CN205345333U - Fast dismouting oar seat device of many rotor crafts - Google Patents
Fast dismouting oar seat device of many rotor crafts Download PDFInfo
- Publication number
- CN205345333U CN205345333U CN201521098279.8U CN201521098279U CN205345333U CN 205345333 U CN205345333 U CN 205345333U CN 201521098279 U CN201521098279 U CN 201521098279U CN 205345333 U CN205345333 U CN 205345333U
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- sliding seat
- screw hole
- seat
- fixing seat
- motor
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Abstract
The utility model discloses a fast dismouting oar seat device of many rotor crafts, including mounting components with install the sliding seat subassembly in mounting components, mounting components includes a motor, and the upper end of motor is provided with two first screw holes, the upper end installation fixing base of motor, the both sides face of fixing base all sets up a constant head tank, the sliding seat subassembly includes a sliding seat, and the up end of sliding seat is provided with the second screw hole, and the upper end that is located the sliding seat sets up a paddle, the upper end of paddle sets up a paddle pressure disk. The utility model discloses under the condition with the help of other instruments not, can realize paddle and driving motor's assembly or separation fast, improved work efficiency greatly, and the oar seat adopts circular structural design, effectively guarantee the motion equilibrium when driving motor rotates, avoid producing because of weight distributes the uneven vibrations that lead to to extension driving motor's life improves having a smooth flight nature of paddle, and overall structure is simple, with low costs, workable.
Description
Technical field
This utility model relates to a kind of oar seat, is specifically related to a kind of multi-rotor aerocraft and dismounts oar base device soon.
Background technology
Along with the acceleration of the popular process of unmanned air vehicle technique advances, multi-rotor aerocraft (unmanned plane) begins at all trades and professions and is used widely.
In actual use, aircraft needs frequently preserving between place and using area or carrying out transition transport between two using areas, in order to ensure to transport safety, the transfer ways generally adopted is: in transport origin, is separated with drive motor dismounting by the blade of aircraft；Then the blade and drive motor of having dismantled separation are transported；On transportation terminal ground, then blade is assembled with drive motor.Visible, how simple and quick efficient disassembly and assembly blade and drive motor, significant.
In prior art, when assembling blade with drive motor, mode mainly with bolts, blade is fixed on drive motor；Therefore, by blade from when drive motor disassembles, it is necessary to use instrument rotating bolt, and then blade disassembled from drive motor.Visible, existing blade and drive motor assembling process and unloading process, all need use instrument, there is the problem wasted time and energy, leverage work efficiency, also increase the additional wear of relevant spare and accessory parts simultaneously, reduce the service life of whole multi-rotor aerocraft.
Summary of the invention
Technical problem to be solved in the utility model is to provide a kind of multi-rotor aerocraft and dismounts oar seat soon, can effectively solve the problems referred to above.
This utility model is achieved through the following technical solutions: a kind of multi-rotor aerocraft dismounts oar base device soon, including fixing holder assembly and the sliding seat assembly being installed in fixing holder assembly, described fixing holder assembly includes a motor, the upper end of motor is provided with two the first screw holes, a fixing seat is installed in the upper end of motor, the bottom of described fixing seat fixedly mounts one or two spring pin or shell fragment, the upper surface of described fixing seat is run through and is arranged two the first screws, fixing seat is fixedly installed in the first screw hole of motor upper end through fixing seat by the first screw, the two sides of described fixing seat are respectively provided with a locating slot, described locating slot is hook-shaped shape, the top side of locating slot is provided with the locking slot upwards offered；
Described sliding seat assembly includes a sliding seat, the upper surface of sliding seat is provided with the second screw hole, the upper end being positioned at sliding seat arranges a blade, the upper end of described blade arranges a blade platen, second screw hole is just being respectively arranged with the 3rd screw hole and the 4th screw hole by described blade platen and blade, second screw hole, the 3rd screw hole and the 4th screw hole are provided with two the second screws, and the bottom of the second screw is fixedly installed in the second screw hole.
As preferred technical scheme, locating slot position is just being provided with two locating dowels by the both sides of described sliding seat, and sliding seat is installed in the locating slot of fixing seat both sides by the locating dowel of both sides.
