CN105065477A - Radial disassembly coupling - Google Patents

Radial disassembly coupling Download PDF

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Publication number
CN105065477A
CN105065477A CN201510478995.7A CN201510478995A CN105065477A CN 105065477 A CN105065477 A CN 105065477A CN 201510478995 A CN201510478995 A CN 201510478995A CN 105065477 A CN105065477 A CN 105065477A
Authority
CN
China
Prior art keywords
overcoat
transfer panel
coupling
shaft
transfer disc
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
CN201510478995.7A
Other languages
Chinese (zh)
Inventor
闫泽
王学志
罗萌
张祥
盛贵宾
王春玲
魏君波
宋成军
丁春华
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.)
703th Research Institute of CSIC
Original Assignee
703th Research Institute of CSIC
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 703th Research Institute of CSIC filed Critical 703th Research Institute of CSIC
Priority to CN201510478995.7A priority Critical patent/CN105065477A/en
Publication of CN105065477A publication Critical patent/CN105065477A/en
Pending legal-status Critical Current

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Abstract

The invention proposes a radial disassembly coupling. A motor output shaft is connected with a transfer disc through a film coupling; the transfer disc and a middle shaft are connected through an outer sleeve; the transfer disc is contacted with a plane of the middle shaft; the outer circle parts of the transfer disc contacted with the plane of the middle shaft are symmetric conical ring surfaces; the outer sides of the two symmetric conical ring surfaces fit and are connected with inner conical ring surfaces at the two sides of the outer sleeve; the tops and the bottoms of the conical ring surfaces at the two sides of the outer sleeve are not contacted with the outer circles of the transfer disc and the middle shaft; the outer sleeve is a two-half structure, and is tightly connected through four bolts; the other end of the middle shaft and the two-half structure are connected with another transfer disc through the outer sleeve; the transfer disc extends into a test box to connect a jigger input shaft through a film coupling; and the film coupling and the jigger input shaft are connected through a locking expansion sleeve. The radial disassembly coupling is small in volume, light in weight, simple in machining and few in connecting bolts. The radial disassembly coupling is disassembled radially and is convenient for installation and disassembly.

Description

A kind of radial dismounting couplers
technical field:
The present invention relates to the engaging experimental bench field of barring gear, specifically a kind of radial dismounting couplers.
background technique:
Barring gear will carry out running adaptation before dispatching from the factory, when using conventional coupling to build pilot system, not bringing extraneous vibration when rotating for making each axle system, will look for middle work to each coupling in transmission system, this link cost manpower is many, the time is long.And after test, by barring gear remove while, the position of test motor and test chamber all will change, destroy adjusted look for middle work, like this when installing the barring gear of next same model, require a great deal of time again and repeat to look for middle work, meanwhile, when using conventional coupling, normally dismantle flange plate or diaphragm coupling, each dismounting all will be dismantled dozens of bolt, and these all substantially prolongs the test period, reduce working efficiency.
summary of the invention:
In order to shorten the cycle of the running-in of mass barring gear and the test of this type, increasing work efficiency, the invention provides a kind of radial dismounting couplers.
Technological scheme of the present invention is: a kind of radial dismounting couplers, comprise motor output shaft, motor output shaft connects transfer panel by diaphragm coupling, transfer panel is connected by overcoat with jack shaft, transfer panel contacts with neutral axis plane, the cylindrical position symmetrically cone torus that transfer panel contacts with neutral axis plane, be connected with the female cone anchor ring of the both sides of overcoat outside these two symmetrical cone torus, the top of the both sides cone torus of overcoat does not all contact with jack shaft cylindrical with transfer panel with bottom, overcoat is two halves structure, be fastenedly connected by four bolts, the other end structure same as described above of jack shaft connects another transfer panel by overcoat, this transfer panel stretches in test chamber and connects jiggering input shaft by diaphragm coupling, be connected by locking expansion set between this diaphragm coupling with jiggering input shaft.
Described overcoat is two halves structure, and after the overcoat of two halves is fastenedly connected, the end face between two halves does not contact.
The present invention has following beneficial effect: volume is little, lightweight, processing simple, attachment bolt is few and dismantled by radial direction, easy installation and removal.
accompanying drawing illustrates:
Fig. 1 sectional view of the present invention;
Accompanying drawing 2 stereogram of the present invention.
1-overcoat in figure, 2-jack shaft, 3-transfer panel, 4-motor output shaft, 5-diaphragm coupling, 6-locks expansion set, 7-jiggering input shaft, 8-test chamber.
embodiment:
Below in conjunction with accompanying drawing, the invention will be further described:
Shown in Fig. 1 composition graphs 2, a kind of radial dismounting couplers, comprise motor output shaft 4, motor output shaft 4 connects transfer panel 3 by diaphragm coupling 5, transfer panel 3 is connected by overcoat 1 with jack shaft 2, transfer panel 3 and jack shaft 1 plane contact, the cylindrical position symmetrically cone torus of transfer panel 3 and jack shaft 2 plane contact, be connected with the female cone anchor ring of the both sides of overcoat 1 outside these two symmetrical cone torus, the top of the both sides cone torus of overcoat 1 does not all contact with jack shaft 2 cylindrical with transfer panel 3 with bottom, overcoat 1 is two halves structure, be fastenedly connected by four bolts, the other end structure same as described above of jack shaft 2 connects another transfer panel 3 by overcoat 1, this transfer panel 3 stretches in test chamber 8 and connects jiggering input shaft 7 by diaphragm coupling 5, be connected by locking expansion set 6 between this diaphragm coupling 5 with jiggering input shaft 7.
Described overcoat 1 is two halves structure, and after the overcoat 1 of two halves is fastenedly connected, the end face between two halves does not contact.
This coupling is divided into overcoat 1, jack shaft 2 and transfer panel 3 three parts, these three parts pass through cone match, under the effect of cover locking bolt tension force outside, the conical surface that the conical surface that the plane that transfer panel 3 coordinates with jack shaft 2, transfer panel 3 coordinate with overcoat 1, overcoat 1 coordinate with jack shaft 2 three surface of contact fluid-tight engagement, produce enough large frictional force to transmit motor and be input to moment of torsion in barring gear, meet power requirements, during Cone fit can be looked for automatically simultaneously, coupling self coaxality is better, can meet rotating accuracy requirement.
The present invention is compared with common coupling, and convenient disassembly, can shorten the test period, increase work efficiency, and its reason is as follows:
When using common coupling, after barring gear running adaptation terminates, when dismantling barring gear, because each connection place all has seam to locate, dismantle if want wherein certain a part, motor or test chamber 8 is just needed to move axially a segment distance, enable axially have certain space to be shifted out by the seam of certain end flange dish, just can pull down each several part component axially connected, like this while dismounting barring gear, just destroy the position of motor or the test chamber adjusted, when the barring gear of same model is installed again, need again to repeat loaded down with trivial details to look for middle work, simultaneously, the attachment bolt of common coupling circumferencial direction is more, the more time is all needed when dismounting and installation.
When using coupling of the present invention, when dismantling barring gear, only lock bolt need be unclamped, to dismantle overcoat 1, due to when mounted, in order to the axial thermal expansion of supplementary axle system, radial dismounting couplers two ends normally tension, when dismantling overcoat 1, axially just can produce very little space, due between jack shaft 2 with transfer panel 3 for plane coordinates, without seam, axially there is short space, just can take out jack shaft 2 by radial direction, after jack shaft 2 takes out, axially just there are enough spaces, so just can when not needing to move axially oriented motor and test chamber 8, remove the component that other axially connect, so the connection of the barring gear of next same model looks for middle work without the need to repeating again.Meanwhile, the attachment bolt of radial dismounting couplers only has 8, saves time during installation and removal.

