CN204750578U - Unmanned aerial vehicle battery quick assembly disassembly structure - Google Patents
Unmanned aerial vehicle battery quick assembly disassembly structure Download PDFInfo
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- CN204750578U CN204750578U CN201520439549.0U CN201520439549U CN204750578U CN 204750578 U CN204750578 U CN 204750578U CN 201520439549 U CN201520439549 U CN 201520439549U CN 204750578 U CN204750578 U CN 204750578U
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- slide rail
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- frame
- clamping boss
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- 230000008569 process Effects 0.000 claims description 9
- 238000005516 engineering process Methods 0.000 description 3
- OJIJEKBXJYRIBZ-UHFFFAOYSA-N cadmium nickel Chemical compound [Ni].[Cd] OJIJEKBXJYRIBZ-UHFFFAOYSA-N 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000003032 molecular docking Methods 0.000 description 2
- 206010044565 Tremor Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
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- 238000004364 calculation method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000037433 frameshift Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
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- 238000000926 separation method Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Abstract
The utility model discloses an unmanned aerial vehicle battery quick assembly disassembly structure, include battery (1) and frame (2) that battery case (3) upper surface is the protruding joint boss (4) that forms upwards, is equipped with slide rail (5) in the frame, the battery passes through joint realization and frame sliding connection between joint boss and slide rail, movable buckle (6) are installed to slide rail one end, and joint boss one end is outwards extended and is formed extension portion (7), and h activity buckle cooperates with extension portion to be fixed the battery in the frame. This compact structure, simple, the steadiness is good to can realize the quick assembly disassembly of battery.
Description
Technical field
The utility model belongs to unmanned plane battery quick fixation structure field, particularly relates to a kind of unmanned plane battery fast assembling disassembling structure.
Background technology
Robot airplane is called for short " unmanned plane ", and english abbreviation is " UAV ", is the non-manned aircraft utilizing radio robot to handle with the process controller provided for oneself.
In order to simplify the project organization of unmanned plane, sometimes fuselage being separated setting with power supply, when needs use unmanned plane, power supply and fuselage being connected, when not needing to use unmanned plane, power supply dismounting being placed, is so also beneficial to the maintenance of fuselage and power supply.
Existing unmanned plane is when installing power supply, the mode of the special bond bonding of usual employing or binding fixes, but due to the own wt that power supply has, in the process bondd or bundle, often need the more material of cost and time, and fixed effect is undesirable, shakes when flying because air-flow or other external factor will cause unmanned plane to produce or jolt simultaneously, power supply easily gets loose, and has certain risk.
Chinese patent 201020176806.3, disclose a kind of telecontrolled aircraft battery fixing structure, track strip is provided with in the inner side of two body plates, track strip is formed with rail groove, and be provided with that carrier plate is embedding is combined in rail groove, forming carrier plate can slide according to rail groove, and carrier plate is for stationary battery, and battery can be made to insert in body plate when promoting carrier plate, or exit body plate simultaneously.
In the program, battery and carrier plate group are determined, and carrier plate can be twitched according to track strip rail groove, and when battery changed by needs or battery need charge, namely only need extract carrier plate out is extract battery out, in like manner, pushes carrier plate and battery can be made to insert in fuselage.
But, be equivalent to one piece of adapter plate in the program and rail groove is supporting is slidably socketed, if only fixed with such structure, aircraft is in flight course, adapter plate to be easy to from rail groove slippage out, and also disclose in open text, also arranged the connecting element such as positioning strip, screw, these connecting elements cause battery in the process removed and installed and are not easy by fast assembling-disassembling.
Chinese patent 03246060.0, disclose a kind of aircraft cadmium-nickel alkaline storage battery, it is disclosed that the locating dowel pin be provided with on cadmium-nickel storage battery on erecting frame that registration arm is connected with aircraft is slippery, between locating dowel pin one end and the guide pin bushing bottom surface of erecting frame, be provided with spring.One end and the erecting frame of bolt are hinged, and bolt is provided with nut, and the lower end of this nut is provided with an exit skirt, link up with match with the L-type be fixed on storage battery.
