CN206807217U - It is a kind of can 660 degree rotation unmanned plane horizontal stage electric machine devices - Google Patents

It is a kind of can 660 degree rotation unmanned plane horizontal stage electric machine devices Download PDF

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Publication number
CN206807217U
CN206807217U CN201720639278.2U CN201720639278U CN206807217U CN 206807217 U CN206807217 U CN 206807217U CN 201720639278 U CN201720639278 U CN 201720639278U CN 206807217 U CN206807217 U CN 206807217U
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CN
China
Prior art keywords
unmanned plane
electric machine
motor
ring
driven torus
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
CN201720639278.2U
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Chinese (zh)
Inventor
刘伟
田伟程
车嘉兴
刘畅
张春雨
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.)
Shenzhen Micromulticopter Aero Technology Co Ltd
Original Assignee
Shenzhen Micromulticopter Aero 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 Shenzhen Micromulticopter Aero Technology Co Ltd filed Critical Shenzhen Micromulticopter Aero Technology Co Ltd
Priority to CN201720639278.2U priority Critical patent/CN206807217U/en
Application granted granted Critical
Publication of CN206807217U publication Critical patent/CN206807217U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses it is a kind of can 660 degree rotation unmanned plane horizontal stage electric machine devices, the peripheral hardware being installed on including electric machine structure and the bidirectionally limited structure of concentric ring on unmanned machine head, concentric ring portion is by driven torus and the bidirectionally limited structure of active ring, rotated by active ring, so as to cause driven torus to rotate, spacing stopping finally being occurred by driven torus and rotor, so as to reach motor can 660 degree rotation, unmanned machine head Multi-orientation multi-angle rotation is realized, solves the functional defect caused by the problems such as angle or time.The utility model, which solves traditional unmanned plane motor, can not realize more than 360 degree Rotations, it ensure that unmanned machine head advantageously realizes that no dead angle is captured in time in real work, observed without dead angle, situations such as fixed point location, broken traditional unmanned machine head runs into dead angle position at work simultaneously, unmanned plane during flying position and angle bottom need to be readjusted, is shortened working hours, improves operating efficiency.

