CN216401755U - Novel unmanned aerial vehicle for cargo transportation - Google Patents

Novel unmanned aerial vehicle for cargo transportation Download PDF

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Publication number
CN216401755U
CN216401755U CN202023287621.2U CN202023287621U CN216401755U CN 216401755 U CN216401755 U CN 216401755U CN 202023287621 U CN202023287621 U CN 202023287621U CN 216401755 U CN216401755 U CN 216401755U
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China
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box body
unmanned aerial
arms
aerial vehicle
side frame
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CN202023287621.2U
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Chinese (zh)
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陈远高
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Shenzhen Gaodafei Technology Co ltd
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Shenzhen Gaodafei Technology Co ltd
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Abstract

The utility model discloses a novel cargo-transporting unmanned aerial vehicle, in particular to the technical field of unmanned aerial vehicles, which comprises a vehicle body, a plurality of arms horizontally arranged on the vehicle body and rotor wing assemblies arranged on the arms, wherein the number of the arms is at least four, and the arms are uniformly arranged around the vehicle body at intervals; install on the fuselage and be used for carrying cargo the thing mechanism of carrying, carry the thing mechanism and include: the box body and at least two connecting pieces are respectively and symmetrically vertically arranged on two sides of the machine body and used for connecting the box body; one end of each connecting piece is respectively fixed on the two machine arms and positioned between the two machine arms, and the other end of each connecting piece is connected with the box body; the connecting piece is provided with a side frame and a hanging frame, wherein the side frame is used for being connected and fixed with the machine arm, and the hanging frame is vertically fixed with the side frame and used for being connected and fixed with the box body; through the design, when the unmanned aerial vehicle carries the thing transportation in flight, can make its stable flight, it is reasonable to have simple structure, convenient to use's characteristics.

