CN107055417A - High-altitude operation vehicle rotary motion mechanism - Google Patents

High-altitude operation vehicle rotary motion mechanism Download PDF

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Publication number
CN107055417A
CN107055417A CN201710244186.9A CN201710244186A CN107055417A CN 107055417 A CN107055417 A CN 107055417A CN 201710244186 A CN201710244186 A CN 201710244186A CN 107055417 A CN107055417 A CN 107055417A
Authority
CN
China
Prior art keywords
conical plate
bellmouth
seat board
hole
rotary motion
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.)
Withdrawn
Application number
CN201710244186.9A
Other languages
Chinese (zh)
Inventor
孙生强
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.)
Suzhou Benchmark Intellectual Property Operation Co Ltd
Original Assignee
Suzhou Benchmark Intellectual Property Operation 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 Suzhou Benchmark Intellectual Property Operation Co Ltd filed Critical Suzhou Benchmark Intellectual Property Operation Co Ltd
Priority to CN201710244186.9A priority Critical patent/CN107055417A/en
Publication of CN107055417A publication Critical patent/CN107055417A/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F11/00Lifting devices specially adapted for particular uses not otherwise provided for
    • B66F11/04Lifting devices specially adapted for particular uses not otherwise provided for for movable platforms or cabins, e.g. on vehicles, permitting workmen to place themselves in any desired position for carrying out required operations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H57/00General details of gearing
    • F16H57/12Arrangements for adjusting or for taking-up backlash not provided for elsewhere

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structural Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Motor Power Transmission Devices (AREA)

Abstract

A kind of high-altitude operation vehicle rotary motion mechanism, it is characterized in that:Bellmouth is formed with the close Bian Kou positions of seat board, the auger port of described bellmouth is upward, one conical plate with bellmouth with identical taper is set in bellmouth, the upper plane of conical plate is higher by the upper plane of seat board, through hole is formed with conical plate, the center line of described through hole and the center line of conical plate have eccentric throw, hydraulic motor axle is fixed together through through hole with conical plate, punching is socketed on hydraulic motor in the middle of annular pressing plate, it is fixed together with bolt with seat board, and compress conical plate, installed on hydraulic motor axle and fix a little gear, described little gear is intermeshed with the tooth on revolving support outer ring, the present invention has Adjustment precision high, advantage easy to adjust and simple in construction.