Be that the location that hand-held storage battery makes its registration arm aim on erecting frame shifts the end onto slightly toward inner, namely completes docking with the docking calculation of aircraft, swing bolt and rotating nut makes the exit skirt of nut and L-type link up with clamps simultaneously, depart from from erecting frame to prevent storage battery.
As can be seen from such scheme, phase is installed to convenient, but can not quick-detachment easily when dismantling battery.
Utility model content
The technical problems to be solved in the utility model is to provide a kind of compact conformation, simple, anti-loose, and can realize the unmanned plane battery fast assembling disassembling structure of fast assembling-disassembling.
The concrete technical scheme realizing foregoing invention object is as follows: a kind of unmanned plane battery fast assembling disassembling structure, comprise battery and frame, battery case upper surface raises up and forms clamping boss, and frame is provided with slide rail, and battery is connected with housing slide with the clamping realization between slide rail by clamping boss; Slide rail one end is provided with movable buckle, and clamping boss one end stretches out formation elongated portion, and movable buckle coordinates with elongated portion and is fixed in frame by battery.
The unmanned plane battery fast assembling disassembling structure that the utility model provides, can realize fast assembling-disassembling, specific operation process is: when needs are to when unmanned plane arranging battery, the shell of battery arranges clamping boss, frame arranges slide rail, and clamping boss slips into slide rail, battery and housing slide clamping.Prevent it from coming off to reinforce battery, the frame of slide rail one end is arranged can the movable buckle of direct manual dismounting, one end of clamping boss arranges an elongated portion, elongated portion offers the draw-in groove coordinated with movable buckle, after clamping boss slips into slide rail predeterminated position, elongated portion stretches out slide rail, and this draw-in groove coordinates clamping with the movable buckle that frame is arranged simultaneously, is directly fixed in frame by battery.
When needs dismounting battery, directly manually, by movable buckle and exact separation, battery can be separated with frame, dismantles complete.
So the structure that this programme provides can realize fast assembling-disassembling battery, and simple structure, simple to operate, the stability maintenance of battery is good simultaneously.
Further, slide rail is opened in the surface of frame or is connected with frame by slide rail by attaching parts.
Further, the both sides of slide rail fixedly prevent battery from departing from the stop sidewall of slide rail, stop that the top of sidewall is zigzag structure part; Clamping boss both sides have and stop the sawtooth that the incised groove structure of sidewall matches.Stop the tooth in the zigzag structure part that the top of sidewall is arranged, and the tooth in the broached-tooth design of clamping boss both sides setting, its size is all equal, and shape is all identical.
Further, clamping boss is fixed on the top of battery case, and slide rail is arranged on the bottom of frame.
Further, slide rail is wedge grooved passageway, and clamping boss is the shape that wedge-like coordinates with slide rail.
Further, movable buckle is Elastic buckle, and one end of Elastic buckle is fixedly connected with frame, the draw-in groove clamping that the other end and clamping boss are offered, and when disassembly is desired, under outside pulling force effect, buckle is separated with one end of draw-in groove clamping; When needs are assembled, under inside thrust, buckle and draw-in groove clamping.
Further, buckle is slip buckle, and slip buckle is located at one end of slide rail, and can reciprocatingly slide along the direction vertical with the length direction of slide rail.
Further, the end face of clamping boss is provided with in unloading process the holding groove that the buckle that slides is stagnated, and holding groove is rectangular recess, and the length direction along clamping boss is arranged, and the width of groove is more than or equal to the width of slip buckle; During dismounting battery, automatically can glide when slip buckle is fixed without external force, now can fall into holding groove.
Advantage of the present utility model and feature are: 1, simple structure, easily makes; 2, battery installation steadiness is good; 3, easy disassembling, save disassembly and assembly time, efficiency is high; 4, effectively prevent battery from coming off; 5, avoiding additionally increasing too much physical weight to unmanned plane causes it to run shakiness.
