CN105314110A - Unmanned aerial vehicle with umbrella - Google Patents

Unmanned aerial vehicle with umbrella Download PDF

Info

Publication number
CN105314110A
CN105314110A CN201510728615.0A CN201510728615A CN105314110A CN 105314110 A CN105314110 A CN 105314110A CN 201510728615 A CN201510728615 A CN 201510728615A CN 105314110 A CN105314110 A CN 105314110A
Authority
CN
China
Prior art keywords
umbrella
unmanned plane
fuselage
contiguous block
aerial vehicle
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.)
Pending
Application number
CN201510728615.0A
Other languages
Chinese (zh)
Inventor
周成
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.)
JIAXING YAOU OPTOELECTRONICS TECHNOLOGY Co Ltd
Original Assignee
JIAXING YAOU OPTOELECTRONICS TECHNOLOGY Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by JIAXING YAOU OPTOELECTRONICS TECHNOLOGY Co Ltd filed Critical JIAXING YAOU OPTOELECTRONICS TECHNOLOGY Co Ltd
Priority to CN201510728615.0A priority Critical patent/CN105314110A/en
Publication of CN105314110A publication Critical patent/CN105314110A/en
Pending legal-status Critical Current

Links

Classifications

    • AHUMAN NECESSITIES
    • A45HAND OR TRAVELLING ARTICLES
    • A45BWALKING STICKS; UMBRELLAS; LADIES' OR LIKE FANS
    • A45B25/00Details of umbrellas
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10Wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00Launching, take-off or landing arrangements
    • B64U70/80Vertical take-off or landing, e.g. using rockets
    • B64U70/83Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
    • AHUMAN NECESSITIES
    • A45HAND OR TRAVELLING ARTICLES
    • A45BWALKING STICKS; UMBRELLAS; LADIES' OR LIKE FANS
    • A45B25/00Details of umbrellas
    • A45B2025/003Accessories not covered by groups A45B25/24 - A45B25/30
    • AHUMAN NECESSITIES
    • A45HAND OR TRAVELLING ARTICLES
    • A45BWALKING STICKS; UMBRELLAS; LADIES' OR LIKE FANS
    • A45B2200/00Details not otherwise provided for in A45B
    • A45B2200/10Umbrellas; Sunshades
    • A45B2200/1009Umbrellas; Sunshades combined with other objects
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • B64U10/13Flying platforms
    • B64U10/14Flying platforms with four distinct rotor axes, e.g. quadcopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Walking Sticks, Umbrellas, And Fans (AREA)

Abstract

The invention relates to an unmanned aerial vehicle with an umbrella. The unmanned aerial vehicle comprises an unmanned aerial vehicle body and the umbrella, wherein the unmanned aerial vehicle body comprises a fuselage; four wings and four feet are arranged on the fuselage; a propeller and a driving motor are arranged on each wing, and each driving motor drives the corresponding propeller to rotate so as to realize ascending, descending and turning of the unmanned aerial vehicle; a connecting block is arranged on the fuselage in an outwardly raised manner relative to the fuselage; the umbrella comprises an umbrella cover and a bracket for supporting the umbrella cover; through a connecting part, the umbrella is mounted on the connecting block of the fuselage. Through the umbrella, the balance of the unmanned aerial vehicle during flying is ensured, and a crash condition caused by out of control of the unmanned aerial vehicle is avoided; meanwhile, the unmanned aerial vehicle is suitable for being used in a rainy environment; in addition, characteristics of the unmanned aerial vehicle body are fully utilized, the umbrella plays the common umbrella function in air, and the unmanned aerial vehicle body and the umbrella cooperate with each other, so that use requirements of people can be met.

