CN106006265A - Deviation indicator for main guide wheel and liner of friction hoist - Google Patents

Deviation indicator for main guide wheel and liner of friction hoist Download PDF

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Publication number
CN106006265A
CN106006265A CN201610417973.4A CN201610417973A CN106006265A CN 106006265 A CN106006265 A CN 106006265A CN 201610417973 A CN201610417973 A CN 201610417973A CN 106006265 A CN106006265 A CN 106006265A
Authority
CN
China
Prior art keywords
module
friction
liner
running
capstan
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
CN201610417973.4A
Other languages
Chinese (zh)
Inventor
廖友民
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.)
Huainan Hongyu Industrial Products Design Co Ltd
Original Assignee
Huainan Hongyu Industrial Products Design 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 Huainan Hongyu Industrial Products Design Co Ltd filed Critical Huainan Hongyu Industrial Products Design Co Ltd
Priority to CN201610417973.4A priority Critical patent/CN106006265A/en
Publication of CN106006265A publication Critical patent/CN106006265A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66BELEVATORS; ESCALATORS OR MOVING WALKWAYS
    • B66B5/00Applications of checking, fault-correcting, or safety devices in elevators
    • B66B5/0006Monitoring devices or performance analysers
    • B66B5/0018Devices monitoring the operating condition of the elevator system
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66BELEVATORS; ESCALATORS OR MOVING WALKWAYS
    • B66B3/00Applications of devices for indicating or signalling operating conditions of elevators
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66BELEVATORS; ESCALATORS OR MOVING WALKWAYS
    • B66B5/00Applications of checking, fault-correcting, or safety devices in elevators
    • B66B5/02Applications of checking, fault-correcting, or safety devices in elevators responsive to abnormal operating conditions

Abstract

The invention discloses a deviation indicator for a main guide wheel and a liner of a friction hoist. The deviation indicator comprises a machine body (1), wherein a running induction module (2), a friction induction module (3), an indication and hinting module (4) and a management module (5) are arranged on the machine body (1); during running of the deviation indicator, the running induction module (2) is used for inducing a running condition of the machine body, the friction induction module (3) is used for inducing a friction condition between the main guide wheel and the liner, the indication and hinting module (4) is used for hinting deviation information, and the management module (5) is used for processing comprehensive information; a speed induction module (6) is arranged on the running induction module (2); a zero return setting module (7) is arranged on the indication and hinting module (4), and used for enabling deviation indication to return to zero when the machine body stops running; and a prompt module (8) is arranged on the management module (5), and used for making a prompt when friction of the machine body or abnormity of a speed is induced. According to the deviation indicator, a contact deviation condition of the main guide wheel and the liner is adjusted according to a running state of the machine body, so that smooth running is realized.

Description

Friction type winder capstan liner deviation indicator
Technical field
The present invention relates to a kind of friction type winder.
Background technology
Friction type winder is a kind of to change the heavy mechanical equipment that potential energy carries out transporting, and has that safety is high, weight of equipment is light Advantage, there is also some defects in terms of capstan liner in friction type winder operation, its contact deviation is not along with running State and adjust, operational effect may be affected.
Summary of the invention
The purpose of the present invention is that a kind of effective friction type winder capstan liner deviation indicator of offer.
The present invention is realized in.Friction type winder capstan liner deviation indicator, including a body, on body Running induction module, friction induction module, instruction signal module, management module, during operation, running induction module sensing are set The function situation of fuselage, friction induction module sensing friction condition between capstan, liner, instruction signal module signal deviation Information, manages resume module integrated information.
Friction type winder capstan liner deviation indicator, arranges velocity response module on running induction module, senses fuselage The situation of change of running speed.
Friction type winder capstan liner deviation indicator, arranges zero setting module, when fuselage stops in instruction signal module When only operating, deviation instruction zero.
Friction type winder capstan liner deviation indicator, arranges reminding module, when sensing fuselage friction in management module Or when speed has abnormal, send prompting.
Friction type winder capstan liner deviation indicator, reminding module sends the mode of prompting and is sound or LED shows.
Above-mentioned friction type winder capstan liner deviation indicator, adjusts the deviation of capstan gasket contacts according to fuselage running status Situation so that function smoothly.
Accompanying drawing explanation
Accompanying drawing is the structural representation of friction type winder capstan liner deviation indicator.
In figure, label is respectively as follows: 1-body, 2-running induction module, 3-friction induction module, 4-instruction signal module, 5-pipe Reason module, 6-velocity response module, 7-make zero setting module, 8-reminding module.
Detailed description of the invention
Embodiment: as shown in drawings.Friction type winder capstan liner deviation indicator, including a body (1), at body (1) running induction module (2), friction induction module (3), instruction signal module (4), management module (5) are set on, during operation, The function situation of running induction module (2) sensing fuselage, friction induction module (3) sensing friction condition between capstan, liner, Instruction signal module (4) signal runout information, management module (5) processes integrated information.
Friction type winder capstan liner deviation indicator, arranges velocity response module (6) in running induction module (2), sense Answer the situation of change of fuselage running speed.
Friction type winder capstan liner deviation indicator, arranges zero setting module (7) in instruction signal module (4), when When fuselage decommissions, deviation instruction zero.
Friction type winder capstan liner deviation indicator, arranges reminding module (8), when sensing machine in management module (5) When body friction or speed have abnormal, send prompting.
Friction type winder capstan liner deviation indicator, it is that sound or LED show that reminding module (8) sends the mode of prompting Show.
Above-mentioned friction type winder capstan liner deviation indicator, adjusts the deviation of capstan gasket contacts according to fuselage running status Situation so that function smoothly.