Accompanying drawing explanation
The structural representation being provided with the battery of clamping boss that Fig. 1 provides for the utility model;
Fig. 2 is the structural representation of the frame being provided with slide rail and fixing buckle;
Fig. 3 is the package assembly schematic diagram of battery and frame;
In figure, 1, battery; 2, frame; 3, shell; 4, clamping boss; 5, slide rail; 6, fixing buckle; 7, elongated portion; 8, holding groove; 9, sawtooth; 10, zigzag structure; 11, draw-in groove.
Detailed description of the invention
Embodiment 1:
A kind of unmanned plane battery fast assembling disassembling structure, as shown in Figure 1-Figure 3, comprise battery 1 and frame 2, battery case 3 upper surface middle part raises up and forms clamping boss 4, frame 2 is provided with slide rail 5, and battery 1 is by the clamping realization between clamping boss 4 and slide rail 5 and frame 2 sliding block joint;
Slide rail 5 one end is provided with removable buckle 6, and clamping boss one end stretches out and forms elongated portion 7, and offer draw-in groove 11 on elongated portion surface, when battery moves to buckle place along slide rail, battery is fixed in frame by draw-in groove and bayonet fitting.
Embodiment 2:
A kind of unmanned plane battery 1 fast assembling disassembling structure, comprise battery 1 and frame 2, battery case 3 upper surface middle part raises up and forms clamping boss 4, frame 2 is provided with slide rail 5, slide rail 5 is opened in the surface of frame 2 or is connected with frame 2 by slide rail 5 by attaching parts, clamping boss is fixed on the top of battery case, and slide rail is arranged on the bottom of frame.Slide rail 5 is wedge grooved passageway, and clamping boss 4 is the shape that wedge-like coordinates with slide rail.
Battery is by the clamping realization between clamping boss 4 and slide rail 5 and frame 2 sliding block joint; Slide rail 5 one end is provided with removable buckle 6, and clamping boss 4 one end stretches out and forms elongated portion 7, offers draw-in groove 11 on elongated portion surface, and when battery moves to buckle place along slide rail 5, battery is fixed in frame 2 by draw-in groove 11 and bayonet fitting.
The both sides of slide rail 5 fixedly prevent battery from departing from the stop sidewall of slide rail, and stop that the top of sidewall is zigzag structure 10, clamping boss both sides have and stop the sawtooth 9 that the incised groove structure of sidewall matches;
Space of tooth in zigzag structure 10 is equal with the space of tooth of the sawtooth 9 that clamping boss 4 both sides are set up separately, meanwhile, and the facewidth degree in the sawtooth 9 of interval width >=clamping boss 4 both sides of tooth adjacent in the zigzag structure 10 on slide rail 5.
In this embodiment, the speed of dismounting battery 1 can be improved further.Particularly, in zigzag structure 10 on slide rail 5, keep at a certain distance away between adjacent tooth, and the zigzag structure 10 on both sides stop sidewall is for being symmetrical arranged, the both sides that the boss of clamping simultaneously 4 contacts with slide rail 5 are also respectively equipped with sawtooth, and during installation, clamping boss 4 slips into the predeterminated position in slide rail 5, slide rail 5 is corresponding with the tooth on clamping boss 4 to be stopped, prevents clamping boss 4 from coming off from slide rail 5; When needs dismounting battery 1, slide rail 5 is stopped the tooth of tooth on sidewall in zigzag structure 10 and clamping boss 4 both sides staggers, the interval namely making the tooth of clamping boss 4 both sides be positioned at slide rail 5 to stop adjacent teeth on sidewall, now, directly battery 1 can be taken out from slide rail 5, and not need clamping boss 4 again to run through completely and slip over slide rail 5 and just can take out.
Conveniently make, improve make efficiency, preferably, the tooth in the zigzag structure 10 of the top setting of the stop sidewall of slide rail 5, all equal with its size of sawtooth 9 that clamping boss 4 both sides are arranged, shape is all identical.
Preferably, the tooth in the zigzag structure part 10 of the top setting of the stop sidewall of slide rail 5, and the tooth in the broached-tooth design 9 of clamping boss 4 both sides setting, it is the equal rectangle of size or triangle.