Description

A kind of unmanned plane carrying umbrella
Technical field
The present invention relates to a kind of unmanned plane, be specifically related to a kind of unmanned plane carrying umbrella.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Without driving compartment on machine, but the equipment such as autopilot, process controller, information collecting device are installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, it is followed the tracks of, locates, remote control, remote measurement and digital communication.Can take off as conventional airplane under radio telecommand or launch with booster rocket, also can be taken to by machine tool and throw in flight in the air.
Wherein, remotely pilotless machine in use, specifically can be controlled the flight of unmanned plane, and utilize the flight of unmanned plane by remote controller.It according to the demand used, unmanned plane can assemble other carrier, such as, carry the unmanned plane of camera or illuminating lamp carrier, can utilize unmanned plane can on high in the feature of flight, carry out the corresponding function of specific implementation.
At present, its flight of existing unmanned plane is generally specifically controlled by the screw propeller on this unmanned plane, be appreciated that, its build of unmanned plane is general less, and correspondingly, the screw propeller that correspondence is assembled on this unmanned plane is less, its on high in the process of flight as run into the weather of strong wind and heavy rain time, it is difficult to, control, even can cause the out of control of this unmanned plane, thus cause the air crash situation of unmanned plane for unmanned plane during flying balance; Meanwhile, unmanned plane is essentially plastics electrical structure part, and it is not suitable for using in the rain.
Summary of the invention
The object of this invention is to provide a kind of unmanned plane carrying umbrella for solving the problems of the technologies described above.
A kind of unmanned plane carrying umbrella provided by the present invention, comprises
Unmanned plane, described unmanned plane comprises fuselage, be located at 4 wings on fuselage and under-chassis, wherein each wing is provided with screw propeller and drive motor separately, and drive screw propeller to rotate by drive motor, to realize the rising of unmanned plane, decline and turning, described fuselage is provided with contiguous block, and described contiguous block outwards protrudes out setting relative to fuselage;
Umbrella, described umbrella comprises umbrella cover and the bracket for supporting umbrella cover, and is assembled on the contiguous block of fuselage by this umbrella by attaching parts.
As preferred version of the present invention, described contiguous block is arranged on described fuselage away from a side end face of under-chassis; Described umbrella is provided with connection projection at umbrella cover on the side end face deviating from bracket, and with attaching parts by this contiguous block be connected projection and be connected and fixed.
As preferred version of the present invention, described contiguous block is arranged on described fuselage away from a side end face of wing; Described umbrella deviates from a side end face of bracket at umbrella cover and is provided with connection projection, and with attaching parts by this contiguous block be connected projection and be connected and fixed.
As preferred version of the present invention, the both sides end face of described fuselage is respectively arranged with contiguous block; Described umbrella is provided with connection projection respectively in the both side ends of umbrella cover.
As preferred version of the present invention, described attaching parts comprises connecting rod, two groups of screw bolt and nut, and a side end of described connecting rod is plugged on the connection projection of umbrella, and end side is plugged in the contiguous block of fuselage, and each personal screw bolt and nut is connected and fixed.
As preferred version of the present invention, described contiguous block is arranged on the position at described body nodal point place; Described connection projection is arranged on the middle part of described umbrella cover.
As preferred version of the present invention, 4 described wings are symmetrical arranged between two relative to fuselage.
As preferred version of the present invention, described fuselage is provided with 2 under-chassis, and described 2 under-chassis are relative to fuselage Central Symmetry.
As preferred version of the present invention, described unmanned plane comprises power supply further, the signal transducer arranged with screw propeller one_to_one corresponding, and controller; Described power supply is used for powering to described drive motor, signal transducer; Described controller carrys out the rotation of corresponding control drive motor by signal transducer.
As preferred version of the present invention, described controller is arranged relative to unmanned plane split.
Due to the utilization of technique scheme, the present invention compared with prior art has following advantages:
The unmanned plane carrying umbrella provided by the present invention, by rational structure, it carries umbrella by unmanned plane, this unmanned plane is made to carry out in the process of flying, the behavior of structure of umbrella can be utilized to carry out choke to unmanned plane keep off the rain, ensure that balance during this unmanned plane during flying, in order to avoid there is the situation of air crash because of the out of control of unmanned plane; Also make this unmanned plane be suitable for using in the environment of rainy day simultaneously; In addition, unmanned plane assembles umbrella, it also can the characteristic of abundant unmanned plane, and umbrella is carried to the effect playing umbrella self in the air, both complement each other, and meet the user demand of people.
Accompanying drawing explanation
The structural representation carrying the unmanned plane of umbrella that Fig. 1 provides for present pre-ferred embodiments.
Detailed description of the invention
For making the object, technical solutions and advantages of the present invention clearly understand, below in conjunction with detailed description of the invention also with reference to accompanying drawing, the present invention is described in more detail.Should be appreciated that, these describe just exemplary, and do not really want to limit the scope of the invention.In addition, in the following description, the description to known features and technology is eliminated, to avoid unnecessarily obscuring concept of the present invention.