Claims (5)

1. friction type winder capstan liner deviation indicator, it is characterised in that include a body (1), set on body (1) Put running induction module (2), friction induction module (3), instruction signal module (4), management module (5), during operation, running sense Answer the function situation of module (2) sensing fuselage, friction induction module (3) sensing friction condition between capstan, liner, instruction Signal module (4) signal runout information, management module (5) processes integrated information.
Friction type winder capstan liner deviation indicator the most according to claim 1, it is characterised in that in running sensing Velocity response module (6), the situation of change of sensing fuselage running speed are set in module (2).
Friction type winder capstan liner deviation indicator the most according to claim 1, it is characterised in that in instruction signal Zero setting module (7) is set in module (4), when fuselage decommissions, deviation instruction zero.
Friction type winder capstan liner deviation indicator the most according to claim 1, it is characterised in that in management module (5) reminding module (8) is set on, when sensing that fuselage friction or speed have abnormal, sends prompting.
Friction type winder capstan liner deviation indicator the most according to claim 4, it is characterised in that reminding module (8) Send the mode of prompting and be sound or LED shows.
CN201610417973.4A 2016-06-07 2016-06-07 Deviation indicator for main guide wheel and liner of friction hoist Pending CN106006265A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610417973.4A CN106006265A (en) 2016-06-07 2016-06-07 Deviation indicator for main guide wheel and liner of friction hoist

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610417973.4A CN106006265A (en) 2016-06-07 2016-06-07 Deviation indicator for main guide wheel and liner of friction hoist

Publications (1)

Publication Number Publication Date
CN106006265A true CN106006265A (en) 2016-10-12

Family

ID=57089012

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610417973.4A Pending CN106006265A (en) 2016-06-07 2016-06-07 Deviation indicator for main guide wheel and liner of friction hoist

Country Status (1)

Country Link
CN (1) CN106006265A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1446158A (en) * 2000-08-04 2003-10-01 都恩罗普空间技术有限公司 Brake condition monitoring
CN1758265A (en) * 2004-10-08 2006-04-12 富士通株式会社 Biological information input media, authenticate device, facture and program and recording medium
CN101862528A (en) * 2010-06-17 2010-10-20 徐峰 Bicycle riding simulator
CN202481390U (en) * 2012-01-11 2012-10-10 成都蓉药集团四川长威制药有限公司 Aluminum-plastic bubble cap packaging machine
CN104340833A (en) * 2014-10-22 2015-02-11 安徽省特种设备检测院 Three-path speed synchronous-detection method for escalator/moving walk
CN204937018U (en) * 2015-08-24 2016-01-06 领航视界科技(深圳)有限公司 A kind of vehicle mounted guidance control loop

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1446158A (en) * 2000-08-04 2003-10-01 都恩罗普空间技术有限公司 Brake condition monitoring
CN1758265A (en) * 2004-10-08 2006-04-12 富士通株式会社 Biological information input media, authenticate device, facture and program and recording medium
CN101862528A (en) * 2010-06-17 2010-10-20 徐峰 Bicycle riding simulator
CN202481390U (en) * 2012-01-11 2012-10-10 成都蓉药集团四川长威制药有限公司 Aluminum-plastic bubble cap packaging machine
CN104340833A (en) * 2014-10-22 2015-02-11 安徽省特种设备检测院 Three-path speed synchronous-detection method for escalator/moving walk
CN204937018U (en) * 2015-08-24 2016-01-06 领航视界科技(深圳)有限公司 A kind of vehicle mounted guidance control loop

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20161012