CN211167376U - Many rotor unmanned aerial vehicle convenient to fold and accomodate - Google Patents
Many rotor unmanned aerial vehicle convenient to fold and accomodate Download PDFInfo
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- CN211167376U CN211167376U CN201921862088.2U CN201921862088U CN211167376U CN 211167376 U CN211167376 U CN 211167376U CN 201921862088 U CN201921862088 U CN 201921862088U CN 211167376 U CN211167376 U CN 211167376U
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- aerial vehicle
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Abstract
The utility model discloses a many rotor unmanned aerial vehicle convenient to folding storage, including unmanned aerial vehicle main part and bracing piece, the outside inner of unmanned aerial vehicle main part has been seted up and has been put the thing groove, and has put the inside left end in thing groove and be fixed with the stand, and the outer end of stand is through changeing groove and guide pillar interconnect simultaneously, the outer end of guide pillar passes through fixed slot and fixed column and unmanned aerial vehicle bulk interconnect, and the outer end of fixed column passes through control flume and unmanned aerial vehicle bulk interconnect, the inside of guide pillar is through flexible groove and movable block interconnect, the inner of movable block passes through slider and spout and guide pillar interconnect, and the outer end of movable block passes through fixture block and draw-in groove and guide pillar interconnect, the inner of fixture block passes through movable groove and extension spring and movable block interconnect, the outer end at the movable block is fixed to. This many rotor unmanned aerial vehicle convenient to fold and accomodate not only is convenient for fold to the guide pillar and accomodates, and convenient to use person carries the device simultaneously.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a many rotor unmanned aerial vehicle convenient to fold and accomodate.
Background
Unmanned aircraft, commonly known as: unmanned planes, unmanned aerial vehicles, unmanned combat airplanes, and bee-type machines; for the various remote control aircraft that do not need the driver to board to drive in the broad sense, refer in particular to the unmanned reconnaissance aircraft of military generally, along with the increase of fuselage weight, distance and lifting power between the rotor probably increase, also increased the size of rotor simultaneously, are not convenient for accomodate unmanned aerial vehicle.
But most unmanned aerial vehicle rotor is fixed knot structure at present, is not convenient for fold and accomodate, influences user's carrying and transportation. To above-mentioned problem, carry out the innovative design on original folding many rotor unmanned aerial vehicle's of accomodating of being convenient for basis.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides a many rotor unmanned aerial vehicle convenient to fold and accomodate has solved present most unmanned aerial vehicle rotor and has been fixed knot structure, is not convenient for fold and accomodate, influences user's the problem of carrying and transporting.
(II) technical scheme
In order to achieve the above object, the utility model provides a following technical scheme: a multi-rotor unmanned aerial vehicle convenient to fold and store comprises an unmanned aerial vehicle main body and a supporting rod, wherein an object placing groove is formed in the inner end of the outer portion of the unmanned aerial vehicle main body, a stand column is fixed to the left end of the inner portion of the object placing groove, the outer end of the stand column is connected with a guide pillar through a rotating groove, the outer end of the guide pillar is connected with the unmanned aerial vehicle main body through a fixing groove and a fixing column, the outer end of the fixing column is connected with the unmanned aerial vehicle main body through a control groove, the inner portion of the guide pillar is connected with a movable block through a telescopic groove, a supporting spring is arranged inside the telescopic groove, the inner end of the movable block is connected with the guide pillar through a sliding block and a sliding groove, the outer end of the movable block is connected with the guide pillar through a clamping block and a clamping groove, a through hole is formed in the inner portion of the clamping, the bracing piece is fixed in the outer end of movable block, and the outer end of bracing piece passes through motor and interior oar interconnect, and the outer end of interior oar passes through hinge and outer oar interconnect simultaneously.
Preferably, the guide post and the upright post form a turnover mechanism through the rotary groove, and the turnover angle of the turnover mechanism is 0-90 degrees.
Preferably, the outer surface of the fixing column and the inner surface of the control groove are both in a thread structure, and the fixing column and the control groove are in threaded connection.
Preferably, the movable block and the guide post form a telescopic mechanism through a support spring, a telescopic groove and the guide post, and the initial length of the support spring is equal to the depth of the telescopic groove.
Preferably, the movable block and the telescopic slot form a sliding mechanism through a sliding block and a sliding slot, and the sliding direction of the sliding mechanism is the same as the direction of the telescopic slot.
Preferably, the movable block is connected with the guide post in a clamping mode through a clamping block and a clamping groove, and the inner end of the clamping block and the movable block form a telescopic mechanism through an extension spring and a movable groove.
