CN205396522U - Unmanned aerial vehicle - Google Patents

Unmanned aerial vehicle Download PDF

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Publication number
CN205396522U
CN205396522U CN201521133161.4U CN201521133161U CN205396522U CN 205396522 U CN205396522 U CN 205396522U CN 201521133161 U CN201521133161 U CN 201521133161U CN 205396522 U CN205396522 U CN 205396522U
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CN
China
Prior art keywords
unmanned vehicle
attitude
flight controller
telescope support
housing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201521133161.4U
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Chinese (zh)
Inventor
冯川
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tianjin Touju Technology Co Ltd
Original Assignee
Tianjin Zhongke Haoyu Technology Co ltd
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Filing date
Publication date
Application filed by Tianjin Zhongke Haoyu Technology Co ltd filed Critical Tianjin Zhongke Haoyu Technology Co ltd
Priority to CN201521133161.4U priority Critical patent/CN205396522U/en
Application granted granted Critical
Publication of CN205396522U publication Critical patent/CN205396522U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to an unmanned aerial vehicle, which comprises a flight controller, an attitude sensor connected with the flight controller, a main propeller and four attitude propellers, the main propeller is coaxially connected with a main motor, the attitude propeller is coaxially connected with an attitude motor, the lower part of the unmanned aerial vehicle is provided with an installation plane, a shell for storing and transporting articles is arranged on the mounting plane, a human-computer interface input device for opening the shell is arranged on the shell, an electromagnet absorber is embedded at the bottom of the shell, a telescopic bracket is arranged at the lower part of the unmanned aerial vehicle, when the telescopic bracket is in a retraction state, the bottom end of the telescopic bracket is lower than the bottom end surface of the shell, the unmanned aerial vehicle is characterized by further comprising a GPS navigation module and an infrared ranging module, and the GPS navigation module and the infrared ranging module are connected with the flight controller. The utility model discloses can carry out the conveying of article, use like the commodity circulation express delivery, reduce the commodity circulation and passed through the trouble of manpower.