Description

High-altitude operation vehicle rotary motion mechanism
Technical field
The present invention relates to high-altitude operation vehicle rotary motion mechanism, belong to high-altitude operation vehicle technical field.
Background technology
The rotary motion mechanism of high-altitude operation vehicle was assembled and run at the scene after a period of time, due to rotary reducer Foozle and abrasion between pivoting support, so as to cause both back lashes to become big, this is accomplished by revolution driving Mechanism central moment is adjusted.At present, the technology for the adjustment centre of gyration square having, what is not only adjusted is limited in scope, and The mode of adjustment is not quite reasonable, and adjustment gets up very inconvenient, and desired perfect condition can not be reached sometimes.
The content of the invention
There is provided one aiming at the drawbacks described above present in existing high-altitude operation vehicle rotary motion mechanism for the purpose of the present invention Adjustable and rational in infrastructure, the easy to adjust high-altitude operation vehicle rotary motion mechanism in gap between kind travelling gear.
High-altitude operation vehicle rotary motion mechanism of the present invention, it is mainly to include hydraulic motor(1), annular pressing plate (2), bolt first(3), seat board(4), bolt second(5), revolving support inner ring(6), base(7), bolt third(8), outside revolving support Circle(9), little gear(10), conical plate(11), by revolving support inner ring(6)With revolving support outer ring(9)The cyclotron mechanism of composition, Revolving support outer ring in cyclotron mechanism(9)Pass through bolt third(8)It is fixed on base(7)On, seat board(4)Pass through bolt second (5)It is fixedly mounted on the revolving support inner ring in cyclotron mechanism(6)On, it is characterized in that:In seat board(4)Close Bian Kou position systems There is bellmouth(12), described bellmouth(12)Center line and slew gear diameter parallel, described bellmouth(12)'s Auger port is upward, described bellmouth(12)It is interior that one and bellmouth are set(12)Conical plate with identical taper(11), Described conical plate(11)Upper plane be higher by seat board(4)Upper plane, described conical plate(11)On be formed with through hole(13), institute The through hole stated(13)Center line and conical plate(11)Center line there is eccentric throw, hydraulic motor(1)Axle passes through through hole(13) With conical plate(11)It is fixed together, annular pressing plate(2)Centre punching is socketed in hydraulic motor(1)On, use bolt first(3)With seat Plate(4)It is fixed together, and by conical plate(11)Compress, in hydraulic motor(1)Installed on axle and fix a little gear(10), institute The little gear stated(10)With revolving support outer ring(9)On tooth intermeshing.
Beneficial effect:The present invention is needing to adjust little gear(10)With revolving support outer ring(9)On tooth be intermeshed it Between gap when, only need to unclamp bolt first(3), rotation conic plate(11), then conical plate(11)On through hole(13)With revolution Support outer ring(9)Between centre-to-centre spacing change therewith, the present invention is with high, easy to adjust and simple in construction excellent of Adjustment precision Point.
Brief description of the drawings
Fig. 1 is the structure principle chart of the present invention;
Fig. 2 is the front view of conical plate;
Fig. 3 is Fig. 2 Section A-A figure.
Shown in figure:1 be hydraulic motor, 2 be annular pressing plate, 3 be bolt first, 4 be seat board, 5 be bolt second, 6 be revolution Support inner ring, 7 be base, 8 be bolt third, 9 be revolving support outer ring, 10 be little gear, 11 be conical plate, 12 be bellmouth, 13 be through hole.
Embodiment
With reference to Fig. 1, Fig. 2, Fig. 3, embodiment of the invention is:Described high-altitude operation vehicle rotary motion mechanism, It is mainly to include hydraulic motor(1), annular pressing plate(2), bolt first(3), seat board(4), bolt second(5), revolving support inner ring (6), base(7), bolt third(8), revolving support outer ring(9), little gear(10), conical plate(11), by revolving support inner ring(6) With revolving support outer ring(9)Revolving support outer ring in the cyclotron mechanism of composition, cyclotron mechanism(9)Pass through bolt third(8)Install solid It is scheduled on base(7)On, seat board(4)Pass through bolt second(5)It is fixedly mounted on the revolving support inner ring in cyclotron mechanism(6)On, its It is characterized in:In seat board(4)Close Bian Kou positions be formed with bellmouth(12), described bellmouth(12)Center line and turn-around machine The diameter parallel of structure, described bellmouth(12)Auger port upwards, described bellmouth(12)It is interior that one and taper are set Hole(12)Conical plate with identical taper(11), described conical plate(11)Upper plane be higher by seat board(4)Upper plane, institute The conical plate stated(11)On be formed with through hole(13), described through hole(13)Center line and conical plate(11)Center line have it is inclined The heart is away from hydraulic motor(1)Axle passes through through hole(13)With conical plate(11)It is fixed together, annular pressing plate(2)Centre punching socket In hydraulic motor(1)On, use bolt first(3)With seat board(4)It is fixed together, and by conical plate(11)Compress, in hydraulic motor (1)Installed on axle and fix a little gear(10), described little gear(10)With revolving support outer ring(9)On tooth mutually nibble Close.