Preferably, the inner paddle and the outer paddle form a turnover mechanism through a hinge, and the turnover angle of the turnover mechanism is 0-180 degrees.
(III) advantageous effects
The utility model provides a many rotor unmanned aerial vehicle convenient to fold and accomodate. The method has the following beneficial effects:
(1) this many rotor unmanned aerial vehicle convenient to folding accomodate, guide pillar 5 and stand 3's tilting mechanism person of facilitating the use receive guide pillar 5 in the inside of putting thing groove 2, the holistic storage of the device of being convenient for and transportation, fixed column 7 and control tank 8's threaded connection have increased the compactness that the two is connected, be convenient for simultaneously fix the rotation angle of guide pillar 5, movable block 10 is convenient for pack up movable block 10 and bracing piece 21 with the telescopic machanism of guide pillar 5, the device of further being convenient for accomodate.
(2) This many rotor unmanned aerial vehicle convenient to folding accomodate, the sliding mechanism of movable block 10 and flexible groove 9 can avoid the movable block 10 in the inside rotation of flexible groove 9, increase the stability of bracing piece 21, the movable block 10 is connected with the block of guide pillar 5 and has increased the steadiness when the device is opened and is packed up, improve the security of device, the tilting mechanism person of facilitating the use of inner oar 23 and outer oar 25 carries out enstrophe to outer oar 25, improve the portability of device.
Drawings
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is an enlarged schematic view of the structure at A of FIG. 1 according to the present invention;
fig. 3 is an enlarged schematic structural diagram of the point B in fig. 1 according to the present invention.
In the figure: 1. an unmanned aerial vehicle main body; 2. a storage groove; 3. a column; 4. rotating the groove; 5. a guide post; 6. fixing grooves; 7. fixing a column; 8. a control slot; 9. a telescopic groove; 10. a movable block; 11. a support spring; 12. a slider; 13. a chute; 14. a clamping block; 15. a card slot; 16. a through hole; 17. a movable groove; 18. an extension spring; 19. a movable hole; 20. a column shaft; 21. a support bar; 22. a motor; 23. an inner paddle; 24. a hinge; 25. an outer paddle.
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.
As shown in fig. 1-3, the utility model provides a technical solution: a multi-rotor unmanned aerial vehicle convenient to fold and store comprises an unmanned aerial vehicle main body 1, a storage groove 2, an upright post 3, a rotary groove 4, a guide post 5, a fixing groove 6, a fixing column 7, a control groove 8, a telescopic groove 9, a movable block 10, a supporting spring 11, a sliding block 12, a sliding groove 13, a clamping block 14, a clamping groove 15, a through hole 16, a movable groove 17, a tension spring 18, a movable hole 19, an axle post 20, a supporting rod 21, a motor 22, an inner paddle 23, a hinge 24 and an outer paddle 25, wherein the storage groove 2 is formed in the inner end of the outer portion of the unmanned aerial vehicle main body 1, the upright post 3 is fixed at the left end of the inner portion of the storage groove 2, the outer end of the upright post 3 is connected with the guide post 5 through the rotary groove 4, the outer end of the guide post 5 is connected with the unmanned aerial vehicle main body 1 through the fixing groove 6 and the fixing column 7, the outer end, a supporting spring 11 is arranged in the telescopic groove 9, the inner end of the movable block 10 is connected with the guide post 5 through a sliding block 12 and a sliding groove 13, the outer end of the movable block 10 is connected with the guide post 5 through a clamping block 14 and a clamping groove 15, a through hole 16 is formed in the clamping groove 15, the inner end of the clamping block 14 is connected with the movable block 10 through a movable groove 17 and a stretching spring 18, the inner end of the movable block 10 is connected with the shaft post 20 through a movable hole 19, a supporting rod 21 is fixed at the outer end of the movable block 10, the outer end of the supporting rod 21 is connected with an inner paddle 23 through a motor 22, and the outer end of the inner paddle 23 is connected with an outer paddle 25 through a hinge 24;
the guide post 5 and the upright post 3 form a turnover mechanism through the rotary groove 4, the turnover angle of the turnover mechanism is 0-90 degrees, the turnover mechanism of the guide post 5 and the upright post 3 is convenient for a user to store the guide post 5 in the storage groove 2, and the integral storage and transportation of the device are convenient;
the outer surface of the fixed column 7 and the inner surface of the control groove 8 are both in threaded structures and are in threaded connection, and the threaded connection of the fixed column 7 and the control groove 8 increases the connection tightness of the fixed column 7 and the control groove, and is convenient for fixing the turning angle of the guide column 5;
the movable block 10 and the guide post 5 form a telescopic mechanism through the support spring 11 and the telescopic groove 9, the initial length of the support spring 11 is equal to the depth of the telescopic groove 9, and the telescopic mechanism of the movable block 10 and the guide post 5 is convenient for retracting the movable block 10 and the support rod 21, so that the device is further convenient to store;
the movable block 10 and the telescopic groove 9 form a sliding mechanism through the sliding block 12 and the sliding groove 13, the sliding direction of the sliding mechanism is the same as that of the telescopic groove 9, the sliding mechanism of the movable block 10 and the telescopic groove 9 can prevent the movable block 10 from rotating in the telescopic groove 9, and the stability of the support rod 21 is improved;
the movable block 10 is connected with the guide post 5 in a clamping mode through a clamping block 14 and a clamping groove 15, the inner end of the clamping block 14 and the movable block 10 form a telescopic mechanism through an extension spring 18 and a movable groove 17, and the clamping connection of the movable block 10 and the guide post 5 increases the stability of the device when the device is opened and retracted and improves the safety of the device;
the inner paddle 23 and the outer paddle 25 form a turnover mechanism through the hinge 24, the turnover angle of the turnover mechanism is 0-180 degrees, the turnover mechanism of the inner paddle 23 and the outer paddle 25 is convenient for a user to turn the outer paddle 25 inwards, and the portability of the device is improved.
