CN204197289U - A kind of rack construction of many rotor wing unmanned aerial vehicles - Google Patents
A kind of rack construction of many rotor wing unmanned aerial vehicles Download PDFInfo
- Publication number
- CN204197289U CN204197289U CN201420659368.4U CN201420659368U CN204197289U CN 204197289 U CN204197289 U CN 204197289U CN 201420659368 U CN201420659368 U CN 201420659368U CN 204197289 U CN204197289 U CN 204197289U
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- telescopic rod
- unmanned aerial
- rotor wing
- wing unmanned
- aerial vehicles
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Abstract
The utility model discloses a kind of rack construction of many rotor wing unmanned aerial vehicles, comprise Rack Body and multiple screw propeller, described Rack Body comprises upper cover plate and lower cover, connector is fixedly welded with between described upper cover plate and described lower cover, the sidewall of described connector is provided with the telescopic rod of many hollow structures, described screw propeller is arranged on described telescopic rod, many described telescopic rods and multiple described screw propeller one_to_one corresponding.The rack construction of many rotor wing unmanned aerial vehicles described in the utility model, be provided with telescopic rod, when recovery is deposited, collapsible telescopic rod, by the overall framework shrinkage of unmanned plane frame to minimum, greatly saved parking space, and telescopic rod can be hollow structure, the control cable of the driver train of screw propeller can penetrate and extend to Rack Body in telescopic rod, and the installation of control system is more simple, reliable.
Description
Technical field
The utility model relates to a kind of unmanned plane, particularly relates to a kind of rack construction with many rotor wing unmanned aerial vehicles of telescopic rod.
Background technology
Unmanned plane is that one is in and develops middle modernization high-end devices rapidly, its have maneuverability, reaction fast, unmanned flight and the low advantage of operation requirements.Unmanned plane is by carrying multiclass sensor, the function such as image real-time Transmission and high-risk areas detection can be realized, at present, many rotor wing unmanned aerial vehicles many, it has the advantages such as flight stability, power is strong, but many rotor wing unmanned aerial vehicles are when recovery is deposited, because the overall skeleton of its frame is comparatively large, often take larger space.
Utility model content
The purpose of this utility model is just to provide a kind of rack construction with many rotor wing unmanned aerial vehicles of telescopic rod to solve the problem.
The utility model is achieved through the following technical solutions above-mentioned purpose:
A kind of rack construction of many rotor wing unmanned aerial vehicles, comprise Rack Body and multiple screw propeller, described Rack Body comprises upper cover plate and lower cover, connector is fixedly welded with between described upper cover plate and described lower cover, the sidewall of described connector is provided with the telescopic rod of many hollow structures, described screw propeller is arranged on described telescopic rod, many described telescopic rods and multiple described screw propeller one_to_one corresponding.
As preferably, described upper cover plate and described lower cover are circle, and be provided with square hole in the middle of described upper cover plate and described lower cover, described connector is the square body of hollow structure.
As preferably, the inwall of described connector is provided with link.
Further, one end of described telescopic rod is provided with adapter plate, and described adapter plate is bolted on the sidewall of described connector, and the other end of described telescopic rod is telescopic end, and described screw propeller is arranged on the telescopic end of described telescopic rod.
As preferably, described telescopic rod is provided with pin and multiple pin-and-hole.
As preferably, described upper cover plate, described lower cover, described connector and described telescopic rod are light aluminum alloy material.
The beneficial effects of the utility model are:
The rack construction of many rotor wing unmanned aerial vehicles described in the utility model, be provided with telescopic rod, when recovery is deposited, collapsible telescopic rod, by the overall framework shrinkage of unmanned plane frame to minimum, greatly saved parking space, and telescopic rod can be hollow structure, the control cable of the driver train of screw propeller can penetrate and extend to Rack Body in telescopic rod, and the installation of control system is more simple, reliable.
Accompanying drawing explanation
Fig. 1 is the birds-eye view of the rack construction of many rotor wing unmanned aerial vehicles described in the utility model;
Fig. 2 is the lateral plan of the rack construction of many rotor wing unmanned aerial vehicles described in the utility model;
Fig. 3 is the cutaway view of Rack Body described in the utility model.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail:
As shown in Figure 1, Figure 2 and Figure 3, the utility model comprises Rack Body and multiple screw propeller 1, Rack Body comprises upper cover plate 3 and lower cover 6, connector 5 is fixedly welded with between upper cover plate 3 and lower cover 6, the sidewall of connector 5 is provided with the telescopic rod 2 of many hollow structures, screw propeller 1 is arranged on telescopic rod 2, many telescopic rods 2 and multiple screw propeller 1 one_to_one corresponding.
