CN212605810U - Unmanned aerial vehicle paddle structure - Google Patents
Unmanned aerial vehicle paddle structure Download PDFInfo
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- CN212605810U CN212605810U CN202021482426.2U CN202021482426U CN212605810U CN 212605810 U CN212605810 U CN 212605810U CN 202021482426 U CN202021482426 U CN 202021482426U CN 212605810 U CN212605810 U CN 212605810U
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- unmanned aerial
- aerial vehicle
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- blade
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle paddle structure, which comprises a mounting structure for mounting on a motor base of an unmanned aerial vehicle, wherein the bottom of the mounting structure is provided with a clamping structure, the motor base is provided with a limiting structure for matching and clamping the clamping structure, and the limiting structure is rotatably connected with the motor base; through the design, the blade structure and the motor base can be simply and quickly disassembled and assembled, and the motor base has the characteristics of simple and reasonable structure and convenience in use; in addition, the clamping block is matched with the guide structure, so that the condition of wrong installation of the forward propeller and the reverse propeller can be avoided; moreover, through the design of light-emitting component, increased unmanned aerial vehicle night flight enjoyment, can satisfy user's demand, practical value is high.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned aerial vehicle paddle structure.
Background
A drone is an unmanned aircraft that is operated with a radio remote control device and self-contained program control, or is operated autonomously, either completely or intermittently, by an onboard computer.
At present, with the acceleration of the civilization process of unmanned aerial vehicle technology, multi-rotor aircraft (unmanned aerial vehicle) begins to be widely applied in various industries. In practical use, the aircraft needs to frequently carry out transition transportation between the storage place and the use place, or between two use places, and in order to guarantee transportation safety, the transportation mode that usually adopts is: at the beginning of transportation, detaching and separating the blades of the aircraft from the driving motor; then transporting the disassembled and separated blade and the driving motor; at the end of the transport, the blade is then assembled with the drive motor.
Therefore, how to simply, quickly and efficiently disassemble and assemble the paddle and the driving motor has important significance; therefore, research and improvement on the structure of the unmanned aerial vehicle luminous paddle are needed; in order to solve the above problems, the present invention is proposed.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle paddle structure to solve at least one of the above-mentioned defect that prior art exists.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle paddle structure, is including being used for installing the mounting structure on unmanned aerial vehicle's motor cabinet, mounting structure's bottom is equipped with the screens structure, be equipped with the confession on the motor cabinet the limit structure of screens structure cooperation joint, wherein, this limit structure with the motor cabinet rotates to be connected.
The utility model discloses a further improvement, the screens structural latch segment that has, limit structure is last to have the confession the opening that the latch segment penetrated, opening one side has and is used for the confession the stop part of latch segment cooperation locking, the latch segment with the stop part is supported each other and is pressed.
The utility model discloses a further improvement, limit structure is last to have bellied guide structure, the screens is structural to have to block and establishes guide structure is last and rather than the gliding screens piece of cooperation.
The utility model discloses a further improvement, the screens piece card is established guide structure's inboard or outside.
The utility model discloses a further improvement, this mounting structure still contain the casing, the light emitting component has been arranged on the casing.
The utility model discloses a further improvement, be equipped with two at least leaf bodies on the mounting structure, the casing with the confession has between the screens structure the mount pad of leaf body installation, the one end of the leaf body is equipped with the fixed part, the fixed part pass through the mounting with mount pad fixed connection.
The utility model discloses a further improvement, light emitting component includes that the holding is in circuit board in the casing and fixing the lamp area on blade surface.
The utility model discloses a further improvement, the one end in lamp area penetrates in the casing with the circuit board electricity is connected, open the casing bottom has the confession the perforation that the lamp area penetrated, just it has the confession to open on the blade body the recess of lamp area holding.
The utility model discloses a further improvement, the epaxial cover of power of motor cabinet is equipped with the elastic component, open the mount pad bottom has and is used for the cover to establish the epaxial mounting hole of power.
The utility model discloses a further improvement, the casing pass through the connecting block with screens structure fixed connection, the through-hole has on the connecting block, just the through-hole with the casing with the mounting hole intercommunication of mount pad.
