CN106239541A - A kind of light-duty paw of unmanned plane - Google Patents

A kind of light-duty paw of unmanned plane Download PDF

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Publication number
CN106239541A
CN106239541A CN201610835260.XA CN201610835260A CN106239541A CN 106239541 A CN106239541 A CN 106239541A CN 201610835260 A CN201610835260 A CN 201610835260A CN 106239541 A CN106239541 A CN 106239541A
Authority
CN
China
Prior art keywords
paw
duty
slide block
unmanned plane
light
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
CN201610835260.XA
Other languages
Chinese (zh)
Inventor
恽为民
张栋梁
庞作伟
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.)
Shanghai Xpartner Robotics Co Ltd
Original Assignee
Shanghai Xpartner Robotics 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 Shanghai Xpartner Robotics Co Ltd filed Critical Shanghai Xpartner Robotics Co Ltd
Priority to CN201610835260.XA priority Critical patent/CN106239541A/en
Publication of CN106239541A publication Critical patent/CN106239541A/en
Priority to PCT/CN2017/079514 priority patent/WO2018054033A1/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25JMANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J15/00Gripping heads and other end effectors
    • B25J15/0009Gripping heads and other end effectors comprising multi-articulated fingers, e.g. resembling a human hand
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25JMANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J15/00Gripping heads and other end effectors
    • B25J15/02Gripping heads and other end effectors servo-actuated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25JMANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J15/00Gripping heads and other end effectors
    • B25J15/08Gripping heads and other end effectors having finger members
    • B25J15/10Gripping heads and other end effectors having finger members with three or more finger members

Abstract

A kind of light-duty paw of unmanned plane, including: the driving motor of fixed frame, fixed and arranged to fixed frame, the multiple internal drive gears being arranged on fixed frame, connection fixed frame and multiple screw mandrels of each internal drive gear, multiple slide block, multiple paw arm and the multiple fixing nut being fixed on each slide block;Wherein, slide block is can be arranged on corresponding screw mandrel in the way of sliding on corresponding screw mandrel, and drives motor by driving internal drive gear so that each slide block slides on corresponding screw mandrel;Paw arm has closing fluting;And each fixing nut is each passed through corresponding closing and slots and be fixed on each slide block so that each paw arm can move via the slip in each self-enclosed fluting of each slide block.The unmanned plane light-duty paw portable construction of the present invention, chucking power is stable, and paw has auto-lock function, and current of electric closed loop control chucking power algorithm is simple, and Control system architecture is succinct, installs adaptability good.