Description

It is a kind of can 660 degree rotation unmanned plane horizontal stage electric machine devices
Technical field
The utility model is related to unmanned plane field, and in particular to it is a kind of can 660 degree rotation unmanned plane horizontal stage electric machine devices.
Background technology
It is increasing the scene such as using unmanned plane fixed point shooting to be carried out now, jettisoning, observe, rescuing, simultaneously because market Upper many unmanned plane horizontal stage electric machine devices are operated operation, while many unmanned machine head operations in less than 360 degree angles Because angle limitation causes to frequently occur adjustment fuselage positions and angle during operation, to bringing great not convenient property in work, Also influence simultaneously in unmanned plane during flying task, waste the energy, can not accurately complete the execution of aerial mission;
Many unmanned machine head carries using conventional motors device work when, no matter pinpoint candids photograph, observe or jettisoning, Rescue etc., because the angle limitation of motor result in the not convenient property of operation, generally by adjusting flying height, position, angle Deng, to realize work requirements, to unmanned plane during flying operation bring greatly it is not convenient with test, while give unmanned plane during flying supply The energy also brings test.
Other unmanned plane electric machines are mostly using simple unidirectional spacing, so as to cause the anglec of rotation inadequate, work In there is dead angle, bring limitation to aerial mission.
The content of the invention
Technical problem to be solved in the utility model is to provide one kind and solves unmanned machine head and can not smoothly have in time The completion aerial mission problem of effect, it is ensured that will not be made because of under the conditions of the energy, time, skilled operation degree, angle, position etc. Into work can not timely performance, while broken the inadequate situation of traditional horizontal stage electric machine anglec of rotation, also solved Unmanned plane during flying task is more effective, it is more intelligent, be more quickly completed.
The utility model is achieved through the following technical solutions:It is a kind of can 660 degree rotation unmanned plane horizontal stage electric machines Device, including electric machine structure are installed on the peripheral hardware on unmanned machine head with the bidirectionally limited structure of concentric ring, and the peripheral hardware includes motor Part and concentric ring part, motor part include stator and rotor, nebenkern part include driven torus and active ring group into pair To position limiting structure, rotated by active ring, drive driven torus rotation.
As preferable technical scheme, the motor part is mainly comprising motor stator and two parts of rotor, Liang Zhetong Magnetic cylinder, iron core, bearing, rotating shaft, pad, magnet ring set, clip spring structure are crossed, and utilizes brushless electric machine operation principle, increase rotor is determined To spacing, realize that motor can 660 or less than 360 degree angle spinfunctions.
It is in pairs to position limiting structure from driven torus and active ring group as preferable technical scheme, rotated by active ring, so as to Cause driven torus to rotate, spacing stopping finally being occurred by driven torus and rotor, can 660 degree of rotations so as to reach motor.
The beneficial effects of the utility model are:The utility model solves traditional unmanned plane motor and can not realized more than 360 Spend Rotation, it is ensured that unmanned machine head advantageously realizes that no dead angle is captured in time in real work, and no dead angle observation is fixed Situations such as point location, while broken traditional unmanned machine head and run into dead angle position at work, unmanned plane need to be readjusted Flight position and angle bottom, shorten working hours, and improve operating efficiency.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is overall structure diagram of the present utility model;
Fig. 2 is internal structure schematic diagram of the present utility model;
Fig. 3 is operation principle schematic diagram of the present utility model.
Embodiment
All features disclosed in this specification, or disclosed all methods or during the step of, except mutually exclusive Feature and/or step beyond, can combine in any way.
Any feature disclosed in this specification (including any accessory claim, summary and accompanying drawing), except non-specifically chatting State, can alternative features equivalent by other or with similar purpose replaced.I.e., unless specifically stated otherwise, each feature It is an example in a series of equivalent or similar characteristics.
As shown in figure 1, the peripheral hardware on unmanned machine head is installed on including electric machine structure and the bidirectionally limited structure of concentric ring, should Peripheral hardware includes motor part 1 and concentric ring part 2, and motor part 1 includes the structure such as stator 5 and rotor 6, nebenkern part by Driven torus 4 and 3 bidirectionally limited structure of active ring.
As shown in Fig. 2 electric machine structure part, mainly comprising motor stator and two parts of rotor, both pass through magnetic cylinder, iron Core, bearing, rotating shaft, pad, magnet ring set, jump ring etc., using brushless electric machine operation principle, increase rotor orientation is spacing, realizes electricity Machine can 660 or more than 360 degree angle spinfunctions;The bidirectionally limited structure division driven torus of the concentric ring, active ring, copper sheathing Deng composition.
Wherein, concentric ring is caused to rotate by motor rotation, finally by spacing stopping occurs with rotor, so as to reach electricity Machine can be more than 360 degree of rotations, realize that unmanned 660 degree of machine head rotates without dead angle.
As shown in figure 3, concentric ring portion driven torus is illustrated with the rotation of active ring, rotated by active ring, it is driven so as to cause Ring rotates, and spacing stopping finally occurring by driven torus and rotor, so as to reach motor can 660 degree rotate, realize unmanned plane Head Multi-orientation multi-angle rotates,.
After wherein active ring drives 330 degree of rotation by motor stator, and driven torus is spacing contacts and drive driven torus to rotate, After rotating 330 degree again, driven torus is contacted and stopped the rotation with rotor spacing place, synchronous according to need of work, rotation Angle can be reset to original state, carry out repeated multiple times rotation, complete unmanned plane during flying mission requirements.
Operation principle:After rotating 330 degree for main rotating ring, then 330 degree of driven torus rotation is driven, and rotor is spacing contacts And stop operating, starting reset by task demand turns to initial position, reaches aerial mission demand.
The beneficial effects of the utility model are:
(1) motor multi-angle rotary direction can be passed through, it is ensured that various visual angles, multi-faceted behaviour in unmanned plane during flying task Make, simplify operating process, improve operating efficiency;
(2) nothing can also be saved by motor multi-angle rotary direction simultaneously in various visual angles with multi-faceted convenient operation The waste of the man-machine energy, extend the unmanned plane during flying time;
(3) due to simplifying operation, with the raising of operating efficiency, the service life of unmanned plane motor is also carried It is high;
(4) at the same in unmanned plane during flying task carry out fixed point shooting, jettisoning, observe, rescue etc. scene provide it is higher Precision.
It is described above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to In this, any change or replacement expected without creative work, should all cover within the scope of protection of the utility model. Therefore, the scope of protection of the utility model should be determined by the scope of protection defined in the claims.

