CN216546660U - Unmanned aerial vehicle fuselage and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle fuselage and unmanned aerial vehicle Download PDFInfo
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- CN216546660U CN216546660U CN202220311725.2U CN202220311725U CN216546660U CN 216546660 U CN216546660 U CN 216546660U CN 202220311725 U CN202220311725 U CN 202220311725U CN 216546660 U CN216546660 U CN 216546660U
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Abstract
The utility model discloses an unmanned aerial vehicle body, which comprises a middle main frame, wherein a body main body is arranged on the outer side of the middle main frame, a connecting cover is arranged between the body main bodies, body bases are arranged on the lower sides of the body main body and the connecting cover, an arm seat is arranged at one end of the connecting cover, the arm seat and the connecting cover are of an integrally formed structure, an installation slot is arranged on the inner side of the arm seat, an installation screw is screwed on the lower side of the arm seat, the other end of the connecting cover is inserted into the inner side of the middle main frame, and the connecting cover is fixedly connected with the middle main frame through a screw; through well body frame, fuselage main part and the connection lid of design, set up the horn seat when using and cover in the connection, only need when carrying out the dismouting connect the lid from the fuselage main part in take out can, need not to take the casing whole apart when using, only need to take the connection lid that needs to pull down apart can.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle body and an unmanned aerial vehicle.
Background
The fuselage material of the drone is a composite material. At present, carbon fiber reinforced PC and PA materials are generally used in China, and composite materials become main structural materials in the field of unmanned aerial vehicles, such as carbon fiber composite materials, glass fiber composite materials, honeycomb sandwich composite materials and the like. Generally, in an unmanned aerial vehicle, structural members such as keels, beams, bulkheads and landing gears of a fuselage are made of aluminum alloy, and structural members such as wings, empennages and various antenna housings, guard plates and skins are made of composite materials in a large quantity. In addition, on small and medium-sized unmanned aerial vehicles, nonmetal materials such as wood materials, light plastics and plastic films are also used in a large quantity. The application of the composite material plays a crucial role in lightening, miniaturizing and improving the performance of the unmanned aircraft structure. Many materials vendors are also developing materials more suitable for drones, such as polyseleon, which have developed plastic materials specific for drones.
The existing unmanned aerial vehicle fuselage is generally installed and fixed by adopting an upper shell and a lower shell when in use, is square or circular and the like when in use, and solves the problems of instability and convenience when the unmanned aerial vehicle arm and the like are disassembled and assembled when in use, so that the unmanned aerial vehicle fuselage and the unmanned aerial vehicle are provided.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an unmanned aerial vehicle body and an unmanned aerial vehicle, and aims to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme:
unmanned aerial vehicle fuselage, including well body frame, the outside of well body frame is provided with the fuselage main part, be provided with the connection lid between the fuselage main part, the downside of fuselage main part and connection lid is provided with the fuselage base, the one end of connecting the lid sets up the horn seat, and the horn seat is the integrated into one piece structure with the connection lid, the inboard of horn seat is provided with the installation slot, the downside of horn seat has closed the installation screw soon, the other end of connecting the lid inserts the inboard of well body frame, and passes through screw fixed connection between connection lid and the well body frame.
Preferably, the main body of the main body and the connecting cover are regular octagon in overall shape, and the connecting cover and the main body of the main body are arranged on the middle main frame in a staggered mode.
Preferably, the fuselage base middle part is provided with the lamp stand, the outside of lamp stand is central symmetry and is provided with the unmanned aerial vehicle lamp.
Preferably, the center of the lamp holder is provided with a positioning hole, and the positioning hole is clamped at one end of the middle main frame.
Preferably, the inboard of fuselage base is provided with the location fixture block, the location fixture block is in the junction of fuselage main part and connection lid, the inboard of fuselage base is provided with fixed screw seat, the fuselage base passes through fixed screw seat and screw and fuselage main part and connection lid fixed connection.
Unmanned aerial vehicle, including unmanned aerial vehicle fuselage, unmanned aerial vehicle horn and unmanned aerial vehicle screw, the inboard of horn seat is inserted to the one end of unmanned aerial vehicle horn, and unmanned aerial vehicle horn and horn seat pass through installation screw fixed connection, the one end at the unmanned aerial vehicle horn is installed to the unmanned aerial vehicle screw.