Description

A kind of light-duty paw of unmanned plane
Technical field
The present invention relates to unmanned plane field, particularly relate to a kind of light-duty paw of unmanned plane.
Background technology
Currently, unmanned plane is installed paw to go to perform the development trend that relevant task is technology application.Due to unmanned plane Payload limited, paw prescription is light and handy, to have certain chucking power to capturing thing, requires that paw is for capturing simultaneously The profile of object has good adaptability, can be from main regulation grasp force.
Conventional unmanned plane retaining paw all uses steering wheel gear or steering wheel pull rope structural principle, cannot to chucking power Continual and steady holding, motor rotation blockage overlong time, easy motor damage.Specifically, the product of current unmanned plane paw is few, Common structure has two kinds: one to be light-duty steering wheel and gear clamping device composition;Two is to use cable winding machine and tightrope mechanism.Above-mentioned Although structure meets light and handy demand, but, chucking power is unstable, the easy stall of motor.
Therefore, those skilled in the art is devoted to develop a kind of portable construction and the stable light-duty hands of unmanned plane of chucking power Pawl.
Summary of the invention
Because the drawbacks described above of prior art, the technical problem to be solved be to provide a kind of portable construction and The light-duty paw of unmanned plane that chucking power is stable.
For achieving the above object, the invention provides a kind of light-duty paw of unmanned plane, including: fixed frame, fixed and arranged To described fixed frame drive motor, the multiple internal drive gears being arranged on described fixed frame, connect described fixing Framework and multiple screw mandrels of each internal drive gear, multiple slide block, multiple paw arm and be fixed on each slide block many Individual fixing nut;Wherein, described slide block can be arranged on corresponding screw mandrel in the way of sliding on corresponding screw mandrel, and Described driving motor is by driving internal drive gear so that each slide block slides on corresponding screw mandrel;Described paw arm has There is closing fluting;And each fixing nut is each passed through corresponding closing and slots and be fixed on each slide block so that each Paw arm can move via the slip in each self-enclosed fluting of each slide block.
Preferably, the light-duty paw of described unmanned plane also includes: the multiple paw arms being fixedly connected on described fixed frame Support, and each each paw arm is connected to corresponding paw arm support respectively in precalculated position so that and each paw arm can To rotate around described precalculated position via the slip in each self-enclosed fluting of each slide block.
Preferably, in the light-duty paw of described unmanned plane, described fixed frame is circular fixed frame.
Preferably, in the light-duty paw of described unmanned plane, the quantity of the plurality of paw arm is four.
Preferably, in the light-duty paw of described unmanned plane, when slide block slides into relatively closer to the position of fixed frame, The light-duty paw of unmanned plane is in contraction state according to the preferred embodiment of the invention.
Preferably, in the light-duty paw of described unmanned plane, when slide block slides into the position being relatively farther from fixed frame, The light-duty paw of unmanned plane is in open configuration according to the preferred embodiment of the invention.
Preferably, in the light-duty paw of described unmanned plane, described driving motor uses current of electric closed loop to control clamping Power.
The unmanned plane light-duty paw portable construction of the present invention, chucking power is stable, and paw has auto-lock function, current of electric Closed loop control chucking power algorithm is simple, and Control system architecture is succinct, installs adaptability good.
Below with reference to accompanying drawing, the technique effect of design, concrete structure and the generation of the present invention is described further, with It is fully understood from the purpose of the present invention, feature and effect.
Accompanying drawing explanation
Fig. 1 is the light-duty paw of unmanned plane overall three-dimensional signal in a contracted state according to the preferred embodiment of the invention Figure.
Fig. 2 is the light-duty paw of unmanned plane overall three-dimensional signal under open configuration according to the preferred embodiment of the invention Figure.
Fig. 3 is the kind of drive sketch of the light-duty paw of unmanned plane according to the preferred embodiment of the invention.
Fig. 4 is the drive system partial schematic diagram of the light-duty paw of unmanned plane according to the preferred embodiment of the invention.
It should be noted that accompanying drawing is used for illustrating the present invention, and the unrestricted present invention.Note, represent that the accompanying drawing of structure can Can be not necessarily drawn to scale.Further, in accompanying drawing, same or like element indicates same or like label.
Detailed description of the invention
In the present invention, a kind of light-duty paw of new unmanned plane uses and refers to method of clamping more, and especially four refer to method of clamping, By motor output many (four) individual rotating in same direction, drive four feed screw nut machines, by the mobile drive finger of nut Opening and closing.
The detailed description of the invention of the present invention is described below in conjunction with accompanying drawing.
Fig. 1 is the light-duty paw of unmanned plane overall three-dimensional signal in a contracted state according to the preferred embodiment of the invention Figure, and Fig. 2 is the light-duty paw of unmanned plane overall schematic perspective view under open configuration according to the preferred embodiment of the invention, And Fig. 3 is the kind of drive sketch of the light-duty paw of unmanned plane according to the preferred embodiment of the invention, and Fig. 4 is excellent according to the present invention Select the drive system partial schematic diagram of the light-duty paw of unmanned plane of embodiment.
As shown in Figure 1, Figure 2, Figure 3 and Figure 4, the light-duty paw of unmanned plane includes according to the preferred embodiment of the invention: fixing Framework 100, fixed and arranged to described fixed frame 100 drive motor 10, be arranged on described fixed frame 100 multiple in Portion's travelling gear 20, connect described fixed frame 100 and multiple screw mandrels 30 of each internal drive gear 20, multiple slide block 40, Multiple paw arms 50 and the multiple fixing nut 60 being fixed on each slide block 40.
Wherein, described slide block 40 can be arranged on corresponding screw mandrel 30 in the way of sliding on corresponding screw mandrel 30, And described driving motor 10 is by driving internal drive gear 20 so that each slide block 40 slides on corresponding screw mandrel 30; Described paw arm 50 has closing fluting 51;And each fixing nut 60 is each passed through corresponding closing fluting 51 and is fixed on On each slide block 40 so that each paw arm 50 can be transported via the slip in each self-enclosed fluting 51 of each slide block 40 Dynamic.
Wherein, such as, described driving motor 10 uses current of electric closed loop to control chucking power.
Preferably, described fixed frame 100 is circular fixed frame.
Such as, when slide block slides into relatively closer to the position of fixed frame 100, according to the preferred embodiment of the invention At the light-duty paw of unmanned plane in a contracted state;When slide block slides into the position being relatively farther from fixed frame 100, according to this The light-duty paw of unmanned plane of invention preferred embodiment is under open configuration.
Preferably, as shown in Figure 1, Figure 2 and Figure 3, the light-duty paw of unmanned plane also includes according to the preferred embodiment of the invention: The multiple paw arm supports 70 being fixedly connected on described fixed frame 100, and each each paw arm 50 is respectively predetermined Position 80 is connected to corresponding paw arm support 70.Thus, each paw arm 50 can be via each slide block 40 each self-enclosed Fluting 51 in slip and rotate around described precalculated position 80.
Preferably, the quantity of the plurality of paw arm 50 is four.The situation of four paw arms make grasping stable and Structure can be simplified simultaneously,
The unmanned plane light-duty paw portable construction of the present invention, chucking power is stable, and paw has auto-lock function, current of electric Closed loop control chucking power algorithm is simple, and Control system architecture is succinct, installs adaptability good.
Described above illustrate and describes the preferred embodiments of the present invention, as previously mentioned, it should be understood that the present invention not office Be limited to form disclosed herein, be not to be taken as the eliminating to other embodiments, and can be used for other combinations various, amendment and Environment, and can be changed by above-mentioned teaching or the technology of association area or knowledge in invention contemplated scope described herein Dynamic.And the change that those skilled in the art are carried out and change are without departing from the spirit and scope of the present invention, the most all should be appended by the present invention In scope of the claims.