Claims (2)

1. a radial dismounting couplers, comprise motor output shaft (4), it is characterized in that: motor output shaft (4) connects transfer panel (3) by diaphragm coupling (5), transfer panel (3) is connected by overcoat (1) with jack shaft (2), transfer panel (3) and jack shaft (1) plane contact, the cylindrical position symmetrically cone torus of transfer panel (3) and jack shaft (2) plane contact, be connected with the female cone anchor ring of the both sides of overcoat (1) outside these two symmetrical cone torus, the top of the both sides cone torus of overcoat (1) does not all contact with jack shaft (2) cylindrical with transfer panel (3) with bottom, overcoat (1) is two halves structure, be fastenedly connected by four bolts, the other end structure same as described above of jack shaft (2) connects another transfer panel (3) by overcoat (1), this transfer panel (3) stretches in test chamber (8) and connects jiggering input shaft (7) by diaphragm coupling (5), be connected by locking expansion set (6) between this diaphragm coupling (5) with jiggering input shaft (7).
2. the radial dismounting couplers of one according to claim 1, is characterized in that: described overcoat (1) is two halves structure, and after the overcoat (1) of two halves is fastenedly connected, the end face between two halves does not contact.
CN201510478995.7A 2015-08-07 2015-08-07 Radial disassembly coupling Pending CN105065477A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510478995.7A CN105065477A (en) 2015-08-07 2015-08-07 Radial disassembly coupling

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510478995.7A CN105065477A (en) 2015-08-07 2015-08-07 Radial disassembly coupling

Publications (1)

Publication Number Publication Date
CN105065477A true CN105065477A (en) 2015-11-18

Family

ID=54494946

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510478995.7A Pending CN105065477A (en) 2015-08-07 2015-08-07 Radial disassembly coupling

Country Status (1)

Country Link
CN (1) CN105065477A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109268480A (en) * 2018-11-21 2019-01-25 东莞市卓蓝自动化设备有限公司 A kind of hollow rotating platform
CN114087294A (en) * 2021-11-25 2022-02-25 苏州茗祥机械科技有限公司 Flange unit and prevent flange structure of bolt bite

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR722912A (en) * 1930-10-07 1932-03-30 Improvements to establishing adjustable couplings
CN1044156A (en) * 1989-01-09 1990-07-25 T·J·冈拉克机械公司 coupling
CN201236898Y (en) * 2008-08-14 2009-05-13 无锡创明传动工程有限公司 Diaphragm coupling with low additional bending moment
CN103527650A (en) * 2013-10-29 2014-01-22 中国船舶重工集团公司第七�三研究所 Quick mounting and dismounting coupling
CN204852046U (en) * 2015-08-07 2015-12-09 中国船舶重工集团公司第七�三研究所 Radially dismantle shaft coupling

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR722912A (en) * 1930-10-07 1932-03-30 Improvements to establishing adjustable couplings
CN1044156A (en) * 1989-01-09 1990-07-25 T·J·冈拉克机械公司 coupling
CN201236898Y (en) * 2008-08-14 2009-05-13 无锡创明传动工程有限公司 Diaphragm coupling with low additional bending moment
CN103527650A (en) * 2013-10-29 2014-01-22 中国船舶重工集团公司第七�三研究所 Quick mounting and dismounting coupling
CN204852046U (en) * 2015-08-07 2015-12-09 中国船舶重工集团公司第七�三研究所 Radially dismantle shaft coupling

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109268480A (en) * 2018-11-21 2019-01-25 东莞市卓蓝自动化设备有限公司 A kind of hollow rotating platform
CN114087294A (en) * 2021-11-25 2022-02-25 苏州茗祥机械科技有限公司 Flange unit and prevent flange structure of bolt bite

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
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Application publication date: 20151118