Claims (3)

1. a kind of high-altitude operation vehicle rotary motion mechanism, it is characterized in that:In seat board(4)Close Bian Kou positions be formed with bellmouth (12), described bellmouth(12)Center line and slew gear diameter parallel, described bellmouth(12)Auger port Upwards, described bellmouth(12)It is interior that one and bellmouth are set(12)Conical plate with identical taper(11), described cone Shape plate(11)Upper plane be higher by seat board(4)Upper plane.
2. according to claim 1, a kind of described high-altitude operation vehicle rotary motion mechanism, it is characterized in that:Described conical plate (11)On be formed with through hole(13), described through hole(13)Center line and conical plate(11)Center line there is eccentric throw.
3. according to claim 1, a kind of described high-altitude operation vehicle rotary motion mechanism, it is characterized in that:Hydraulic motor(1)Axle is worn Cross through hole(13)With conical plate(11)It is fixed together, annular pressing plate(2)Centre punching is socketed in hydraulic motor(1)On, use spiral shell Bolt first(3)With seat board(4)It is fixed together, and by conical plate(11)Compress.
CN201710244186.9A 2017-04-14 2017-04-14 High-altitude operation vehicle rotary motion mechanism Withdrawn CN107055417A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710244186.9A CN107055417A (en) 2017-04-14 2017-04-14 High-altitude operation vehicle rotary motion mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710244186.9A CN107055417A (en) 2017-04-14 2017-04-14 High-altitude operation vehicle rotary motion mechanism

Publications (1)

Publication Number Publication Date
CN107055417A true CN107055417A (en) 2017-08-18

Family

ID=59601276

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710244186.9A Withdrawn CN107055417A (en) 2017-04-14 2017-04-14 High-altitude operation vehicle rotary motion mechanism

Country Status (1)

Country Link
CN (1) CN107055417A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20200230809A1 (en) * 2019-01-23 2020-07-23 Fanuc Corporation Robot joint structure and robot with backlash reduction mechanism
CN113915318A (en) * 2021-10-29 2022-01-11 伯朗特机器人股份有限公司 Industrial robot center distance adjusting method
CN113997318A (en) * 2021-10-29 2022-02-01 伯朗特机器人股份有限公司 Center distance adjusting ring of industrial robot

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201021710Y (en) * 2006-11-21 2008-02-13 徐州工程机械科技股份有限公司 Installation base for center distance adjustable turning deceleration machine
CN201934626U (en) * 2010-12-17 2011-08-17 徐州海伦哲专用车辆股份有限公司 Rotary speed reduction device with adjustable central moment
CN202790120U (en) * 2012-09-27 2013-03-13 中联重科股份有限公司 Slewing bearing and slewing device for engineering machinery
CN204985673U (en) * 2015-09-29 2016-01-20 湖北江南专用特种汽车有限公司 But driven adjusting device is supported in gyration of high altitude construction car
CN206692287U (en) * 2017-04-14 2017-12-01 苏州标杆知识产权运营有限公司 High-altitude operation vehicle rotary motion mechanism

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201021710Y (en) * 2006-11-21 2008-02-13 徐州工程机械科技股份有限公司 Installation base for center distance adjustable turning deceleration machine
CN201934626U (en) * 2010-12-17 2011-08-17 徐州海伦哲专用车辆股份有限公司 Rotary speed reduction device with adjustable central moment
CN202790120U (en) * 2012-09-27 2013-03-13 中联重科股份有限公司 Slewing bearing and slewing device for engineering machinery
CN204985673U (en) * 2015-09-29 2016-01-20 湖北江南专用特种汽车有限公司 But driven adjusting device is supported in gyration of high altitude construction car
CN206692287U (en) * 2017-04-14 2017-12-01 苏州标杆知识产权运营有限公司 High-altitude operation vehicle rotary motion mechanism

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20200230809A1 (en) * 2019-01-23 2020-07-23 Fanuc Corporation Robot joint structure and robot with backlash reduction mechanism
CN113915318A (en) * 2021-10-29 2022-01-11 伯朗特机器人股份有限公司 Industrial robot center distance adjusting method
CN113997318A (en) * 2021-10-29 2022-02-01 伯朗特机器人股份有限公司 Center distance adjusting ring of industrial robot

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SE01 Entry into force of request for substantive examination
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WW01 Invention patent application withdrawn after publication

Application publication date: 20170818

WW01 Invention patent application withdrawn after publication