When in use, according to the figures 1 and 3, firstly, a user rotates the fixed column 7 anticlockwise to enable the fixed column 7 to move towards the outer end of the control groove 8 through the threaded connection with the control groove 8, and simultaneously, the fixed column 7 is separated from the fixed groove 6, at the moment, the user can rotate the guide pillar 5 towards the outer end of the upright post 3 through the rotary groove 4, so that the included angle between the guide pillar 5 and the unmanned aerial vehicle main body 1 is 90 degrees, then the user rotates the fixed column 7 clockwise to enable the fixed column 7 to move towards the inner end of the control groove 8, meanwhile, the fixed groove 6 fixes the turning angle of the guide pillar 5, then the user can take the slim rod to push towards the inner end of the through hole 16, the slim rod pushes the fixture block 14 to move towards the inner part of the movable groove 17, meanwhile, the fixture block 14 is separated from the fixture groove 15, at the moment, the movable block 10 receives the elastic, meanwhile, the support rod 21 is pushed to move towards the outer end of the guide post 5, the distance between the inner propeller 23 and the unmanned aerial vehicle main body 1 is increased, the lifting force of the inner propeller 23 on the unmanned aerial vehicle main body 1 is improved, and meanwhile, the outer propeller 25 is turned outwards through the hinge 24, so that the outer propeller 25 and the inner propeller 23 are kept parallel and level;
according to fig. 2, the user only needs to pull the support rod 21 towards the outer end of the guide post 5 to make the movable block 10 located at the inner outer end of the telescopic slot 9, and at this time, the latch 14 receives the pushing force of the extension spring 18 in a compressed state to move towards the outer end of the movable slot 17, so that the latch 14 is located inside the slot 15 at the outer end of the guide post 5 to fix the positions of the movable block 10 and the support rod 21, when the movable block 10 moves in the telescopic slot 9, the movable block 10 keeps stable through the sliding of the sliding block 12 in the sliding slot 13, the rotation of the movable block 10 in the telescopic slot 9 is avoided, meanwhile, the stability of the support rod 21 is ensured, the fixture block 14 slides at the outer end of the shaft column 20 through the movable hole 19, the stability of the fixture block 14 during moving is increased, meanwhile, the distortion of the extension spring 18 is avoided, which is the working principle of the multi-rotor unmanned aerial vehicle convenient for folding and storage, and those not described in detail in this specification are well within the skill of those in the art.
In conclusion, the multi-rotor unmanned aerial vehicle convenient to fold and store is obtained, the turnover mechanism of the guide post 5 and the upright post 3 is convenient for a user to store the guide post 5 in the storage groove 2, the storage and transportation of the whole device are convenient, the connection tightness between the fixed post 7 and the control groove 8 is increased by the threaded connection, the turning angle of the guide post 5 is convenient to fix, the telescopic mechanisms of the movable block 10 and the guide post 5 are convenient to store the movable block 10 and the support rod 21, the storage of the device is further convenient, the rotation of the movable block 10 in the telescopic groove 9 can be avoided by the sliding mechanisms of the movable block 10 and the telescopic groove 9, the stability of the support rod 21 is increased, the clamping connection of the movable block 10 and the guide post 5 increases the stability of the device when the device is opened and stored, the safety of the device is improved, the turnover mechanism of the inner paddle 23 and the outer paddle 25 is convenient for the, improving the portability of the device.