Compared with the prior art, the utility model has the beneficial effects that:
1. through well body frame, fuselage main part and the connection lid of design, set up the horn seat when using and cover in the connection, only need when carrying out the dismouting connect the lid from the fuselage main part in take out can, need not to take the casing whole apart when using, only need to take the connection lid that needs to pull down apart can.
2. Through the fuselage base, location fixture block and the locating hole of design, it is more stable when installing the fuselage base, and the location of cooperation location fixture block and locating hole, make the connection lid install more stably in the fuselage main part.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the connecting cover mounting structure of the present invention;
FIG. 3 is a schematic view of the structure of the fuselage base of the present invention;
fig. 4 is a schematic structural diagram of the drone of the present invention;
in the figure: 1. a middle main frame; 2. a main body of the body; 3. a connecting cover; 4. a boom base; 5. a body base; 6. fixing screws; 7. installing a slot; 8. mounting screws; 9. positioning a fixture block; 10. fixing the screw seat; 11. a lamp socket; 12. an unmanned aerial vehicle light; 13. positioning holes; 14. an unmanned aerial vehicle arm; 15. unmanned aerial vehicle screw.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The first embodiment is as follows:
referring to fig. 1 to 4, the present invention provides a technical solution: an unmanned aerial vehicle body comprises a middle main frame 1, a body main body 2 is arranged on the outer side of the middle main frame 1, a connecting cover 3 is arranged between the body main bodies 2, a body base 5 is arranged on the lower sides of the body main body 2 and the connecting cover 3, a fixing screw base 10 is arranged on the inner side of the body base 5, the body base 5 is fixedly connected with the body main body 2 and the connecting cover 3 through the fixing screw base 10 and screws, the body base 5 is fixedly connected with the body main body 2 and the connecting cover 3 through the fixing screw base 10, a lamp holder 11 is arranged in the middle of the body base 5, unmanned aerial vehicle lamps 12 are arranged on the outer side of the lamp holder 11 in a central symmetry manner, the unmanned aerial vehicle can be conveniently irradiated and used through the lamp holder 11 and the unmanned aerial vehicle lamps 12, an arm base 4 is arranged at one end of the connecting cover 3, the arm base 4 and the connecting cover 3 are of an integrated structure, an installation slot 7 is arranged on the inner side of the arm base 4, and an installation screw 8 is screwed on the lower side of the arm base 4, the other end of the connecting cover 3 is inserted into the inner side of the middle main frame 1, the connecting cover 3 is fixedly connected with the middle main frame 1 through screws, the connecting cover 3 can be directly pulled out of the machine body main body 2 and the middle main frame 1 only by screwing down the fixing screws 6 and the mounting screws 8 and then screwing down the screws in the fixing screw seats 10, then elements on the inner side of the connecting cover 3 can be overhauled, and the unmanned aerial vehicle arm 14 is pulled out of the arm seats 4 for overhauling and replacing; fuselage main part 2 and the overall shape of connecting lid 3 are regular octagon, connect lid 3 and fuselage main part 2 crisscross setting to install in the well body frame 1, make the unmanned aerial vehicle fuselage more stable when using.
As apparent from the above description, the present invention has the following advantageous effects: when in use, the horn base 4 is arranged on the connecting cover 3, only the connecting cover 3 needs to be drawn out from the body main body 2 when in disassembly and assembly, and the connecting cover 3 which needs to be disassembled can be disassembled without disassembling the shell completely when in use.
Unmanned aerial vehicle, including above-mentioned unmanned aerial vehicle fuselage, unmanned aerial vehicle horn 14 and unmanned aerial vehicle screw 15, the inboard of horn seat 4 is inserted to the one end of unmanned aerial vehicle horn 14, and unmanned aerial vehicle horn 14 passes through installation screw 8 fixed connection with horn seat 4, and unmanned aerial vehicle screw 15 is installed in the one end of unmanned aerial vehicle horn 14, through the operation of unmanned aerial vehicle screw 15 on the unmanned aerial vehicle horn 14 to drive unmanned aerial vehicle and lift off the flight.
Example two:
referring to fig. 1 to fig. 3, on the basis of the first embodiment, the present invention provides a technical solution: a positioning hole 13 is formed in the center of the lamp holder 11, the positioning hole 13 is clamped at one end of the middle main frame 1, and the lamp holder 11 and the machine body base 5 are more stably installed through the positioning of the positioning hole 13; the inboard of fuselage base 5 is provided with location fixture block 9, and location fixture block 9 block is more stable when making fuselage main part 2 and connecting between the lid 3 through the location of location fixture block 9 in the junction of fuselage main part 2 and connecting lid 3 to make the fuselage more stable.