Compared with the prior art, the utility model discloses following beneficial effect has:
the unmanned aerial vehicle paddle structure comprises an installation structure used for being installed on a motor base of an unmanned aerial vehicle, wherein a clamping structure is arranged at the bottom of the installation structure, and a limiting structure for matching and clamping the clamping structure is arranged on the motor base; through the design, the blade structure and the motor base can be simply and quickly disassembled and assembled, and the motor base has the characteristics of simple and reasonable structure and convenience in use;
in addition, the clamping block is matched with the guide structure, so that the condition of wrong installation of the forward propeller and the reverse propeller can be avoided; moreover, through the design of light-emitting component, increased unmanned aerial vehicle night flight enjoyment, can satisfy user's demand, practical value is high.
The invention is further described with reference to the drawings and the specific embodiments.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic diagram of the explosion structure of the present invention;
FIG. 3 is a schematic view of a partial structure of the present invention;
fig. 4 is a schematic perspective view of the motor base of the present invention;
fig. 5 is an enlarged schematic view of a portion a of fig. 3 according to the present invention.
Reference numerals:
1. a mounting structure; 101. a clamping structure; 102. a locking block; 103. mounting holes; 104. a bit block; 105. a housing; 106. a mounting seat; 107. perforating; 108. connecting blocks; 109. a through hole; 1010. a bayonet; 2. a limiting structure; 201. an opening; 202. a blocking portion; 203. a guide structure; 3. a motor base; 302. a power shaft; 303. an elastic member; 4. a leaf body; 401. a fixed part; 402. a groove; 5. a light emitting assembly; 501. a circuit board; 502. a light strip; 6. and a fixing member.
Detailed Description
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, 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.
Referring to fig. 1 to 5, the technical solution adopted by the present embodiment is as follows: an unmanned aerial vehicle paddle structure comprises a mounting structure 1 used for being mounted on a motor base 3 of an unmanned aerial vehicle, wherein a clamping structure 101 is arranged at the bottom of the mounting structure 1, and a limiting structure 2 for matching and clamping the clamping structure 101 is arranged on the motor base 3, wherein the limiting structure 2 is rotatably connected with the motor base 3, and the limiting structure 2 is in a ring shape;
the locking block 102 is arranged on the position-clamping structure 101, the locking block 102 is provided with two bent parts, the position-limiting structure 2 is provided with two openings 201 for the locking block 102 to penetrate, one side of each opening 201 is provided with a blocking part 202 for the locking block 102 to be matched and locked, and after the position-clamping structure 101 and the position-limiting structure 2 are matched and assembled, the locking block 102 and the blocking part 202 are tightly pressed against each other under the action of the elastic part 303;
the limiting structure 2 is provided with a convex guide structure 203, the blocking structure 101 is provided with a blocking block 104 which can be blocked on the guide structure 203 and can slide in a matching way with the guide structure 203, specifically, the guide structure 203 is in an arc-shaped strip shape and is arranged on the surface of the limiting structure 2, the blocking block 104 is in an L shape and is positioned on one side of the locking block 102 of the blocking structure 101, and the bayonet 1010 of the blocking block 104 corresponds to the upper surface of the guide structure 203; after assembly, the blocking block 104 is in close contact with the upper surface of the guide structure 203, thereby facilitating the installation of a user;
in addition, the situation of wrong installation of the forward and reverse paddles can be avoided by matching the clamping block 104 with the guide structure 203, the clamping block 104 is clamped at the inner side or the outer side of the guide structure 203, when the clamping opening 1010 of the clamping block 104 is designed at the inner side and assembled with the guide structure 203, the clamping opening 1010 is clamped at the inner side of the guide structure 203, and when the clamping opening 1010 of the clamping block 104 is designed at the outer side and assembled with the guide structure 203, the clamping opening 1010 is clamped at the outer side of the guide structure 203; however, the forward-rotating paddle structure can be designed as the bayonet 1010 at the inner side, and the reverse-rotating paddle structure can be designed as the bayonet 1010 at the outer side, because the bayonet 1010 and the guide structure 203 are symmetrically designed, when the forward-rotating paddle structure is assembled on the limit structure 2 of the reverse-rotating paddle structure, the opening 201 cannot be clamped on the corresponding guide structure 203, and thus the situation that the forward-rotating paddle structure and the reverse-rotating paddle structure are installed wrongly is effectively avoided;