As preferred technical scheme, described fixing seat is full symmetric structure relative to himself central point, and described sliding seat is full symmetric structure relative to himself central point.
As preferred technical scheme, described fixing seat and the equal cylindrical form of sliding seat, fixing seat upper end offers the circular mounting groove for placing sliding seat.
The beneficial effects of the utility model are: this utility model is not when by other instruments, can quickly realize the assembling of blade and drive motor or separate, substantially increase work efficiency, and oar seat adopts circular configuration design, it is effectively ensured moving equilibrium when drive motor rotates, it is to avoid the vibrations caused because of distribution of weight imbalance produce, thus extending the service life of drive motor, improving blade flight stationarity, overall structure is simple, cost is low, easily process.
Accompanying drawing explanation
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the detonation configuration schematic diagram of fixing holder assembly of the present utility model；
Fig. 2 is the detonation configuration schematic diagram of sliding seat assembly of the present utility model；
Fig. 3 is overall package schematic diagram of the present utility model.
Detailed description of the invention
All features disclosed in this specification, or the step in disclosed all methods or process, except mutually exclusive feature and/or step, all can combine by any way.
This specification (include any accessory claim, summary and accompanying drawing) disclosed in any feature, unless specifically stated otherwise, all can by other equivalences or there is the alternative features of similar purpose replaced.That is, unless specifically stated otherwise, each feature is an example in a series of equivalence or similar characteristics.
As shown in Figure 1, including fixing holder assembly and the sliding seat assembly being installed in fixing holder assembly, described fixing holder assembly includes a motor 10, the upper end of motor 10 is provided with two the first screw holes 11, a fixing seat 7 is installed in the upper end of motor 10, the bottom of described fixing seat 7 fixedly mounts one or two spring pin 9 or shell fragment, the upper surface of described fixing seat 7 is run through and is arranged two the first screws 6, fixing seat is fixedly installed in the first screw hole 11 of motor 10 upper end by the first screw 6 through fixing seat 7, the two sides of described fixing seat 7 are respectively provided with a locating slot 8, described locating slot 8 is in hook-shaped shape, the top side of locating slot 8 is provided with the locking slot upwards offered；
As shown in Figure 2, sliding seat assembly includes a sliding seat 4, the upper surface of sliding seat 4 is provided with the second screw hole, the upper end being positioned at sliding seat arranges a blade 3, the upper end of described blade 3 arranges a blade platen 2, on described blade platen 2 and blade 3, second screw hole being just respectively arranged with the 3rd screw hole and the 4th screw hole, the second screw hole, the 3rd screw hole and the 4th screw hole are provided with two the second screws 1, the bottom of the second screw 1 is fixedly installed in the second screw hole.
Wherein, locating slot position is just being provided with two locating dowels 5 by the both sides of sliding seat, and sliding seat is installed in the locating slot of fixing seat both sides by the locating dowel of both sides.
Fixing seat and the equal cylindrical form of sliding seat, fixing seat 7 upper end offers the circular mounting groove for placing sliding seat.Fixing seat is full symmetric structure relative to himself central point, described sliding seat is full symmetric structure relative to himself central point, it is effectively ensured moving equilibrium when drive motor rotates, the vibrations caused because of distribution of weight imbalance are avoided to produce, thus extending the service life of drive motor, improve blade flight stationarity.
Assembling implementation process is as follows:
1) fixing seat portion group implementation:
Two the first spring pins are fixed on the bottom of fixing seat, with two the first screws fixing seat are locked together and be fixed on motor；
2) sliding seat assembly implementation:
With two the second screws, blade platen is fixed and in sliding seat together with blade；
3) the sliding seat assembly assembled is taken, locating dowel in sliding seat is pressed downward against along the locating slot of fixing seat portion group two upper fixed seat, spring pin compresses retrogressing under force, sliding seat assembly is pressed onto the direction of the fixing seat locating slot of end tailing edge and turns clockwise and unclamp after sliding seat, and sliding seat is stuck in the draw-in groove position of sliding seat under the effect of the restoring force of spring pin and realizes blade and be connected with the quick of motor.