Description

A kind of unmanned vehicle
Technical field
This utility model belongs to vehicle technology field, is specifically related to a kind of unmanned vehicle.
Background technology
Along with the progress and development of technology, unmanned flight's machine or unmanned vehicle obtain quick development, are applied in the multiple environment of multiple industry, particularly to monitoring that security protection serves particularly important effect, are also used for taking photo by plane and find a view.
At logistic industry, particularly at present due to the fast development of electricity business, logistics express delivery industry obtains quick development, therefore logistics personnel often to hurry back and forth and carry out delivery in multiple places, pickup etc., very tired, especially for some remote districts or the area that has inconvenient traffic, or when traffic temporary control or interruption, normal dependence logistics courier's delivery is impossible to, and the development of unmanned plane, open for this undoubtedly and a kind of new send pickup mode, therefore, develop a kind of unmanned vehicle that can be used for logistics express delivery use, to overcome above-mentioned defect, have important practical significance.
Utility model content
The purpose of this utility model is in that to solve above-mentioned technical problem and provide a kind of and can be used for the unmanned vehicle that logistics express delivery uses.
For achieving the above object, this utility model adopts the following technical scheme that
nullA kind of unmanned vehicle,Including unmanned vehicle,Described unmanned vehicle includes flight controller、The attitude transducer being connected with flight controller、One main screw and four attitude propellers,The coaxially connected mair motor of described main screw,Described attitude propeller coaxial connects attitude motor,Described attitude motor connects described flight controller by flying governor,The bottom of described unmanned vehicle has a mounting plane,Described mounting plane is provided with the housing for article accumulating,Described housing is provided with the man machine interface input equipment for being opened by described housing,The bottom of described housing is embedded is provided with electric magnet adsorber,The bottom of described unmanned vehicle is provided with telescope support,When described telescope support is in retracted mode,The bottom of described telescope support is lower than the bottom face of described housing,Described unmanned vehicle also includes GPS navigation module and infrared distance measuring module,It is connected with described flight controller.
Described electric magnet adsorber connects power supply by relay, and described relay connects flight controller.
Described telescope support connects telescope support motor by telescoping mechanism, and described telescope support motor connects described flight controller.
The lower fuselage of described unmanned vehicle is provided with draw-in groove, and described housing is arranged on described unmanned vehicle by described draw-in groove.
The outside of described main screw and four attitude propellers is respectively equipped with elastomeric material containment vessel.
nullThis utility model is by including unmanned vehicle,Described unmanned vehicle includes flight controller、The attitude transducer being connected with flight controller、One main screw and four attitude propellers,The coaxially connected mair motor of described main screw,Described attitude propeller coaxial connects attitude motor,Described attitude motor connects described flight controller by flying governor,The bottom of described unmanned vehicle has a mounting plane,Described mounting plane is provided with the housing for article accumulating,Described housing is provided with the man machine interface input equipment for being opened by described housing,The bottom of described housing is embedded is provided with electric magnet adsorber,The bottom of described unmanned vehicle is provided with telescope support,When described telescope support is in retracted mode,The bottom of described telescope support is lower than the bottom face of described housing,Described unmanned vehicle also includes GPS navigation module and infrared distance measuring module,It is connected with described flight controller,This unmanned vehicle can be utilized to carry out the transmission of article,As logistics express delivery uses,Decrease the logistics trouble by manpower,Have great importance.
Accompanying drawing explanation
The schematic diagram of the unmanned vehicle that Fig. 1 provides for this utility model embodiment;
Fig. 2 show the principle schematic of the unmanned vehicle that this utility model embodiment provides.
Detailed description of the invention
Below, in conjunction with example, substantive distinguishing features of the present utility model and advantage are further described, but this utility model is not limited to listed embodiment.
Shown in Figure 1, figure 1 show the schematic structure of a kind of unmanned vehicle that this utility model embodiment provides.For the ease of illustrating, illustrate only the part relevant with this utility model embodiment.
nullReferring to Fig. 1、Shown in 2,A kind of unmanned vehicle,Including unmanned vehicle 1,Described unmanned vehicle includes flight controller、The attitude transducer being connected with flight controller、One main screw 2 and four attitude propellers 3,The coaxially connected mair motor of described main screw,Described attitude propeller coaxial connects attitude motor,Described attitude motor connects described flight controller by flying governor,The bottom of described unmanned vehicle has a mounting plane,Described mounting plane is provided with the housing 5 for article accumulating,Described housing is provided with the man machine interface input equipment for being opened by described housing,The bottom of described housing is embedded is provided with electric magnet adsorber 6,The bottom of described unmanned vehicle is provided with telescope support 4,When described telescope support is in retracted mode,The bottom of described telescope support is lower than the bottom face of described housing,Described unmanned vehicle also includes GPS navigation module and infrared distance measuring module,It is connected with described flight controller.
Implementing, described electric magnet adsorber connects power supply by relay, and described relay connects flight controller.
Concrete, described telescope support connects telescope support motor by telescoping mechanism, and described telescope support motor connects described flight controller.
Wherein, the lower fuselage of described unmanned vehicle is provided with draw-in groove, and described housing is arranged on described unmanned vehicle by described draw-in groove.
Further, the outside of described main screw and four attitude propellers is respectively equipped with elastomeric material containment vessel.
It should be noted that described man machine interface input equipment inputs the pickup password of acquisition in advance for user, after user inputs correct pickup password, the door of housing is opened, and user can take object away.
This utility model is adapted to multiple environment and uses, it is possible to be adsorbed on corresponding object by electric magnet, now needs to retract telescope support, it is also possible to stretch out rear support on supporting surface by telescope support, as such, it is possible to adapt to the needs of multiple environment delivery.
This utility model can be carried use by Express Logistics personnel, lets unmanned vehicle fly away arriving after certain position, delivers to appointed place to consignee or sender, pickup or put part in described housing.
nullThis utility model is by including unmanned vehicle,Described unmanned vehicle includes flight controller、The attitude transducer being connected with flight controller、One main screw and four attitude propellers,The coaxially connected mair motor of described main screw,Described attitude propeller coaxial connects attitude motor,Described attitude motor connects described flight controller by flying governor,The bottom of described unmanned vehicle has a mounting plane,Described mounting plane is provided with the housing for article accumulating,Described housing is provided with the man machine interface input equipment for being opened by described housing,The bottom of described housing is embedded is provided with electric magnet adsorber,The bottom of described unmanned vehicle is provided with telescope support,When described telescope support is in retracted mode,The bottom of described telescope support is lower than the bottom face of described housing,Described unmanned vehicle also includes GPS navigation module and infrared distance measuring module,It is connected with described flight controller,This unmanned vehicle can be utilized to carry out the transmission of article,As logistics express delivery uses,Decrease the logistics trouble by manpower,Have great importance.
The above is only preferred implementation of the present utility model; it should be pointed out that, for those skilled in the art, under the premise without departing from this utility model principle; can also making some improvements and modifications, these improvements and modifications also should be regarded as protection domain of the present utility model.