The rack construction of many rotor wing unmanned aerial vehicles described in the utility model, upper cover plate 3 and lower cover 6 are circle, square hole is provided with in the middle of upper cover plate 3 and lower cover 6, connector 5 is the square body of hollow structure, upper cover plate 3, lower cover 6, connector 5 and telescopic rod 2 are light aluminum alloy material, this structure not only can alleviate the weight of frame, and conveniently installs auxiliary accessories.The inwall of connector 5 is provided with link 4, can carry some article or install auxiliary accessories by link 4.One end of telescopic rod 2 is provided with adapter plate 7, adapter plate 7 is fixed on the sidewall of connector 5 by bolt 8, screw propeller 1 and telescopic rod 2 all can be disassembled from Rack Body easily, and the other end of telescopic rod 2 is telescopic end, and screw propeller 1 is arranged on the telescopic end of telescopic rod 2.Telescopic rod 2 is provided with pin 22 and multiple pin-and-hole 21, by by one of them pin-and-hole 21 of the insertion of pin 22 correspondence, can adjusts and fix the length of telescopic rod.
The rack construction of many rotor wing unmanned aerial vehicles described in the utility model, be provided with telescopic rod 2, when recovery is deposited, collapsible telescopic rod 2, can by the overall framework shrinkage of unmanned plane frame to minimum, greatly save parking space, and telescopic rod 2 is hollow structure, the control cable of the driver train of screw propeller 1 can penetrate and extend to Rack Body in telescopic rod 2, the installation of control system is simpler, reliably, if need long term storage, then many telescopic rods 2 can be taken off from Rack Body very easily.
These are only preferred embodiment of the present utility model, not in order to limit the utility model, all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included in protection domain of the present utility model.
Claims (6)
1. the rack construction of rotor wing unmanned aerial vehicle more than a kind, comprise Rack Body and multiple screw propeller, it is characterized in that: described Rack Body comprises upper cover plate and lower cover, connector is fixedly welded with between described upper cover plate and described lower cover, the sidewall of described connector is provided with the telescopic rod of many hollow structures, described screw propeller is arranged on described telescopic rod, many described telescopic rods and multiple described screw propeller one_to_one corresponding.
2. the rack construction of many rotor wing unmanned aerial vehicles according to claim 1, is characterized in that: described upper cover plate and described lower cover are circle, and be provided with square hole in the middle of described upper cover plate and described lower cover, described connector is the square body of hollow structure.
3. the rack construction of many rotor wing unmanned aerial vehicles according to claim 2, is characterized in that: the inwall of described connector is provided with link.
4. the rack construction of many rotor wing unmanned aerial vehicles according to claim 1, it is characterized in that: one end of described telescopic rod is provided with adapter plate, described adapter plate is bolted on the sidewall of described connector, the other end of described telescopic rod is telescopic end, and described screw propeller is arranged on the telescopic end of described telescopic rod.
5. the rack construction of many rotor wing unmanned aerial vehicles according to claim 1, is characterized in that: described telescopic rod is provided with pin and multiple pin-and-hole.