Release unloading process is as follows:
1) pressing sliding seat assembly, sliding seat presses down in the guiding of fixing seat locating slot, and now spring pin compression stress retreats, and sliding seat portion group one is rotated counterclockwise along the direction of fixing seat locating slot and can realize blade and motor sharp separation.
The beneficial effects of the utility model are: this utility model is not when by other instruments, can quickly realize the assembling of blade and drive motor or separate, substantially increase work efficiency, and oar seat adopts circular configuration design, it is effectively ensured moving equilibrium when drive motor rotates, it is to avoid the vibrations caused because of distribution of weight imbalance produce, thus extending the service life of drive motor, improving blade flight stationarity, overall structure is simple, cost is low, easily process.
The above, be only detailed description of the invention of the present utility model, but protection domain of the present utility model be not limited thereto, any change expected without creative work or replacement, all should be encompassed within protection domain of the present utility model.Therefore, protection domain of the present utility model should be as the criterion with claims protection defined.
Claims (4)
1. a multi-rotor aerocraft dismounts oar base device soon, it is characterized in that: include fixing holder assembly and the sliding seat assembly being installed in fixing holder assembly, described fixing holder assembly includes a motor, the upper end of motor is provided with two the first screw holes, a fixing seat is installed in the upper end of motor, the bottom of described fixing seat fixedly mounts one or two spring pin or shell fragment, the upper surface of described fixing seat is run through and is arranged two the first screws, fixing seat is fixedly installed in the first screw hole of motor upper end through fixing seat by the first screw, the two sides of described fixing seat are respectively provided with a locating slot, described locating slot is hook-shaped shape, the top side of locating slot is provided with the locking slot upwards offered；
Described sliding seat assembly includes a sliding seat, the upper surface of sliding seat is provided with the second screw hole, the upper end being positioned at sliding seat arranges a blade, the upper end of described blade arranges a blade platen, second screw hole is just being respectively arranged with the 3rd screw hole and the 4th screw hole by described blade platen and blade, second screw hole, the 3rd screw hole and the 4th screw hole are provided with two the second screws, and the bottom of the second screw is fixedly installed in the second screw hole.
2. multi-rotor aerocraft according to claim 1 dismounts oar base device soon, it is characterised in that: locating slot position is just being provided with two locating dowels by the both sides of described sliding seat, and sliding seat is installed in the locating slot of fixing seat both sides by the locating dowel of both sides.
3. multi-rotor aerocraft according to claim 1 dismounts oar base device soon, it is characterised in that: described fixing seat is full symmetric structure relative to himself central point, and described sliding seat is full symmetric structure relative to himself central point.
4. multi-rotor aerocraft according to claim 1 dismounts oar base device soon, it is characterised in that: described fixing seat and the equal cylindrical form of sliding seat, fixing seat upper end offers the circular mounting groove for placing sliding seat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521098279.8U CN205345333U (en) | 2015-12-24 | 2015-12-24 | Fast dismouting oar seat device of many rotor crafts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521098279.8U CN205345333U (en) | 2015-12-24 | 2015-12-24 | Fast dismouting oar seat device of many rotor crafts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205345333U true CN205345333U (en) | 2016-06-29 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521098279.8U Expired - Fee Related CN205345333U (en) | 2015-12-24 | 2015-12-24 | Fast dismouting oar seat device of many rotor crafts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205345333U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106347653A (en) * | 2016-11-18 | 2017-01-25 | 深圳市道通智能航空技术有限公司 | Power device, propeller and aircraft |