By adopting the machine body base 5, the positioning fixture block 9 and the positioning hole 13, the installation of the machine body base 5 is more stable, and the positioning fixture block 9 and the positioning hole 13 are matched for positioning, so that the connecting cover 3 is more stable to be installed on the machine body main body 2.
The working principle and the using process of the utility model are as follows: provide lift through unmanned aerial vehicle screw 15 when using and drive the unmanned aerial vehicle fuselage and fly, use unmanned aerial vehicle screw 15 for a long time, connect and cover 3 internal component trouble, only need through screwing down set screw 6 and installation screw 8, can take out connecting cover 3 directly from fuselage main part 2 and well body frame 1 to the screw in the set screw seat 10 is screwed down again, then can overhaul connecting cover 3 internal side component, and take out unmanned aerial vehicle horn 14 from the fuselage 4 in and overhaul the change, the dismouting is more convenient when using, and cooperation location fixture block 9 and locating hole 13 are to fuselage main part 2 and connecting cover 3 location, it is more stable to make fuselage base 5 install in fuselage main part 2 and connecting cover 3, make locating hole 13 block guarantee fuselage base 5 installation stability on well body frame 1, guarantee unmanned aerial vehicle fuselage steady operation when using.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
The above description is only for the purpose of illustrating the technical solutions of the present invention and not for the purpose of limiting the same, and other modifications or equivalent substitutions made by those skilled in the art to the technical solutions of the present invention should be covered within the scope of the claims of the present invention without departing from the spirit and scope of the technical solutions of the present invention.
Claims (6)
1. Unmanned aerial vehicle fuselage, its characterized in that: including well body frame (1), the outside of well body frame (1) is provided with fuselage main part (2), be provided with between fuselage main part (2) and connect lid (3), the downside of fuselage main part (2) and connection lid (3) is provided with fuselage base (5), the one end of connecting lid (3) sets up has horn seat (4), and horn seat (4) and connection lid (3) be the integrated into one piece structure, the inboard of horn seat (4) is provided with installation slot (7), the downside of horn seat (4) has closed mounting screw (8) soon, the other end of connecting lid (3) inserts the inboard of well body frame (1), and passes through screw fixed connection between connection lid (3) and well body frame (1).
2. The unmanned aerial vehicle fuselage of claim 1, characterized in that: the main body (2) and the connection cover (3) are regular octagon in overall shape, and the connection cover (3) and the main body (2) are arranged on the middle main frame (1) in a staggered mode.
3. The unmanned aerial vehicle fuselage of claim 1, characterized in that: fuselage base (5) middle part is provided with lamp stand (11), the outside of lamp stand (11) is central symmetry and is provided with unmanned aerial vehicle lamp (12).
4. The unmanned aerial vehicle fuselage of claim 3, characterized in that: a positioning hole (13) is formed in the center of the lamp holder (11), and the positioning hole (13) is clamped at one end of the middle main frame (1).
5. The unmanned aerial vehicle fuselage of claim 1, characterized in that: the inboard of fuselage base (5) is provided with positioning fixture block (9), positioning fixture block (9) block is in the junction of fuselage main part (2) and connection lid (3), the inboard of fuselage base (5) is provided with fixed screw seat (10), fuselage base (5) are through fixed screw seat (10) and screw and fuselage main part (2) and connection lid (3) fixed connection.
6. Unmanned aerial vehicle, its characterized in that: including the unmanned aerial vehicle fuselage of any one of claims 1 to 5, unmanned aerial vehicle horn (14) and unmanned aerial vehicle screw (15), the inboard of horn seat (4) is inserted to the one end of unmanned aerial vehicle horn (14), and unmanned aerial vehicle horn (14) and horn seat (4) through installation screw (8) fixed connection, the one end at unmanned aerial vehicle horn (14) is installed in unmanned aerial vehicle propeller (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220311725.2U CN216546660U (en) | 2022-02-16 | 2022-02-16 | Unmanned aerial vehicle fuselage and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220311725.2U CN216546660U (en) | 2022-02-16 | 2022-02-16 | Unmanned aerial vehicle fuselage and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216546660U true CN216546660U (en) | 2022-05-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220311725.2U Active CN216546660U (en) | 2022-02-16 | 2022-02-16 | Unmanned aerial vehicle fuselage and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216546660U (en) |
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2022
- 2022-02-16 CN CN202220311725.2U patent/CN216546660U/en active Active
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