Claims (7)

1. the light-duty paw of unmanned plane, it is characterised in that including: the driving of fixed frame, fixed and arranged to described fixed frame Motor, the multiple internal drive gears being arranged on described fixed frame, connect described fixed frame and each internal drive tooth Multiple screw mandrels of wheel, multiple slide block, multiple paw arm and the multiple fixing nut being fixed on each slide block;Wherein, described Slide block is can be arranged on corresponding screw mandrel in the way of sliding on corresponding screw mandrel, and described driving motor is by driving Internal drive gear is so that each slide block slides on corresponding screw mandrel;Described paw arm has closing fluting;And each Fixing nut is each passed through corresponding closing and slots and be fixed on each slide block so that each paw arm can be sliding via each Block slip in each self-enclosed fluting and move.
2. the light-duty paw of unmanned plane as claimed in claim 1, it is characterised in that also include: be fixedly connected on described fixed frame On multiple paw arm supports, and each each paw arm is connected to corresponding paw arm support respectively in precalculated position, makes Obtain each paw arm to rotate around described precalculated position via the slip in each self-enclosed fluting of each slide block.
3. the light-duty paw of unmanned plane as claimed in claim 1 or 2, it is characterised in that described fixed frame is circular fixed frame Frame.
4. the light-duty paw of unmanned plane as claimed in claim 1 or 2, it is characterised in that the quantity of the plurality of paw arm is four Individual.
5. the light-duty paw of unmanned plane as claimed in claim 1 or 2, it is characterised in that when slide block slides into relatively closer to solid When determining the position of framework, the light-duty paw of unmanned plane is in contraction state according to the preferred embodiment of the invention.
6. the light-duty paw of unmanned plane as claimed in claim 1 or 2, it is characterised in that be relatively farther from admittedly when slide block slides into When determining the position of framework, the light-duty paw of unmanned plane is in open configuration according to the preferred embodiment of the invention.
7. the light-duty paw of unmanned plane as claimed in claim 1 or 2, it is characterised in that described driving motor uses current of electric Closed loop controls chucking power.
CN201610835260.XA 2016-09-20 2016-09-20 A kind of light-duty paw of unmanned plane Pending CN106239541A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201610835260.XA CN106239541A (en) 2016-09-20 2016-09-20 A kind of light-duty paw of unmanned plane
PCT/CN2017/079514 WO2018054033A1 (en) 2016-09-20 2017-04-06 Unmanned aerial vehicle light gripper

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610835260.XA CN106239541A (en) 2016-09-20 2016-09-20 A kind of light-duty paw of unmanned plane

Publications (1)

Publication Number Publication Date
CN106239541A true CN106239541A (en) 2016-12-21