| CN106672210A (en) * | 2017-02-21 | 2017-05-17 | 上海未来伙伴机器人有限公司 | Quick disassembly propeller and unmanned aerial vehicle adopting same |
| CN107187591A (en) * | 2017-05-27 | 2017-09-22 | 昆山优尼电能运动科技有限公司 | Portable unmanned machine, blade runner assembly, rotation system and its assemble method |
| CN107187590A (en) * | 2017-05-27 | 2017-09-22 | 昆山优尼电能运动科技有限公司 | Portable unmanned machine, blade runner assembly, rotation system and its assemble method |
| CN107352027A (en) * | 2017-07-25 | 2017-11-17 | 成都天麒科技有限公司 | A kind of unmanned plane blade attachment structure |
| WO2018027683A1 (en) * | 2016-08-10 | 2018-02-15 | 张琬彬 | Quick disassembling and assembling wing of unmanned aerial vehicle |
| WO2018090281A1 (en) * | 2016-11-17 | 2018-05-24 | XDynamics Limited | A manually detachable locking mechanism |
| WO2018161406A1 (en) * | 2017-03-10 | 2018-09-13 | 歌尔科技有限公司 | Quick installation and removal structure for propeller, and unmanned aerial vehicle |
| CN114701645A (en) * | 2022-04-02 | 2022-07-05 | 深圳市昱晟通讯设备有限公司 | Multi-rotor unmanned aerial vehicle |
-
2015
- 2015-12-24 CN CN201521098279.8U patent/CN205345333U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018027683A1 (en) * | 2016-08-10 | 2018-02-15 | 张琬彬 | Quick disassembling and assembling wing of unmanned aerial vehicle |
| WO2018090281A1 (en) * | 2016-11-17 | 2018-05-24 | XDynamics Limited | A manually detachable locking mechanism |
| CN106347653A (en) * | 2016-11-18 | 2017-01-25 | 深圳市道通智能航空技术有限公司 | Power device, propeller and aircraft |
| CN106347653B (en) * | 2016-11-18 | 2019-12-10 | 深圳市道通智能航空技术有限公司 | power device, screw and aircraft |
| US10759526B2 (en) | 2016-11-18 | 2020-09-01 | Autel Robotics Co., Ltd. | Power assembly and aircraft |
| CN106672210A (en) * | 2017-02-21 | 2017-05-17 | 上海未来伙伴机器人有限公司 | Quick disassembly propeller and unmanned aerial vehicle adopting same |
| CN106672210B (en) * | 2017-02-21 | 2023-09-05 | 上海未来伙伴机器人有限公司 | Quick detach oar and adopt its unmanned aerial vehicle |
| WO2018161406A1 (en) * | 2017-03-10 | 2018-09-13 | 歌尔科技有限公司 | Quick installation and removal structure for propeller, and unmanned aerial vehicle |
| CN107187591A (en) * | 2017-05-27 | 2017-09-22 | 昆山优尼电能运动科技有限公司 | Portable unmanned machine, blade runner assembly, rotation system and its assemble method |
| CN107187590A (en) * | 2017-05-27 | 2017-09-22 | 昆山优尼电能运动科技有限公司 | Portable unmanned machine, blade runner assembly, rotation system and its assemble method |
| CN107352027A (en) * | 2017-07-25 | 2017-11-17 | 成都天麒科技有限公司 | A kind of unmanned plane blade attachment structure |
| CN114701645A (en) * | 2022-04-02 | 2022-07-05 | 深圳市昱晟通讯设备有限公司 | Multi-rotor unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170313 Address after: 518000 Guangdong Province, Shenzhen City Shilong Baoan District Shiyan Street Community Yihe Road No. 1 Corbett aviation science and Technology Park Building 3 (Yuan Jin Dahua Industrial Zone) Patentee after: SHENZHEN MICROMULTICOPTER Co.,Ltd. Address before: 518000 Guangdong city of Shenzhen province Baoan District A road 301 building a garden together Patentee before: Lu Zhihui |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20171019 Address after: Jiaxing City, Zhejiang province Jiashan County 314100 street to Luoxing Valley Park Business Center D block 4 Building Patentee after: ZHEJIANG KEBITE TECHNOLOGY CO.,LTD. Address before: 518000 Guangdong Province, Shenzhen City Shilong Baoan District Shiyan Street Community Yihe Road No. 1 Corbett aviation science and Technology Park Building 3 (Yuan Jin Dahua Industrial Zone) Patentee before: SHENZHEN MICROMULTICOPTER Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160629 Termination date: 20211224 |
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| CF01 | Termination of patent right due to non-payment of annual fee |