6. the rack construction of many rotor wing unmanned aerial vehicles according to claim 1, is characterized in that: described upper cover plate, described lower cover, described connector and described telescopic rod are light aluminum alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420659368.4U CN204197289U (en) | 2014-11-05 | 2014-11-05 | A kind of rack construction of many rotor wing unmanned aerial vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420659368.4U CN204197289U (en) | 2014-11-05 | 2014-11-05 | A kind of rack construction of many rotor wing unmanned aerial vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204197289U true CN204197289U (en) | 2015-03-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420659368.4U Expired - Fee Related CN204197289U (en) | 2014-11-05 | 2014-11-05 | A kind of rack construction of many rotor wing unmanned aerial vehicles |
Country Status (1)
| Country | Link |
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| CN (1) | CN204197289U (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104787327A (en) * | 2015-05-12 | 2015-07-22 | 无锡职业技术学院 | Axle distance-variable multi-rotor aircraft |
| CN104875888A (en) * | 2015-04-13 | 2015-09-02 | 华南农业大学 | Detachable ring-pillar type hollow unmanned aerial vehicle and operation method thereof |
| CN105173058A (en) * | 2015-09-25 | 2015-12-23 | 联想(北京)有限公司 | Electronic equipment |
| CN105292510A (en) * | 2015-11-21 | 2016-02-03 | 长沙学院 | Multi-functional aerial photography aircraft |
| CN106275382A (en) * | 2016-08-10 | 2017-01-04 | 张琬彬 | A kind of unmanned plane fast assembling-disassembling wing |
| CN106275383A (en) * | 2016-08-10 | 2017-01-04 | 张琬彬 | A kind of unmanned plane wing-folding structure |
| CN106314783A (en) * | 2016-10-24 | 2017-01-11 | 杭州鼎曜信息技术有限公司 | Anti-hurt multi-rotor unmanned plane and control method thereof |
| CN106394887A (en) * | 2016-10-24 | 2017-02-15 | 杭州鼎曜信息技术有限公司 | Multi-rotor-wing unmanned aerial vehicle and control method thereof |
| CN106540462A (en) * | 2016-10-17 | 2017-03-29 | 合肥齐飞信息技术有限公司 | A kind of assembly type just repaiies unmanned plane test model |
| WO2018108148A1 (en) * | 2016-12-16 | 2018-06-21 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle |
| CN108583880A (en) * | 2018-04-03 | 2018-09-28 | 芜湖纵横智能制造产业技术研究有限公司 | A kind of sensorcraft with automatic regulating function |
-
2014
- 2014-11-05 CN CN201420659368.4U patent/CN204197289U/en not_active Expired - Fee Related
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104875888B (en) * | 2015-04-13 | 2017-03-01 | 华南农业大学 | A kind of detachable annulated column formula hollow unmanned plane and its operational method |
| CN104875888A (en) * | 2015-04-13 | 2015-09-02 | 华南农业大学 | Detachable ring-pillar type hollow unmanned aerial vehicle and operation method thereof |
| CN104787327A (en) * | 2015-05-12 | 2015-07-22 | 无锡职业技术学院 | Axle distance-variable multi-rotor aircraft |
| CN105173058A (en) * | 2015-09-25 | 2015-12-23 | 联想(北京)有限公司 | Electronic equipment |
| CN105173058B (en) * | 2015-09-25 | 2017-05-24 | 联想(北京)有限公司 | Electronic equipment |
| CN105292510A (en) * | 2015-11-21 | 2016-02-03 | 长沙学院 | Multi-functional aerial photography aircraft |
| CN105292510B (en) * | 2015-11-21 | 2017-06-30 | 长沙学院 | A kind of multi-functional aerial photography aircraft |
| CN106275382A (en) * | 2016-08-10 | 2017-01-04 | 张琬彬 | A kind of unmanned plane fast assembling-disassembling wing |
| CN106275383A (en) * | 2016-08-10 | 2017-01-04 | 张琬彬 | A kind of unmanned plane wing-folding structure |
| CN106275382B (en) * | 2016-08-10 | 2018-08-17 | 深圳市盛禾无人飞机科技有限公司 | A kind of unmanned plane fast assembling-disassembling wing |
| CN106275383B (en) * | 2016-08-10 | 2019-02-26 | 深圳市盛禾农业科技有限公司 | A kind of unmanned plane wing-folding structure |
| CN106540462A (en) * | 2016-10-17 | 2017-03-29 | 合肥齐飞信息技术有限公司 | A kind of assembly type just repaiies unmanned plane test model |
| CN106394887A (en) * | 2016-10-24 | 2017-02-15 | 杭州鼎曜信息技术有限公司 | Multi-rotor-wing unmanned aerial vehicle and control method thereof |
| CN106314783A (en) * | 2016-10-24 | 2017-01-11 | 杭州鼎曜信息技术有限公司 | Anti-hurt multi-rotor unmanned plane and control method thereof |
| CN106394887B (en) * | 2016-10-24 | 2018-06-26 | 杭州鼎曜信息技术有限公司 | Multi-rotor unmanned aerial vehicle and its control method |
| CN106314783B (en) * | 2016-10-24 | 2018-09-14 | 杭州鼎曜信息技术有限公司 | Anti- hurt sb.'s feelings multi-rotor unmanned aerial vehicle and its control method |
| WO2018108148A1 (en) * | 2016-12-16 | 2018-06-21 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle |
| CN108583880A (en) * | 2018-04-03 | 2018-09-28 | 芜湖纵横智能制造产业技术研究有限公司 | A kind of sensorcraft with automatic regulating function |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150311 Termination date: 20151105 |
|
| EXPY | Termination of patent right or utility model |