
Specifically, as shown in fig. 3, the two sets of side supporting plates 5, the two sets of side baffles 11 and the lower top plate 17 are all provided with a protective layer 20.
Through adopting above-mentioned technical scheme, inoxidizing coating 20 can play the guard action to the goods, prevents that the goods from being caused the damage by side layer board 5, side shield 11 and roof 17 down, has strengthened unmanned aerial vehicle's security.
The working principle is as follows: when loading goods with regular shapes, a user retracts the extension rod 13 into the fixed sleeve 3, the folding rod 12 is upwards rotated at the joint of the extension rod 13, the positioning rod 21 is connected with the connecting frame 2, the user can drive the side supporting plate 5 to move by adjusting the first telescopic rod 6 according to the size of the goods, so that the goods are fixed in the front-back direction, the user can rotate the threaded rod 9, the threaded rod 9 and the telescopic sleeve 10 move relatively, the threaded rod 9 drives the side baffle plate 11 to move, so that the goods are fixed in the left-right direction, when loading goods with longer length, the user can rotate the folding rod 12 to be horizontal to the extension rod 13, then the side baffle plate 11 is tightly attached to the folding rod 12 through the threaded rod 9, the user presses the positioning column 7 inwards to enable the positioning column 7 to slide into the positioning hole, the extension rod 13 is pulled out according to the length of the goods, then hold case 4 back with the freight loading, inwards adjust extension rod 13, make locating lever 21 hug closely with the left end and the right-hand member of goods to fixed with the goods, reached and to have been applicable to the transportation that length is greater than the nothing of express delivery box or express delivery storehouse, reduced transportation unmanned aerial vehicle's use limitation.
The utility model discloses the use of organism 1 and above-mentioned part that adopts all adopts the utility model provides a background data is given, and cooperate the utility model discloses a description of specification, affiliated technical field personnel can reach its use to obtain corresponding result of use, the event does not have the one-by-one.
The utility model provides a product model is only for the use that this technical scheme goes on according to the structural feature of product, and its product can be adjusted and reform transform after purchasing, makes it match more and accord with the utility model belongs to technical scheme, it is the technical scheme of an optimal application of this technical scheme, and the model of its product can be replaced and reform transform according to the technical parameter of its needs, and it is familiar for technical staff that belongs to in the field, consequently, what technical staff that belongs to in the field can be clear passes through the utility model provides a technical scheme obtains corresponding result of use.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. The utility model provides a hybrid's transportation unmanned aerial vehicle which characterized in that: the machine body (1), a connecting frame (2), four groups of fixing rods, four groups of fixing sleeves (3), a containing box (4), two groups of side supporting plates (5), two groups of first telescopic rods (6), four groups of positioning rods (21), four groups of positioning columns (7), four groups of positioning springs (8), four groups of threaded rods (9), four groups of telescopic sleeves (10) and two groups of side baffles (11), wherein the bottom end of the machine body (1) is connected with the top end of the connecting frame (2), the bottom end of the connecting frame (2) is connected with the top end of the containing box (4), a containing cavity is arranged in the containing box (4), one ends of the two groups of first telescopic rods (6) are respectively connected with the front wall and the rear wall of the containing cavity, the other ends of the two groups of first telescopic rods (6) are respectively connected with the outer sides of the two groups of side supporting plates (5), the top ends of the two groups of fixing sleeves (3) are respectively, the four groups of fixing rods comprise folding rods (12) and extension rods (13), the four groups of extension rods (13) are respectively sleeved with the four groups of fixing sleeves (3), the outer sides of the four groups of extension rods (13) are respectively hinged with one ends of the four groups of folding rods (12), the other ends of the four groups of folding rods (12) are respectively connected with one ends of the four groups of positioning rods (21), one ends of the four groups of extension rods (13) respectively sleeved with the four groups of fixing sleeves (3) are respectively provided with a positioning cavity, the side walls of the four groups of fixing sleeves (3) are provided with a plurality of groups of positioning holes, one ends of the four groups of positioning springs (8) are respectively connected with the side walls of the four groups of positioning cavities, the other ends of the four groups of positioning springs (8) are respectively connected with one ends of the four groups of positioning columns (7), and the other ends of the four groups of positioning columns (7) respectively penetrate through the, the side walls of the four groups of telescopic sleeves (10) are respectively connected with the inner sides of the four groups of folding rods (12), and the top ends of the four groups of threaded rods (9) are respectively screwed and penetrate through the four groups of telescopic sleeves (10) to be respectively rotatably connected with the front part and the rear part of the bottom ends of the two groups of side baffles (11).
2. The hybrid transport unmanned aerial vehicle of claim 1, wherein: the top ends of the four groups of positioning rods (21) are provided with buckles (14), the left part and the right part of the connecting frame (2) are provided with two groups of clamping seats (15), and the four groups of buckles (14) are respectively matched with the four groups of clamping seats (15).
3. The hybrid transport unmanned aerial vehicle of claim 2, wherein: the telescopic rod fixing device is characterized by further comprising four groups of positioning sleeves (16), wherein the four groups of positioning sleeves (16) are respectively sleeved with the four groups of extension rods (13), and one ends of the four groups of positioning sleeves (16) are respectively screwed with the four groups of fixing sleeves (3).
4. The hybrid transport unmanned aerial vehicle of claim 3, wherein: the four groups of extension rods (13) are respectively provided with external threads at the outer side of one end connected with the four groups of folding rods (12), and the four groups of positioning sleeves (16) are respectively provided with internal threads.
5. The hybrid transport unmanned aerial vehicle of claim 4, wherein: the multifunctional food storage box is characterized by further comprising a lower top plate (17) and a second telescopic rod (18), wherein the top end of the second telescopic rod (18) is connected with the upper wall of the containing cavity, and the bottom end of the second telescopic rod (18) is connected with the top end of the lower top plate (17).
6. The hybrid transport unmanned aerial vehicle of claim 5, wherein: the device is characterized by further comprising four groups of turntables (19), wherein the top ends of the four groups of turntables (19) are respectively connected with the bottom ends of the four groups of threaded rods (9).
7. The hybrid transport unmanned aerial vehicle of claim 6, wherein: the two groups of side supporting plates (5), the two groups of side baffles (11) and the lower top plate (17) are provided with protective layers (20).
CN202021242769.1U 2020-06-30 2020-06-30 Oil-electricity hybrid's transportation unmanned aerial vehicle Active CN212473904U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021242769.1U CN212473904U (en) 2020-06-30 2020-06-30 Oil-electricity hybrid's transportation unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021242769.1U CN212473904U (en) 2020-06-30 2020-06-30 Oil-electricity hybrid's transportation unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN212473904U true CN212473904U (en) 2021-02-05

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CN202021242769.1U Active CN212473904U (en) 2020-06-30 2020-06-30 Oil-electricity hybrid's transportation unmanned aerial vehicle

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CN (1) CN212473904U (en)

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