When being set to triangle, with it, the tooth that the stop sidewall of slide rail 5 both sides is arranged respectively thinks that tooth that corresponding clamping boss 4 both sides arrange is for being symmetrical arranged
Embodiment 3:
A kind of unmanned plane battery 1 fast assembling disassembling structure, comprise battery 1 and frame 2, battery case 3 upper surface middle part raises up and forms clamping boss 4, frame 2 is provided with slide rail 5, slide rail 5 is opened in the surface of frame 2 or is connected with frame 2 by slide rail 5 by attaching parts, clamping boss is fixed on the top of battery case, and slide rail is arranged on the bottom of frame.Slide rail 5 is wedge grooved passageway, and clamping boss 4 is the shape that wedge-like coordinates with slide rail.
One end of slide rail 5 is provided with can the Elastic buckle of direct manual dismounting, one end of Elastic buckle is fixedly connected with frame 2, draw-in groove 11 clamping that the other end and clamping boss 4 are arranged, when disassembly is desired, under outside pulling force effect, Elastic buckle is separated with one end of draw-in groove 11 clamping; When needs are assembled, under inside thrust, Elastic buckle and draw-in groove 11 clamping.
In the program, buckle 6 is set to Elastic buckle, more easily by battery 1 and frame 2 snapping, and can not need can complete by external tool or external force in the process of dismounting, and fixes effective.
Preferably, buckle 6 is slip buckle, and slip buckle is located at one end of slide rail 5, and can reciprocatingly slide along the direction vertical with the length direction of slide rail 5.
One end of slip buckle is wedge shape, and one end of wedge shape is slipped in the draw-in groove 11 on clamping boss 4, with its socket.
When installing battery 1, slip buckle is slided to the side of slide rail 5, clamping boss 4 slips into slide rail 5, and after arriving predeterminated position, slip buckle restores, and on it, one end of wedge shape is slipped in the draw-in groove on clamping boss 4, is fixed in frame 2 by battery 1.
When dismantling battery 1, moved to the direction away from slide rail 5 by slip buckle, one end of wedge shape is separated with the draw-in groove 11 on clamping boss 4, and battery 1 skids off from slide rail 5 along with clamping boss 4, is disassembled.
In order to prevent in the process of dismounting battery 1, slip buckle is not fixed, easily slide back to initial position, shock is caused to clamping boss 4, preferably, the end face of clamping boss 4 is provided with in unloading process the holding groove 8 that the buckle that slides is stagnated, and holding groove 8 is rectangular recess, Width along clamping boss 4 is arranged, and the width of groove is more than or equal to the maximum width of slip buckle; During dismounting battery, automatically can glide when slip buckle is fixed without external force, now can fall into holding groove 8.
The above; for the better case study on implementation of the utility model content; not utility model content is imposed any restrictions; every above embodiment is done according to the utility model content technologies essence any simple modification, change and equivalent structure change, all still belong in the protection domain of the utility model content technologies scheme.
Claims (8)
1. a unmanned plane battery fast assembling disassembling structure, comprise battery (1) and frame (2), it is characterized in that, battery case (3) upper surface raises up and forms clamping boss (4), frame is provided with slide rail (5), and battery is connected with housing slide with the clamping realization between slide rail by clamping boss; Slide rail one end is provided with movable buckle (6), and clamping boss one end stretches out and forms elongated portion (7), and buckle coordinates with elongated portion and is fixed in frame by battery.
2. unmanned plane battery fast assembling disassembling structure according to claim 1, is characterized in that, slide rail is opened in the surface of frame or is connected with frame by slide rail by attaching parts.
3. unmanned plane battery fast assembling disassembling structure according to claim 1, is characterized in that, the both sides of slide rail are the stop sidewall preventing battery from departing from slide rail, stops that the top of sidewall is zigzag structure (10); Clamping boss both sides have and the sawtooth (9) stopping that the incised groove structure of sidewall matches.
4. unmanned plane battery fast assembling disassembling structure according to claim 1, it is characterized in that, clamping boss is fixed on the top of battery case, and slide rail is arranged on the bottom of frame.