Description

Novel unmanned aerial vehicle for cargo transportation
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a novel cargo-transporting unmanned aerial vehicle.
Background
Unmanned aircraft, also called "drone" for short, is an unmanned aircraft operated by means of radio remote control devices and self-contained program control devices, or autonomously operated by an on-board computer, either completely or intermittently. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
In the process of flying and transporting goods, the conventional novel cargo-transporting unmanned aerial vehicle usually shakes goods, so that the unmanned aerial vehicle is unstable, and the unmanned aerial vehicle is easy to lose control; there is thus a need for research and improvement in the structure of this new type of cargo drone; in order to solve the above problems, the present invention is proposed.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a novel cargo unmanned aerial vehicle to solve at least one of the above defects in the prior art.
In order to achieve the purpose, the utility model provides the following technical scheme: a novel cargo unmanned aerial vehicle comprises a fuselage, a plurality of arms horizontally arranged on the fuselage and rotor wing assemblies arranged on the arms, wherein the number of the arms is at least four, and the arms are uniformly arranged around the fuselage at intervals;
install on the fuselage and be used for the year thing mechanism of delivery, it includes to carry the thing mechanism: the box body and the at least two connecting pieces are respectively and symmetrically and vertically arranged on two sides of the machine body and used for connecting the box body;
one end of each of the two connecting pieces is fixed on the two machine arms and positioned between the two machine arms, and the other end of each of the two connecting pieces is connected with the box body;
the connecting piece is provided with a side frame and a hanging frame, the side frame is used for being connected and fixed with the machine arm, and the hanging frame is vertically fixed with the side frame and used for being connected and fixed with the box body.
According to a further improvement of the utility model, the number of the hanging brackets is at least two, and the hanging brackets are arranged at regular intervals.
According to the further improvement of the utility model, two ends of the side frame are respectively fixed with the two machine arms and are positioned between the two machine arms.
According to the further improvement of the utility model, one end of the hanging bracket, which is far away from the side frame, is inserted in the box body, and the hanging bracket can move telescopically relative to the box body.
In a further development of the utility model, one side of the box has a locking element for adjustably locking the hanger.
The utility model further improves the structure that the edge of the box body is provided with a notch which is used for the insertion of the hanging bracket and is sunken inwards, the hanging bracket is provided with a plurality of positioning holes which are arranged at intervals and are used for matching with the locking piece for locking, and one side of the box body is provided with a positioning groove which corresponds to the positioning holes and is used for the penetration of the locking piece.
According to the further improvement of the utility model, the inner wall of the box body is provided with a raised guide block, a partition plate is connected between the guide blocks in a sliding manner, a guide groove is formed in the side end of the partition plate, and the guide block is connected with the guide groove in a sliding manner.
In a further improvement of the utility model, the number of the guide blocks is at least two, and the guide blocks are symmetrically arranged on two sides of the inner wall.
In a further development of the utility model, the guide block is located in the middle of the box.
Compared with the prior art, the utility model has the following beneficial effects:
the novel cargo unmanned aerial vehicle comprises a fuselage, a plurality of arms horizontally arranged on the fuselage and rotor wing assemblies arranged on the arms, wherein the number of the arms is at least four, and the arms are uniformly arranged around the fuselage at intervals; install on the fuselage and be used for the year thing mechanism of delivery, it includes to carry the thing mechanism: the box body and the at least two connecting pieces are respectively and symmetrically and vertically arranged on two sides of the machine body and used for connecting the box body; one end of each of the two connecting pieces is fixed on the two machine arms and positioned between the two machine arms, and the other end of each of the two connecting pieces is connected with the box body; the connecting piece is provided with a side frame and a hanging frame, the side frame is used for being connected and fixed with the machine arm, and the hanging frame is vertically fixed with the side frame and used for being connected and fixed with the box body; through the design, when the unmanned aerial vehicle is in flight, carries objects and transports, the unmanned aerial vehicle can fly stably and has the characteristics of simple and reasonable structure and convenient use;
in addition, through the stretching of gallows for form between fuselage and the year thing mechanism and place the district, can be used to supplying the placing of goods, thereby on the one hand, increased the transportation capacity of goods, on the other hand, can supply the freight of multiple type, for example, rectangular packing box can bulge in the outside of box when placing, has improved the flexibility.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic illustration of an explosive structure according to the present invention;
FIG. 3 is a schematic cross-sectional view of the case according to the present invention.
In the figure: 1. a body; 2. a horn; 3. a rotor assembly; 4. a carrying mechanism; 401. a box body; 402. a connecting member; 403. a side frame; 404. a hanger; 405. positioning holes; 406. a notch; 407. positioning a groove; 408. a guide block; 5. a locking member; 6. a partition plate; 601 guide grooves.
Detailed Description
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention.
Referring to fig. 1 to fig. 3, the technical solution adopted by the present embodiment is: a novel cargo unmanned aerial vehicle comprises a fuselage 1, a plurality of arms 2 horizontally mounted on the fuselage 1 and rotor assemblies 3 mounted on the arms 2, wherein the number of the arms 2 is at least four, and the arms 2 are uniformly arranged around the fuselage 1 at intervals; install the year thing mechanism 4 that is used for the delivery goods on the fuselage 1, it includes to carry thing mechanism 4: the connecting device comprises a box body 401 and at least two connecting pieces 402, wherein the connecting pieces 402 are respectively symmetrically and vertically arranged on two sides of the machine body 1 and used for connecting the box body 401; one end of each of the two connecting pieces 402 is fixed on each of the two arms 2 and located between the two arms 2, and the other end is connected to the box 401; the connecting piece 402 is provided with a side frame 403 and a hanging frame 404, the side frame 403 is used for being connected and fixed with the machine arm 2, and the hanging frame 404 is vertically fixed with the side frame 403 and is used for being connected and fixed with the box body 401; through the design, when the unmanned aerial vehicle carries the thing transportation in flight, can make its stable flight.
The number of the hanging brackets 404 is at least two, and the hanging brackets are arranged at regular intervals, so that the stability is enhanced; two ends of the side frame 403 are respectively fixed with the two machine arms 2 and are positioned between the two machine arms 2, and the side frame 403 is equidistantly arranged on two sides of the machine body 1; thereby enlarging the range of connection of the hanger 404 to facilitate the connection fixation of the hanger 404.
One end of the hanger 404, which is far away from the side frame 403, is inserted into the box 401, and the hanger 404 can move telescopically relative to the box 401; one side of the box body 401 is provided with a locking piece 5 for adjusting and locking the hanging bracket 404; the edge of the box 401 is provided with a notch 406 for the hanging bracket 404 to be inserted and recessed inwards, the hanging bracket 404 is provided with a plurality of positioning holes 405 arranged at intervals and used for matching with the locking piece 5 to be locked, and one side of the box 401 is provided with a positioning groove 407 corresponding to the positioning holes 405 and used for the locking piece 5 to penetrate through.
Specifically, at least four hanging brackets 404 are respectively fixed on the side frame 403 at intervals, during assembly, the hanging brackets 404 are respectively inserted into corresponding notches 406 on the box body 401, and when the positioning holes 405 on the hanging brackets 404 correspond to the positioning grooves 407 on the box body 401, the locking pieces 5 are inserted into the positioning grooves 407 and are connected and locked with the positioning holes 405, wherein the locking pieces 5 are in threaded connection with the positioning holes 405, however, the locking pieces 5 have external threads, and the positioning holes 405 have internal threads; the up-and-down adjustment of the machine body 1 can be realized through the up-and-down adjustment of the hanging bracket 404, so that the distance between the machine body 1 and the box body 401 is lengthened, and a placing area is formed between the machine body 1 and the box body 401 and can be used for placing goods; the transportation capacity of goods has been increased, can supply multiple type freight in addition, for example, rectangular packing box etc. when placing, protrusion in the outside of box 401 has improved the flexibility.
The inner wall of the box body 401 is provided with a raised guide block 408, a partition plate 6 is connected between the guide blocks 408 in a sliding manner, a guide groove is formed in the side end of the partition plate 6, and the guide blocks 408 are connected with the guide groove in a sliding manner; the number of the guide blocks 408 is at least two, and the guide blocks are symmetrically arranged on two sides of the inner wall; the guide block 408 is located at a middle position of the case 401.
When two kinds of goods need to be distinguished, guide block 408 and guide way can be aimed at, inside baffle 6 inserted box 401, make baffle 6 slide into box 401 along guide block 408 inside, can separate two parking spaces with the inside of box 401 through baffle 6 like this, improve the practicality, in addition, can be with even the placing in two parking spaces of goods through baffle 6, and then reach steady effect.
To sum up, this kind of novel freight unmanned aerial vehicle has simple structure rationally, and convenient to use's characteristics can satisfy user's demand, and practical value is high.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The detachable installation mode has various modes, for example, a mode of matching with a buckle through plugging, for example, a mode of connecting through a bolt, and the like.
The conception, the specific structure and the technical effects of the present invention are clearly and completely described above in connection with the embodiments and the accompanying drawings, so that the objects, the features and the effects of the present invention can be fully understood. It is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and those skilled in the art can obtain other embodiments without inventive effort based on the embodiments of the present invention, and all embodiments are within the protection scope of the present invention. In addition, all the coupling/connection relationships mentioned herein do not mean that the components are directly connected, but mean that a better coupling structure can be formed by adding or reducing coupling accessories according to specific implementation conditions.
The above embodiments are only for further illustration of the present invention, and should not be construed as limiting the scope of the present invention, and the technical engineers in the art can make insubstantial modifications and adaptations of the present invention based on the above disclosure and disclosure of the utility model.