Claims (3)

1. it is a kind of can 660 degree rotation unmanned plane horizontal stage electric machine devices, it is characterised in that:It is two-way with concentric ring including electric machine structure Position limiting structure is installed on the peripheral hardware on unmanned machine head, and the peripheral hardware includes motor part and concentric ring part, and motor part includes Stator and rotor, nebenkern part include driven torus and active ring group into bidirectionally limited structure, rotated by active ring, drive from Rotating ring rotates.
2. as claimed in claim 1 can 660 degree rotation unmanned plane horizontal stage electric machine devices, it is characterised in that:The motor section It is divided to mainly comprising motor stator and two parts of rotor, both pass through magnetic cylinder, iron core, bearing, rotating shaft, pad, magnet ring set, jump ring Structure, and utilize brushless electric machine operation principle, increase rotor orientation is spacing, realize motor can 660 or less than 360 degree angles revolve Rotating function.
3. as claimed in claim 1 can 660 degree rotation unmanned plane horizontal stage electric machine devices, it is characterised in that:By driven torus with Active ring group is in pairs to position limiting structure, is rotated by active ring, so as to cause driven torus to rotate, finally by driven torus and rotor The spacing stopping of generation, can 660 degree of rotations so as to reach motor.
CN201720639278.2U 2017-06-05 2017-06-05 It is a kind of can 660 degree rotation unmanned plane horizontal stage electric machine devices Expired - Fee Related CN206807217U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720639278.2U CN206807217U (en) 2017-06-05 2017-06-05 It is a kind of can 660 degree rotation unmanned plane horizontal stage electric machine devices

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720639278.2U CN206807217U (en) 2017-06-05 2017-06-05 It is a kind of can 660 degree rotation unmanned plane horizontal stage electric machine devices

Publications (1)

Publication Number Publication Date
CN206807217U true CN206807217U (en) 2017-12-26

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107947429A (en) * 2017-12-29 2018-04-20 中山市盟拓机电有限公司 A kind of plastic cement holds the position limiting structure of horizontal stage electric machine
CN108462300A (en) * 2018-02-08 2018-08-28 深圳市固胜智能科技有限公司 The position-limit mechanism of motor and motor applied to holder
CN112204944A (en) * 2019-08-13 2021-01-08 深圳市大疆创新科技有限公司 Shooting detection method, device, holder, system and storage medium

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107947429A (en) * 2017-12-29 2018-04-20 中山市盟拓机电有限公司 A kind of plastic cement holds the position limiting structure of horizontal stage electric machine
CN107947429B (en) * 2017-12-29 2024-01-12 桂林飞宇科技股份有限公司 Limit structure of plastic handheld cradle head motor
CN108462300A (en) * 2018-02-08 2018-08-28 深圳市固胜智能科技有限公司 The position-limit mechanism of motor and motor applied to holder
CN112204944A (en) * 2019-08-13 2021-01-08 深圳市大疆创新科技有限公司 Shooting detection method, device, holder, system and storage medium
CN112204944B (en) * 2019-08-13 2021-10-15 深圳市大疆创新科技有限公司 Shooting detection method, device, holder, system and storage medium

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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: 20171226