the mounting structure 1 further comprises a housing 105, a light-emitting component 5 is arranged on the housing 105, at least two blade bodies 4 are assembled on the mounting structure 1, a mounting seat 106 for mounting the blade bodies 4 is arranged between the housing 105 and the clamping structure 101, the mounting seat 106 and the locking block 102 are integrated, a fixing part 401 is arranged at one end of each blade body 4, and the fixing part 401 is fixedly connected with the mounting seat 106 through a fixing part 6, so that the mounting is quick and convenient;
the fixing piece 6 is cylindrical, the fixing part 401 of the blade body 4 is a hollow fixing part, the fixing part 401 is sleeved on the fixing piece 6 for limiting and fixing, and meanwhile, the fixing part 401 can be rotated, so that the blade body can be rotated and bent, however, the occupied area is reduced, and the blade body is convenient to store and carry;
the light emitting component 5 comprises a circuit board 501 accommodated in the housing 105 and a lamp strip 502 fixed on the surface of the blade 4, wherein the lamp strip 502 is a flexible lamp strip; one end of the light strip 502 penetrates into the shell 105 to be electrically connected with the circuit board 501, a through hole 107 for the light strip 502 to penetrate through is formed in the bottom of the shell 105, a groove 402 for accommodating the light strip 502 is formed in the blade body 4, the groove 402 is located at the bottom of the blade body 4, and the bottom is a windward side; therefore, the luminous effect is achieved, the visual effect of the unmanned aerial vehicle is better and more cool when the unmanned aerial vehicle flies in the air, and the position of the unmanned aerial vehicle is easier to determine when the unmanned aerial vehicle flies at night;
an elastic piece 303 is sleeved on a power shaft 302 of the motor base 3, and a mounting hole 103 for sleeving the power shaft 302 is formed in the bottom of the mounting base 106; the shell 105 is fixedly connected with the clamping structure 101 through a connecting block 108, a through hole 109 is formed in the connecting block 108, and the through hole 109 is communicated with the shell 105 and the mounting hole 103 of the mounting seat 106;
in addition, a power pack electrically connected with the circuit board 501 is arranged in the shell, and the power pack is a charging button, so that the power pack has the advantages of small volume and light weight;
in this embodiment, first, the circuit board 501 of the light emitting component 5 is fixed in the housing 105, then one end of the light strip 502 penetrates through the through hole 107 to be connected with the circuit board 501, then the two blade bodies 4 are assembled on the mounting seat 106 and fixed by the fixing member 6, the light strip 502 is fixed on the blade bodies 4, and then the clamping structure 101 of the mounting structure 1 is clamped and fixed with the limiting structure 2 of the motor seat 3; during assembly, the locking block 102 of the clamping structure 101 is aligned to the bayonet 1010 of the limiting structure 2 and is pressed to be clamped in, meanwhile, the power shaft 302 of the motor base 3 penetrates through the mounting hole 103 of the mounting base 106, the elastic piece 303 is blocked and pressed on the outer side of the mounting base 106, then the locking block 102 is pressed on the bottom of the blocking portion 202 by rotating the clamping structure 101, and under the action of the elastic piece 303, the locking block 102 is tightly pressed on the blocking portion 202, so that the installation is quick and convenient.
In conclusion, the blade structure of the unmanned aerial vehicle and the motor base 3 can be simply and quickly disassembled and assembled, and the blade structure has the characteristics of simple and reasonable structure and convenience in use; in addition, the clamping block 104 is matched with the guide structure 203, so that the condition of wrong installation of the forward propeller and the reverse propeller can be avoided; moreover, through the design of light emitting component 5, unmanned aerial vehicle night flight enjoyment has been increased, user's demand can be satisfied, and practical value is high.