Claims (9)

1. The novel cargo unmanned aerial vehicle is characterized by comprising a fuselage (1), a plurality of arms (2) horizontally mounted on the fuselage (1) and rotor wing assemblies (3) mounted on the arms (2), wherein the number of the arms (2) is at least four, and the arms are uniformly arranged around the fuselage (1) at intervals;
install on fuselage (1) and be used for carrying cargo year thing mechanism (4), it includes to carry thing mechanism (4): the connecting device comprises a box body (401) and at least two connecting pieces (402), wherein the connecting pieces (402) are respectively symmetrically and vertically arranged on two sides of the machine body (1) and used for connecting the box body (401);
one end of each of the two connecting pieces (402) is fixed on the two machine arms (2) and positioned between the two machine arms (2), and the other end of each of the two connecting pieces is connected with the box body (401);
the connecting piece (402) is provided with a side frame (403) and a hanging frame (404), the side frame (403) is used for being connected and fixed with the machine arm (2), and the hanging frame (404) is vertically fixed with the side frame (403) and used for being connected and fixed with the box body (401).
2. A new type of unmanned aerial vehicle for cargo transportation as defined in claim 1, wherein: the number of the hanging brackets (404) is at least two, and the hanging brackets are arranged at regular intervals.
3. A new type of unmanned aerial vehicle for cargo transportation as defined in claim 1, wherein: two ends of the side frame (403) are respectively fixed with the two machine arms (2) and are positioned between the two machine arms (2).
4. A new type of unmanned aerial vehicle for cargo transportation as defined in claim 1, wherein: one end of the hanging bracket (404) far away from the side frame (403) is inserted into the box body (401), and the hanging bracket (404) can move in a telescopic mode relative to the box body (401).
5. A new type of unmanned aerial vehicle for cargo transportation as defined in claim 4, wherein: one side of the box body (401) is provided with a locking piece (5) for adjusting and locking the hanging bracket (404).
6. A new type of unmanned aerial vehicle for cargo transportation as defined in claim 5, wherein: the edge of the box body (401) is provided with a notch (406) which is used for inserting the hanging bracket (404) and is sunken inwards, the hanging bracket (404) is provided with a plurality of positioning holes (405) which are arranged at intervals and used for being matched with the locking piece (5) for locking, and one side of the box body (401) is provided with positioning grooves (407) which correspond to the positioning holes (405) and are used for allowing the locking piece (5) to penetrate through.
7. A new type of unmanned aerial vehicle for cargo transportation as defined in claim 1, wherein: the inner wall of the box body (401) is provided with a raised guide block (408), a partition plate (6) is connected between the guide blocks (408) in a sliding mode, a guide groove is formed in the side end of the partition plate (6), and the guide block (408) is connected with the guide groove in a sliding mode.
8. A new type of unmanned aerial vehicle for cargo transportation as defined in claim 7, wherein: the number of the guide blocks (408) is at least two, and the guide blocks are symmetrically arranged on two sides of the inner wall.
9. A new type of unmanned aerial vehicle for cargo transportation according to any of claims 7-8, characterized in that: the guide block (408) is positioned in the middle of the box body (401).
CN202023287621.2U 2020-12-30 2020-12-30 Novel unmanned aerial vehicle for cargo transportation Active CN216401755U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202023287621.2U CN216401755U (en) 2020-12-30 2020-12-30 Novel unmanned aerial vehicle for cargo transportation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202023287621.2U CN216401755U (en) 2020-12-30 2020-12-30 Novel unmanned aerial vehicle for cargo transportation

Publications (1)

Publication Number Publication Date
CN216401755U true CN216401755U (en) 2022-04-29

Family

ID=81282086

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202023287621.2U Active CN216401755U (en) 2020-12-30 2020-12-30 Novel unmanned aerial vehicle for cargo transportation

Country Status (1)

Country Link
CN (1) CN216401755U (en)

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