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.
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 many rotor unmanned aerial vehicle convenient to folding accomodate, includes unmanned aerial vehicle main part (1) and bracing piece (21), its characterized in that: the unmanned aerial vehicle is characterized in that an object placing groove (2) is formed in the inner end of the outer portion of the unmanned aerial vehicle main body (1), a stand column (3) is fixed to the left end of the inner portion of the object placing groove (2), the outer end of the stand column (3) is connected with a guide column (5) through a rotating groove (4), the outer end of the guide column (5) is connected with the unmanned aerial vehicle main body (1) through a fixing groove (6) and a fixing column (7), the outer end of the fixing column (7) is connected with the unmanned aerial vehicle main body (1) through a control groove (8), the inner portion of the guide column (5) is connected with a movable block (10) through a telescopic groove (9), a supporting spring (11) is arranged in the telescopic groove (9), the inner end of the movable block (10) is connected with the guide column (5) through a sliding block (12) and a sliding groove (13), and the outer end of the movable block (10) is connected with, through-hole (16) have been seted up to the inside of draw-in groove (15) simultaneously, the inner of fixture block (14) is through activity groove (17) and extension spring (18) and movable block (10) interconnect, and the inner inside of movable block (10) is through activity hole (19) and jack-post (20) interconnect, the outer end at movable block (10) is fixed in bracing piece (21), and the outer end of bracing piece (21) passes through motor (22) and interior oar (23) interconnect, and hinge (24) and outer oar (25) interconnect are passed through to the outer end of interior oar (23) simultaneously.
2. A multi-rotor drone convenient to fold and stow according to claim 1, characterized in that: the guide post (5) and the upright post (3) form a turnover mechanism through the rotary groove (4), and the turnover angle of the turnover mechanism is 0-90 degrees.
3. A multi-rotor drone convenient to fold and stow according to claim 1, characterized in that: the outer surface of the fixing column (7) and the inner surface of the control groove (8) are both in thread structures and are in threaded connection.
4. A multi-rotor drone convenient to fold and stow according to claim 1, characterized in that: the movable block (10) and the guide post (5) form a telescopic mechanism through a support spring (11) and a telescopic groove (9), and the initial length of the support spring (11) is equal to the depth of the telescopic groove (9).
5. A multi-rotor drone convenient to fold and stow according to claim 1, characterized in that: the movable block (10) and the telescopic groove (9) form a sliding mechanism through a sliding block (12) and a sliding groove (13), and the sliding direction of the sliding mechanism is the same as that of the telescopic groove (9).
6. A multi-rotor drone convenient to fold and stow according to claim 1, characterized in that: the movable block (10) is connected with the guide post (5) in a clamping mode through a clamping block (14) and a clamping groove (15), and the inner end of the clamping block (14) forms a telescopic mechanism with the movable block (10) through an extension spring (18) and a movable groove (17).
7. A multi-rotor drone convenient to fold and stow according to claim 1, characterized in that: the inner paddle (23) and the outer paddle (25) form a turnover mechanism through a hinge (24), and the turnover angle of the turnover mechanism is 0-180 degrees.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921862088.2U CN211167376U (en) | 2019-10-31 | 2019-10-31 | Many rotor unmanned aerial vehicle convenient to fold and accomodate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921862088.2U CN211167376U (en) | 2019-10-31 | 2019-10-31 | Many rotor unmanned aerial vehicle convenient to fold and accomodate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211167376U true CN211167376U (en) | 2020-08-04 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921862088.2U Expired - Fee Related CN211167376U (en) | 2019-10-31 | 2019-10-31 | Many rotor unmanned aerial vehicle convenient to fold and accomodate |
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| Country | Link |
|---|---|
| CN (1) | CN211167376U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116750227A (en) * | 2023-07-13 | 2023-09-15 | 深圳市畅天游智能科技有限公司 | Portable multi-rotor folding unmanned aerial vehicle |
-
2019
- 2019-10-31 CN CN201921862088.2U patent/CN211167376U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116750227A (en) * | 2023-07-13 | 2023-09-15 | 深圳市畅天游智能科技有限公司 | Portable multi-rotor folding unmanned aerial vehicle |
| CN116750227B (en) * | 2023-07-13 | 2024-01-12 | 深圳市畅天游智能科技有限公司 | Portable multi-rotor folding unmanned aerial vehicle |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200804 Termination date: 20211031 |
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| CF01 | Termination of patent right due to non-payment of annual fee |