The conception, the specific structure, and the technical effects produced by the present invention will be clearly and completely described above with reference to the embodiments and the accompanying drawings, so as to fully understand the objects, the features, and the effects of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and other embodiments obtained by those skilled in the art without inventive labor based on the embodiments of the present invention all belong to 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 used for further explanation of the present invention, and it is not understood that the present invention is limited by the protection scope of the present invention, and the technical engineers in the field are right according to the above contents of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle paddle structure, is including being used for installing mounting structure (1) on unmanned aerial vehicle's motor cabinet (3), its characterized in that: the bottom of mounting structure (1) is equipped with clamping structure (101), be equipped with the confession on motor cabinet (3) clamping structure (101) cooperation joint limit structure (2), wherein, this limit structure (2) with motor cabinet (3) rotate to be connected.
2. The unmanned aerial vehicle blade structure of claim 1, wherein: the clamping structure (101) is provided with a locking block (102), the limiting structure (2) is provided with an opening (201) for the locking block (102) to penetrate, one side of the opening (201) is provided with a blocking portion (202) for the locking block (102) to be matched and locked, and the locking block (102) and the blocking portion (202) are mutually abutted and pressed.
3. The unmanned aerial vehicle blade structure of claim 1, wherein: the limiting structure (2) is provided with a convex guide structure (203), and the clamping structure (101) is provided with a clamping block (104) which can be clamped on the guide structure (203) and can slide in a matching manner.
4. The unmanned aerial vehicle blade structure of claim 3, wherein: the clamping block (104) is clamped on the inner side or the outer side of the guide structure (203).
5. The unmanned aerial vehicle blade structure of claim 1, wherein: the mounting structure (1) further comprises a housing (105), on which housing (105) the light emitting assembly (5) is arranged.
6. The unmanned aerial vehicle blade structure of claim 5, wherein: at least two blade bodies (4) are assembled on the mounting structure (1), the shell (105) and an installation seat (106) for installing the blade bodies (4) are arranged between the clamping structures (101), a fixing part (401) is arranged at one end of each blade body (4), and the fixing part (401) is fixedly connected with the installation seat (106) through a fixing part (6).
7. The unmanned aerial vehicle blade structure of claim 6, wherein: the light-emitting component (5) comprises a circuit board (501) accommodated in the shell (105) and a lamp strip (502) fixed on the surface of the blade body (4).
8. The unmanned aerial vehicle blade structure of claim 7, wherein: one end of the lamp strip (502) penetrates into the shell (105) to be electrically connected with the circuit board (501), a through hole (107) for the lamp strip (502) to penetrate is formed in the bottom of the shell (105), and a groove (402) for accommodating the lamp strip (502) is formed in the blade body (4).
9. The unmanned aerial vehicle blade structure of claim 6, wherein: an elastic piece (303) is sleeved on a power shaft (302) of the motor base (3), and a mounting hole (103) used for being sleeved on the power shaft (302) is formed in the bottom of the mounting base (106).
10. The unmanned aerial vehicle blade structure of claim 9, wherein: the shell (105) is fixedly connected with the clamping structure (101) through a connecting block (108), a through hole (109) is formed in the connecting block (108), and the through hole (109) is communicated with the shell (105) and a mounting hole (103) of the mounting seat (106).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021482426.2U CN212605810U (en) | 2020-07-24 | 2020-07-24 | Unmanned aerial vehicle paddle structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021482426.2U CN212605810U (en) | 2020-07-24 | 2020-07-24 | Unmanned aerial vehicle paddle structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212605810U true CN212605810U (en) | 2021-02-26 |
Family
ID=74720319
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021482426.2U Active CN212605810U (en) | 2020-07-24 | 2020-07-24 | Unmanned aerial vehicle paddle structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212605810U (en) |
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2020
- 2020-07-24 CN CN202021482426.2U patent/CN212605810U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210611 Address after: 518000 Room 401, building 4 (b), zhonghaixin innovation industry city, Kangle community, Nanwan street, Longgang District, Shenzhen City, Guangdong Province Patentee after: Shenzhen siyufei Technology Co.,Ltd. Address before: No. 405, building 4, zhonghisense Industrial Park, No. 2, Shengbao Road, Nanwan street, Longgang District, Shenzhen City, Guangdong Province Patentee before: SHENZHEN SUYITONG TECHNOLOGY Co.,Ltd. |