Refer to Fig. 1, the unmanned plane 100 of what present pre-ferred embodiments provided carry umbrella, the umbrella 20 comprising unmanned plane 10 and be located on this unmanned plane 10.
Described unmanned plane 10 comprises fuselage 11,4 wings 12, under-chassis 13, power supply (not shown), signal transducer (not shown) and the controller 14 be located on this fuselage 11.Be appreciated that controller 14 is that split is arranged relative to this unmanned plane 10, described power supply is for powering to drive motor, signal transducer, and the power supply by arranging in this controller 14 during the power supply of controller 14 realizes.Further, 4 described wings 12 are symmetrical arranged between two relative to fuselage 11, described fuselage 11 are provided with 2 under-chassis 13, and described 2 under-chassis 13 are relative to fuselage 11 Central Symmetry.
In the present embodiment, each wing 12 comprises respectively screw propeller 121 and drive motor (not shown), each drive motor correspondence controls corresponding screw propeller 121, and drive screw propeller 121 to rotate by drive motor, to realize the rising of this unmanned plane 10, decline and turning, that is realize the flight of this unmanned plane 10.Be appreciated that, in the unmanned plane 100 of the present embodiment, signal transducer and screw propeller 121 are that one_to_one corresponding is arranged, when such people carry out operation control to this unmanned plane 10, signal can be sent to signal transducer by controller 14, and carry out corresponding conversion by the signal of signal transducer through receiving and flow to drive motor, realize control to drive motor rotating speed, and then achieve this controller 14 and control driving this unmanned plane 10 to carry out to fly the screw propeller 121 controlled.
Described umbrella 20 comprises umbrella cover 21, and for supporting the bracket (not shown) of umbrella cover 21, be appreciated that, use to realize this umbrella 20 to be assembled on unmanned plane 10, it there are certain requirements umbrella cover 21 tool of umbrella 20, particularly, requires that the weight of this umbrella 20 entirety is little as much as possible on the one hand, when this umbrella 20 being assembled on unmanned plane 10 to alleviate, to unmanned plane 10 load pressure; On the other hand, the umbrella cover 21 of this umbrella 20 its compare the performance that common umbrella has the anti-rain of better wind resistance, and unmanned plane 10 carries this umbrella 20 when using, and it better can guide wind, to strengthen the balance quality of unmanned plane 10 in flight course further.So the umbrella 20 of the present embodiment, in the process of concrete selection, can pay the utmost attention to the material of above requirement, such as with bracket prepared by titanium alloy material, the umbrella cover 21 having nano material to make.
In order to realize the assembling of this unmanned plane 10 and umbrella 20, the present embodiment arranges contiguous block 111 on the fuselage 11 of unmanned plane 10, and described contiguous block 111 outwards protrudes out setting relative to fuselage 11.Correspondingly, the umbrella cover 21 of described umbrella 20 is provided with and connects projection 211, and with the concrete assembling that attaching parts comes between specific implementation unmanned plane 10 and umbrella 20 to contiguous block 111 and the connection being connected projection 211.Further, described attaching parts comprises connecting rod 31, two groups of bolts 32 and nut 33, one side end of described connecting rod 31 is plugged on the connection projection 211 of umbrella 20, and end side is plugged in the contiguous block 111 of fuselage 11, and each personal bolt 32 and nut 33 are connected and fixed.Further, described contiguous block 111 is specifically arranged on the position at the center of gravity place of fuselage 11, and described connection projection 211 is also specifically arranged on the middle part of described umbrella cover 21.
Being appreciated that the demand according to using, this umbrella 20 specifically can being assembled to the top of unmanned plane 10, also this umbrella 20 can being assembled to the below of unmanned plane 10.
Particularly, first kind of way: when only needing this umbrella 20 to be assembled to the top of unmanned plane 10, described contiguous block 111 is arranged on described fuselage 11 away from a side end face of under-chassis 13; Correspondingly, described umbrella 20 is provided with at umbrella cover 21 and connects projection 211 on the side end face deviating from bracket, and with attaching parts by this contiguous block 111 be connected projection 211 and carry out being connected and fixed realizing.The second way: when only needing this umbrella 20 to be assembled to the below of unmanned plane 10, described contiguous block 111 is arranged on described fuselage 11 away from a side end face of wing 12; Correspondingly, described umbrella 20 connects projection 211 at umbrella cover 21 being provided with on a side end face of bracket, and with attaching parts by this contiguous block 111 be connected projection 211 and carry out being connected and fixed realizing.The third mode: when both this umbrella 20 being assembled to the top of unmanned plane 10, when also can be assembled to the below of unmanned plane 10, the both sides end face of described fuselage 11 is respectively arranged with contiguous block 111; Described umbrella 20 is provided with respectively in the both side ends of umbrella cover 21 and connects projection 211, at the present embodiment, preferably selects the third mode.
In sum, the unmanned plane carrying umbrella provided by the present invention, by rational structure, it carries umbrella by unmanned plane, this unmanned plane is made to carry out in the process of flying, the behavior of structure of umbrella can be utilized to carry out choke to unmanned plane keep off the rain, ensure that balance during this unmanned plane during flying, in order to avoid there is the situation of air crash because of the out of control of unmanned plane; Also make this unmanned plane be suitable for using in the environment of rainy day simultaneously; In addition, unmanned plane assembles umbrella, it also can the characteristic of abundant unmanned plane, and umbrella is carried to the effect playing umbrella self in the air, both complement each other, and meet the user demand of people.
The foregoing is only preferred embodiment of the present invention, be not limited to the present invention, within the spirit and principles in the present invention all, any amendment made, equivalent replacement, improvement etc., all should be included within the scope of protection of the invention.