Claims (5)

  1. null1. a unmanned vehicle,It is characterized in that,Including unmanned vehicle,Described unmanned vehicle includes flight controller、The attitude transducer being connected with flight controller、One main screw and four attitude propellers,The coaxially connected mair motor of described main screw,Described attitude propeller coaxial connects attitude motor,Described attitude motor connects described flight controller by flying governor,The bottom of described unmanned vehicle has a mounting plane,Described mounting plane is provided with the housing for article accumulating,Described housing is provided with the man machine interface input equipment for being opened by described housing,The bottom of described housing is embedded is provided with electric magnet adsorber,The bottom of described unmanned vehicle is provided with telescope support,When described telescope support is in retracted mode,The bottom of described telescope support is lower than the bottom face of described housing,Described unmanned vehicle also includes GPS navigation module and infrared distance measuring module,It is connected with described flight controller.
  2. 2. unmanned vehicle according to claim 1, it is characterised in that described electric magnet adsorber connects power supply by relay, described relay connects flight controller.
  3. 3. unmanned vehicle according to claim 1 or claim 2, it is characterised in that described telescope support connects telescope support motor by telescoping mechanism, described telescope support motor connects described flight controller.
  4. 4. unmanned vehicle according to claim 3, it is characterised in that the lower fuselage of described unmanned vehicle is provided with draw-in groove, and described housing is arranged on described unmanned vehicle by described draw-in groove.
  5. 5. unmanned vehicle according to claim 1 or 4, it is characterised in that the outside of described main screw and four attitude propellers is respectively equipped with elastomeric material containment vessel.
CN201521133161.4U 2015-12-29 2015-12-29 Unmanned aerial vehicle Expired - Fee Related CN205396522U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201521133161.4U CN205396522U (en) 2015-12-29 2015-12-29 Unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201521133161.4U CN205396522U (en) 2015-12-29 2015-12-29 Unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN205396522U true CN205396522U (en) 2016-07-27

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CN (1) CN205396522U (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106314780A (en) * 2016-09-23 2017-01-11 安徽翼讯飞行安全技术有限公司 Unmanned aerial vehicle (UAV) for logistics
CN106347645A (en) * 2016-09-23 2017-01-25 安徽翼讯飞行安全技术有限公司 Unmanned aerial vehicle for distribution
CN106347652A (en) * 2016-09-23 2017-01-25 安徽翼讯飞行安全技术有限公司 UAV (Unmanned Aerial Vehicle) for aerial photographing
CN106379513A (en) * 2016-09-23 2017-02-08 安徽翼讯飞行安全技术有限公司 Unmanned aerial vehicle
CN106379512A (en) * 2016-09-23 2017-02-08 安徽翼讯飞行安全技术有限公司 Lightweight unmanned aerial vehicle
CN106477035A (en) * 2016-11-29 2017-03-08 江苏新思维信息系统工程有限公司 A kind of express mail transport unmanned plane
CN106628212A (en) * 2016-09-28 2017-05-10 哈尔滨云控机器人科技有限公司 Unmanned aerial vehicle device for installing sensor at high altitude and installing method thereof
CN107065921A (en) * 2016-10-26 2017-08-18 济南舜风科技有限公司 Method offline on inspection robot is realized using the unmanned plane with magnechuck
CN107140185A (en) * 2017-05-22 2017-09-08 程伯儒 A kind of intelligent multi-rotor unmanned aerial vehicle
CN108516084A (en) * 2018-03-30 2018-09-11 贵州大鸟创新科技有限公司 A kind of unmanned plane
CN108873044A (en) * 2018-07-05 2018-11-23 北京航空航天大学 A method of helicopter screw propeller is surveyed with respect to fuselage posture with GPS receiver
CN108945406A (en) * 2018-05-15 2018-12-07 镇江国中亿家科技有限公司 A kind of logistics distribution unmanned plane that can be positioned in real time based on Internet of Things
CN110077579A (en) * 2019-05-16 2019-08-02 唐曾美 Unmanned vehicle