5. unmanned plane battery fast assembling disassembling structure according to claim 1, is characterized in that, slide rail is wedge grooved passageway, and clamping boss is the shape that wedge-like coordinates with slide rail.
6. unmanned plane battery fast assembling disassembling structure according to claim 1, it is characterized in that, movable buckle is Elastic buckle, draw-in groove (11) is offered on the elongated portion surface of clamping boss, one end of Elastic buckle is fixedly connected with frame, the other end can with the draw-in groove clamping that arranges on clamping boss, when disassembly is desired, under outside pulling force effect, Elastic buckle is separated with one end of draw-in groove clamping; When needs are assembled, under inside thrust, Elastic buckle and draw-in groove clamping.
7. unmanned plane battery fast assembling disassembling structure according to claim 1, is characterized in that, movable buckle is slip buckle, and slip buckle is located at one end of slide rail, and can reciprocatingly slide along the direction vertical with the length direction of slide rail.
8. unmanned plane battery fast assembling disassembling structure according to claim 7, it is characterized in that, the end face of clamping boss is provided with in unloading process the holding groove (8) that the buckle that slides is stagnated, holding groove is rectangular recess, Width along clamping boss is arranged, and the width of groove is more than or equal to the width of slip buckle; During dismounting battery, automatically can glide when slip buckle is fixed without external force, now can fall into holding groove.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520439549.0U CN204750578U (en) | 2015-06-24 | 2015-06-24 | Unmanned aerial vehicle battery quick assembly disassembly structure |
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| CN201520439549.0U CN204750578U (en) | 2015-06-24 | 2015-06-24 | Unmanned aerial vehicle battery quick assembly disassembly structure |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017185488A1 (en) * | 2016-04-28 | 2017-11-02 | 深圳市龙云创新航空科技有限公司 | Tool-free structure for fast replacement and mounting of external module to unmanned aerial vehicle |
| CN108297950A (en) * | 2018-01-17 | 2018-07-20 | 西安工业大学 | Carry the crawler type offroad vehicle and its method of unmanned plane |
| WO2018152785A1 (en) * | 2017-02-24 | 2018-08-30 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
-
2015
- 2015-06-24 CN CN201520439549.0U patent/CN204750578U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017185488A1 (en) * | 2016-04-28 | 2017-11-02 | 深圳市龙云创新航空科技有限公司 | Tool-free structure for fast replacement and mounting of external module to unmanned aerial vehicle |
| WO2018152785A1 (en) * | 2017-02-24 | 2018-08-30 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN108521774A (en) * | 2017-02-24 | 2018-09-11 | 深圳市大疆创新科技有限公司 | Unmanned vehicle |
| CN108297950A (en) * | 2018-01-17 | 2018-07-20 | 西安工业大学 | Carry the crawler type offroad vehicle and its method of unmanned plane |
| CN108297950B (en) * | 2018-01-17 | 2024-03-22 | 西安工业大学 | Crawler-type off-road vehicle carrying unmanned aerial vehicle and method thereof |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Unmanned aerial vehicle battery quick assembly disassembly structure Effective date of registration: 20170327 Granted publication date: 20151111 Pledgee: XinDa national equity investment fund (Shanghai) partnership (L.P.)|Beijing Civil Aviation Heyuan Investment Center (L.P.) Pledgor: ZEROTECH (BEIJING) INTELLIGENCE TECHNOLOGY Co.,Ltd. Registration number: 2017990000242 |
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Effective date of registration: 20190906 Granted publication date: 20151111 |
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Date of cancellation: 20220406 Granted publication date: 20151111 |
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Effective date of registration: 20220406 Granted publication date: 20151111 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20221008 Granted publication date: 20151111 Pledgee: XinDa national equity investment fund (Shanghai) partnership (L.P.)|Beijing Civil Aviation Heyuan Investment Center (L.P.) Pledgor: ZEROTECH (BEIJING) INTELLIGENCE TECHNOLOGY Co.,Ltd. Registration number: 2017990000242 |
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Effective date of registration: 20220918 Granted publication date: 20151111 |