Claims (10)

1. carry a unmanned plane for umbrella, it is characterized in that: comprise
Unmanned plane, described unmanned plane comprises fuselage, be located at 4 wings on fuselage and under-chassis, wherein each wing is provided with screw propeller and drive motor separately, and drive screw propeller to rotate by drive motor, to realize the rising of unmanned plane, decline and turning, described fuselage is provided with contiguous block, and described contiguous block outwards protrudes out setting relative to fuselage;
Umbrella, described umbrella comprises umbrella cover and the bracket for supporting umbrella cover, and is assembled on the contiguous block of fuselage by this umbrella by attaching parts.
2. the unmanned plane carrying umbrella according to claim 1, is characterized in that: described contiguous block is arranged on described fuselage away from a side end face of under-chassis; Described umbrella is provided with connection projection at umbrella cover on the side end face deviating from bracket, and with attaching parts by this contiguous block be connected projection and be connected and fixed.
3. the unmanned plane carrying umbrella according to claim 1, is characterized in that: described contiguous block is arranged on described fuselage away from a side end face of wing; Described umbrella deviates from a side end face of bracket at umbrella cover and is provided with connection projection, and with attaching parts by this contiguous block be connected projection and be connected and fixed.
4. the unmanned plane carrying umbrella according to claim 1, is characterized in that: the both sides end face of described fuselage is respectively arranged with contiguous block; Described umbrella is provided with connection projection respectively in the both side ends of umbrella cover.
5. the unmanned plane carrying umbrella according to claim 2,3 or 4, it is characterized in that: described attaching parts comprises connecting rod, two groups of screw bolt and nut, one side end of described connecting rod is plugged on the connection projection of umbrella, end side is plugged in the contiguous block of fuselage, and each personal screw bolt and nut is connected and fixed.
6. the unmanned plane carrying umbrella according to claim 5, is characterized in that: described contiguous block is arranged on the position at described body nodal point place; Described connection projection is arranged on the middle part of described umbrella cover.
7. the unmanned plane carrying umbrella according to claim 1, is characterized in that: 4 described wings are symmetrical arranged between two relative to fuselage.
8. the unmanned plane carrying umbrella according to claim 1, is characterized in that: described fuselage is provided with 2 under-chassis, and described 2 under-chassis are relative to fuselage Central Symmetry.
9. the unmanned plane carrying umbrella according to claim 1, is characterized in that: described unmanned plane comprises power supply further, the signal transducer arranged with screw propeller one_to_one corresponding, and controller; Described power supply is used for powering to described drive motor, signal transducer; Described controller carrys out the rotation of corresponding control drive motor by signal transducer.
10. the unmanned plane carrying umbrella according to claim 9, is characterized in that: described controller is arranged relative to unmanned plane split.
CN201510728615.0A 2015-10-30 2015-10-30 Unmanned aerial vehicle with umbrella Pending CN105314110A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510728615.0A CN105314110A (en) 2015-10-30 2015-10-30 Unmanned aerial vehicle with umbrella