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CN (1) CN106239541A (en)
WO (1) WO2018054033A1 (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106864766A (en) * 2017-03-16 2017-06-20 山东大学 It is applied to unmanned plane independently the battery clamp device of continuation of the journey and replacing device and method
CN107053226A (en) * 2017-02-12 2017-08-18 上海云线娃娃信息科技有限公司 It is a kind of to clamp and hold up simultaneously the manipulator of article
CN107813335A (en) * 2017-12-01 2018-03-20 揭阳市腾晟科技咨询有限公司 A kind of anti abrasive manipulator
WO2018054033A1 (en) * 2016-09-20 2018-03-29 上海未来伙伴机器人有限公司 Unmanned aerial vehicle light gripper
CN109625258A (en) * 2019-01-26 2019-04-16 哈尔滨学院 A kind of Multi-axis aircraft
CN110342249A (en) * 2019-08-13 2019-10-18 广西科技大学 A kind of arm end executing agency of high-precise synchronization crawl
CN110921497A (en) * 2019-12-06 2020-03-27 界首市天瓴建筑工程有限公司 Heavy object snatchs mechanism for building
CN110994458A (en) * 2019-12-21 2020-04-10 陕西同力智慧能源服务有限公司 Bird's nest extirpation instrument for electric power engineering
CN112830239A (en) * 2021-02-04 2021-05-25 北京鸿霁科技有限公司 Grabbing device and packaging machine with same

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CN110053967A (en) * 2019-05-23 2019-07-26 沈阳吕尚科技有限公司 A kind of intelligent cleft hand under the environment for nuclear pollution
CN110202601A (en) * 2019-05-23 2019-09-06 江苏精正自动化科技有限公司 The novel mini multi-functional electronic claw of version
CN110181498B (en) * 2019-05-31 2023-06-23 西安工业大学 Underwater execution arm and execution method thereof
CN110253606B (en) * 2019-07-10 2022-03-25 重庆大学 Soft tongs of imitative paper folding structure
CN111390953B (en) * 2020-03-23 2022-12-23 上海大学 Enveloping type under-actuated robot paw
CN111958625B (en) * 2020-08-27 2022-11-15 上海大学 Self-adaptive multi-connecting-rod type three-jaw picking manipulator
CN112157666B (en) * 2020-09-01 2022-08-05 南京信息职业技术学院 Multi-claw synchronous gathering paw
CN113581473A (en) * 2021-08-04 2021-11-02 桂林航天工业学院 Unmanned aerial vehicle with gripper
CN113697372B (en) * 2021-09-06 2023-03-31 合肥奥博特自动化设备有限公司 Ore raw material transportation anti-blocking device
CN114081546B (en) * 2022-01-24 2022-04-15 河南工学院 Board pincers with adjustable clamping jaw and application of board pincers to livestock veterinarian bloodletting needle

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CN206367013U (en) * 2016-09-20 2017-08-01 上海未来伙伴机器人有限公司 A kind of light-duty paw of unmanned plane

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CN206367013U (en) * 2016-09-20 2017-08-01 上海未来伙伴机器人有限公司 A kind of light-duty paw of unmanned plane

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Publication number Priority date Publication date Assignee Title
WO2018054033A1 (en) * 2016-09-20 2018-03-29 上海未来伙伴机器人有限公司 Unmanned aerial vehicle light gripper
CN107053226A (en) * 2017-02-12 2017-08-18 上海云线娃娃信息科技有限公司 It is a kind of to clamp and hold up simultaneously the manipulator of article
CN107053226B (en) * 2017-02-12 2023-11-17 玉沣科技(西安)有限公司 Manipulator capable of simultaneously clamping and supporting articles
CN106864766A (en) * 2017-03-16 2017-06-20 山东大学 It is applied to unmanned plane independently the battery clamp device of continuation of the journey and replacing device and method
CN106864766B (en) * 2017-03-16 2019-09-03 山东大学 The battery clamp device and replacement device and method independently continued a journey applied to unmanned plane
CN107813335A (en) * 2017-12-01 2018-03-20 揭阳市腾晟科技咨询有限公司 A kind of anti abrasive manipulator
CN109625258A (en) * 2019-01-26 2019-04-16 哈尔滨学院 A kind of Multi-axis aircraft
CN110342249A (en) * 2019-08-13 2019-10-18 广西科技大学 A kind of arm end executing agency of high-precise synchronization crawl
CN110921497A (en) * 2019-12-06 2020-03-27 界首市天瓴建筑工程有限公司 Heavy object snatchs mechanism for building
CN110921497B (en) * 2019-12-06 2021-11-30 合肥托卡拉图科技有限公司 Heavy object snatchs mechanism for building
CN110994458A (en) * 2019-12-21 2020-04-10 陕西同力智慧能源服务有限公司 Bird's nest extirpation instrument for electric power engineering
CN112830239A (en) * 2021-02-04 2021-05-25 北京鸿霁科技有限公司 Grabbing device and packaging machine with same

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