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106347645A (en) * 2016-09-23 2017-01-25 安徽翼讯飞行安全技术有限公司 Unmanned aerial vehicle for distribution
CN106347652A (en) * 2016-09-23 2017-01-25 安徽翼讯飞行安全技术有限公司 UAV (Unmanned Aerial Vehicle) for aerial photographing
CN106379513A (en) * 2016-09-23 2017-02-08 安徽翼讯飞行安全技术有限公司 Unmanned aerial vehicle
CN106379512A (en) * 2016-09-23 2017-02-08 安徽翼讯飞行安全技术有限公司 Lightweight unmanned aerial vehicle
CN106314780A (en) * 2016-09-23 2017-01-11 安徽翼讯飞行安全技术有限公司 Unmanned aerial vehicle (UAV) for logistics
CN106628212A (en) * 2016-09-28 2017-05-10 哈尔滨云控机器人科技有限公司 Unmanned aerial vehicle device for installing sensor at high altitude and installing method thereof
CN107065921B (en) * 2016-10-26 2023-08-15 济南舜风科技有限公司 Method for realizing line inspection robot line-up and line-down by using unmanned aerial vehicle with electromagnetic chuck
CN107065921A (en) * 2016-10-26 2017-08-18 济南舜风科技有限公司 Method offline on inspection robot is realized using the unmanned plane with magnechuck
CN106477035A (en) * 2016-11-29 2017-03-08 江苏新思维信息系统工程有限公司 A kind of express mail transport unmanned plane
CN107140185A (en) * 2017-05-22 2017-09-08 程伯儒 A kind of intelligent multi-rotor unmanned aerial vehicle
CN108516084B (en) * 2018-03-30 2021-06-25 贵州大鸟创新科技有限公司 Unmanned aerial vehicle
CN108516084A (en) * 2018-03-30 2018-09-11 贵州大鸟创新科技有限公司 A kind of unmanned plane
CN108945406A (en) * 2018-05-15 2018-12-07 镇江国中亿家科技有限公司 A kind of logistics distribution unmanned plane that can be positioned in real time based on Internet of Things
CN108945406B (en) * 2018-05-15 2024-06-07 镇江亚夫兴农股份有限公司 Logistics distribution unmanned aerial vehicle capable of being positioned in real time based on Internet of things
CN108873044A (en) * 2018-07-05 2018-11-23 北京航空航天大学 A method of helicopter screw propeller is surveyed with respect to fuselage posture with GPS receiver
CN110077579A (en) * 2019-05-16 2019-08-02 唐曾美 Unmanned vehicle
CN110077579B (en) * 2019-05-16 2020-11-06 观典防务技术股份有限公司 Unmanned aerial vehicle

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C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20170310

Address after: 300385 the Binhai New Area of Tianjin Huayuan Industrial Zone (outer ring) six Haitai development road 3 Star Enterprise Innovation workshop No. 301 R & D Center

Patentee after: TIANJIN TOUJU TECHNOLOGY CO., LTD.

Address before: 300385 the Binhai New Area of Tianjin Huayuan Industrial Zone (outer ring) six Haitai development road 3 star enterprise No. 5- three on the eastern side of Park plant

Patentee before: TIANJIN ZHONGKE HAOYU TECHNOLOGY CO., LTD.

CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160727

Termination date: 20181229