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510728615.0A CN105314110A (en) 2015-10-30 2015-10-30 Unmanned aerial vehicle with umbrella

Publications (1)

Publication Number Publication Date
CN105314110A true CN105314110A (en) 2016-02-10

Family

ID=55242611

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510728615.0A Pending CN105314110A (en) 2015-10-30 2015-10-30 Unmanned aerial vehicle with umbrella

Country Status (1)

Country Link
CN (1) CN105314110A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107415837A (en) * 2017-06-15 2017-12-01 浙江吉利控股集团有限公司 Vehicle-mounted unmanned aerial vehicle and the automatic system and method that opens an umbrella
CN107627827A (en) * 2017-09-11 2018-01-26 太仓史瑞克工业设计有限公司 A kind of intelligent shading system and its control method based on automobile
CN107776880A (en) * 2016-08-25 2018-03-09 酷波(厦门)进出口有限公司 Has the unmanned vehicle of shielding cell
CN108181918A (en) * 2018-01-05 2018-06-19 华侨大学 A kind of mobile aerial sunshade flies paulin and its implementation
CN108445915A (en) * 2018-02-28 2018-08-24 深圳臻迪信息技术有限公司 Flight control method and device
CN108741491A (en) * 2018-07-15 2018-11-06 王伟 A kind of umbrella
CN108974358A (en) * 2018-06-15 2018-12-11 黄佩媛 A kind of automatic intelligent traction unmanned plane
EP3422895A4 (en) * 2016-03-02 2019-07-31 Lazo-Antunez, Raynel Automated hands-free umbrella
CN112173106A (en) * 2020-09-27 2021-01-05 华南理工大学 Unmanned aerial vehicle umbrella
CN115184087A (en) * 2022-07-05 2022-10-14 南京邮电大学 Unmanned aerial vehicle sampling device for water quality testing

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102756804A (en) * 2011-03-29 2012-10-31 郑鹏 Method for performing fly-lifting rescue in mountain ravine and off-road ambulance
CN202828097U (en) * 2012-09-05 2013-03-27 郴州市成城金属有限公司 Rotorcraft engine compartment
CN104527974A (en) * 2015-01-09 2015-04-22 金陵科技学院 Rotary wing type rain-proof unmanned aerial vehicle
CN204279940U (en) * 2014-11-05 2015-04-22 成都盛世普益科技有限公司 A kind of many rotor wing unmanned aerial vehicles device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102756804A (en) * 2011-03-29 2012-10-31 郑鹏 Method for performing fly-lifting rescue in mountain ravine and off-road ambulance
CN202828097U (en) * 2012-09-05 2013-03-27 郴州市成城金属有限公司 Rotorcraft engine compartment
CN204279940U (en) * 2014-11-05 2015-04-22 成都盛世普益科技有限公司 A kind of many rotor wing unmanned aerial vehicles device
CN104527974A (en) * 2015-01-09 2015-04-22 金陵科技学院 Rotary wing type rain-proof unmanned aerial vehicle

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3422895A4 (en) * 2016-03-02 2019-07-31 Lazo-Antunez, Raynel Automated hands-free umbrella
CN107776880A (en) * 2016-08-25 2018-03-09 酷波(厦门)进出口有限公司 Has the unmanned vehicle of shielding cell
CN107415837A (en) * 2017-06-15 2017-12-01 浙江吉利控股集团有限公司 Vehicle-mounted unmanned aerial vehicle and the automatic system and method that opens an umbrella
US11361655B2 (en) 2017-06-15 2022-06-14 Zhejiang Geely Holding Group Co., Ltd. Unmanned aerial vehicle (UAV) and method and system for holding umbrella using UAV
EP3609743A4 (en) * 2017-06-15 2020-05-06 Zhejiang Geely Holding Group Co., Ltd. Unmanned aerial vehicle (uav) and method and system for holding umbrella using uav
CN107415837B (en) * 2017-06-15 2019-10-25 浙江吉利控股集团有限公司 Vehicle-mounted unmanned aerial vehicle, open an umbrella system and the control method that opens an umbrella automatically automatically
CN107627827A (en) * 2017-09-11 2018-01-26 太仓史瑞克工业设计有限公司 A kind of intelligent shading system and its control method based on automobile
CN108181918A (en) * 2018-01-05 2018-06-19 华侨大学 A kind of mobile aerial sunshade flies paulin and its implementation
CN108445915B (en) * 2018-02-28 2021-09-14 深圳臻迪信息技术有限公司 Flight control method and device
CN108445915A (en) * 2018-02-28 2018-08-24 深圳臻迪信息技术有限公司 Flight control method and device
CN108974358A (en) * 2018-06-15 2018-12-11 黄佩媛 A kind of automatic intelligent traction unmanned plane
CN108974358B (en) * 2018-06-15 2020-12-25 安徽省冠腾信息科技有限公司 Automatic change intelligence and pull unmanned aerial vehicle
CN108741491A (en) * 2018-07-15 2018-11-06 王伟 A kind of umbrella
CN112173106A (en) * 2020-09-27 2021-01-05 华南理工大学 Unmanned aerial vehicle umbrella
CN115184087A (en) * 2022-07-05 2022-10-14 南京邮电大学 Unmanned aerial vehicle sampling device for water quality testing

Similar Documents

Publication Publication Date Title
CN105314110A (en) Unmanned aerial vehicle with umbrella
CN106143898B (en) A kind of VTOL tilting rotor fixed wing aircraft
CN203996886U (en) A kind of four axle eight oars aircraft of taking photo by plane
CN104843181A (en) Petrol-electric hybrid power fixed wing vertical take-off and landing unmanned plane system
CN103979104B (en) One can variant X-type wing vertical landing minute vehicle
CN203528816U (en) Aerial photo unmanned plane
CN105799923A (en) Four-rotor aircraft-based carrying manipulator
CN203318686U (en) Aerial photography cloud deck for aeromodelling aircraft
CN204527630U (en) A kind of oil electric mixed dynamic fixed-wing VUAV system
CN205574270U (en) Delivery manipulator based on four rotor crafts
CN205022853U (en) Many rotors flight equipment
CN103171763A (en) Novel unmanned plane
CN107161329A (en) A kind of restructural amphibious robot
CN204078068U (en) A kind of four-axle aircraft of overlength flying power
CN205022913U (en) Carry image signal collection system's flight equipment
CN205186530U (en) Carry unmanned aerial vehicle of umbrella
CN110775268A (en) Unmanned aerial vehicle aircraft
CN203268313U (en) Novel unmanned aerial vehicle
CN107458593A (en) A kind of duct propulsion system based on multi-rotor unmanned aerial vehicle
CN205216194U (en) But fixed -wing aircraft of VTOL
CN106965921A (en) Fixed-wing and the integral unmanned aerial vehicle of many rotors
CN206954510U (en) It is a kind of can VTOL fixed-wing unmanned plane
CN203666982U (en) Multi-propeller aircraft on mooring platform
CN213768958U (en) Vertical take-off and landing fixed wing unmanned aerial vehicle
CN205131661U (en) Novel adherence unmanned aerial vehicle device

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20160210