CN202073947U - Long-shaft type elastic coupling with multi-diaphragm structure - Google Patents

Long-shaft type elastic coupling with multi-diaphragm structure Download PDF

Info

Publication number
CN202073947U
CN202073947U CN2011201736739U CN201120173673U CN202073947U CN 202073947 U CN202073947 U CN 202073947U CN 2011201736739 U CN2011201736739 U CN 2011201736739U CN 201120173673 U CN201120173673 U CN 201120173673U CN 202073947 U CN202073947 U CN 202073947U
Authority
CN
China
Prior art keywords
diaphragm
inner pressure
pressure ring
diaphragms
group
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
CN2011201736739U
Other languages
Chinese (zh)
Inventor
张攀
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.)
WUXI VULKAN TECHNOLOGY CO LTD
Original Assignee
WUXI VULKAN 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 WUXI VULKAN TECHNOLOGY CO LTD filed Critical WUXI VULKAN TECHNOLOGY CO LTD
Priority to CN2011201736739U priority Critical patent/CN202073947U/en
Application granted granted Critical
Publication of CN202073947U publication Critical patent/CN202073947U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Measuring Fluid Pressure (AREA)

Abstract

The utility model disclose a long-shaft type elastic coupling with a multi-diaphragm structure, which comprises a left flange, a right flange, an intermediate shaft, diaphragm assemblies, a diaphragm seat, intermediate rings arranged at two sides of the intermediate shaft, a first inner pressure ring and a second inner pressure ring. Diaphragms in the diaphragm assemblies are in the circular shape, a group of diaphragm assemblies are respectively positioned between the left flange and the first inner pressure ring and between the right flange and the first inner pressure ring, another group of diaphragm assemblies are respectively arranged between two ends of the intermediate shaft and the second inner pressure rings at two ends. Two end faces of the intermediate rings arranged at two sides of the intermediate shaft are respectively connected with two groups of diaphragm assemblies and the diaphragm seat through first bolts. The diaphragms are changed into the circular structure and provided with four groups of diaphragm assemblies, and each group of diaphragm assembly is only provided with two diaphragms. Inner ring bolt holes of diaphragms are connected with the inner pressure rings, and outer ring bolt holes are connected with the diaphragm seat, thereby greatly improving axial, radial and angular displacement compensation capacity of the coupling, reducing alignment accuracy of necessary adjustment in installation, reducing the work amount, guaranteeing actual status of the diaphragms can be conveniently observed from the outside of the coupling and facilitating daily observation and maintenance of the diaphragms.

Description

A kind of elastic coupling flexible coupling of major axis type multimembrane chip architecture
Technical field
The utility model relates to a kind of elastic coupling flexible coupling of major axis type multimembrane chip architecture, belongs to big-and-middle-sized power transmission system technical field.
Background technique
In big-and-middle-sized power transmission system, in Ship Power Equipment axle system, device, elastic coupling flexible coupling is housed all between diesel engine and gear-box.Traditional major axis type diaphragm type coupling is equipped with 2 groups of diaphragm units usually, and diaphragm is a round structure, and every group of diaphragm unit has 5-6 diaphragms; Be made up of intermediate propeller shaft, two end flange and Bolt Connection, the bending deflection by diaphragm makes the diaphragm type coupling have the bigger angular displacement compensation ability that axially, radially reaches.But then, diaphragm coupling is very exquisite, damages if in use misapply or do not have correct installation then be easy to, and therefore in installation process higher installation precision must be arranged; In traditional diaphragm coupling, diaphragm is installed in the compact structure more, is difficult to observe the virtual condition of diaphragm in the coupling outside, is unfavorable for the daily observation and the maintenance of coupling simultaneously.
Summary of the invention
Technical problem to be solved in the utility model provides a kind of bigger angular displacement compensation ability that axially, radially reaches that has, workload when reduce installing, and can conveniently carry out the elastic coupling flexible coupling of the major axis type multimembrane chip architecture of the daily observation of diaphragm and maintenance.
The technical solution of the utility model is:
A kind of elastic coupling flexible coupling of major axis type multimembrane chip architecture, comprise left flange and right flange, jack shaft, diaphragm unit, the diaphragm seat, the central ring of jack shaft both sides, also comprise first inner pressure ring and second inner pressure ring, diaphragm in the diaphragm unit is a ring, between the left side flange and first inner pressure ring, be respectively arranged with one group of diaphragm unit between the right flange and first inner pressure ring, be respectively arranged with another group diaphragm unit between the two ends of jack shaft and two ends second inner pressure ring, the both ends of the surface of the central ring of jack shaft both sides connect by first bolt respectively and between two groups of diaphragm units and the diaphragm seat.
Be connected by second bolt respectively with the one group of diaphragm unit that is provided with between the left side flange and first inner pressure ring with between the one group of diaphragm unit, right flange and first inner pressure ring that are provided with.
Be connected by second bolt with another group diaphragm unit that is provided with respectively between the two ends of jack shaft and two ends second inner pressure ring.
The diaphragm number that diaphragm unit is every group is two.
Beneficial effect: adopt the elastic coupling flexible coupling diaphragm of major axis type multimembrane chip architecture of the present utility model to change cirque structure into, and 4 groups of diaphragm units are housed, every group of diaphragm unit only is equipped with 2 diaphragms; The inner ring bolt hole of diaphragm is connected with inner pressure ring, and the outer ring bolt hole connects with the diaphragm seat.By above-mentioned improvement, make each of coupling reduce to rigidity, the length of regulating jack shaft simultaneously, the angular displacement compensation ability that axially, radially reaches of coupling improves greatly, has reduced the accuracy of alignment that need adjust when installing, has reduced workload; And guarantee conveniently to observe the virtual condition of diaphragm, conveniently carry out the daily observation and the maintenance of diaphragm in the coupling outside.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Among the figure: 1-left flange, 2-diaphragm, 3-jack shaft, 4-right flange, 5-the first bolt, 6-central ring, 7-diaphragm seat, 8-the second bolt, 9-the first inner pressure ring, 9A-second inner pressure ring.
Embodiment
The utility model is described in further detail below in conjunction with accompanying drawing.
A kind of elastic coupling flexible coupling of major axis type multimembrane chip architecture, comprise left flange 1 and right flange 4, jack shaft 3, diaphragm unit 2, diaphragm seat 7, the central ring 6 of jack shaft 3 both sides, also comprise first inner pressure ring 9 and the second inner pressure ring 9A, diaphragm in the diaphragm unit 2 is a ring, between the left side flange 1 and first inner pressure ring 9, be respectively arranged with one group of diaphragm unit 2 between the right flange 4 and first inner pressure ring 9, be respectively arranged with another group diaphragm unit 2 between the two ends of jack shaft 3 and the two ends second inner pressure ring 9A, the both ends of the surface of the central ring 6 of jack shaft 3 both sides connect by first bolt 5 respectively and between two groups of diaphragm units 2 and the diaphragm seat 7.
Be connected by second bolt 8 respectively with the one group of diaphragm unit 2 that is provided with between the left side flange 1 and first inner pressure ring 9 with between the one group of diaphragm unit 2, right flange 4 and first inner pressure ring 9 that are provided with.
Be connected by second bolt 8 with another group diaphragm unit 2 that is provided with respectively between the two ends of jack shaft 3 and the two ends second inner pressure ring 9A.
The diaphragm number that diaphragm unit is 2 every groups is two.
Input power can be by input flange sequence delivery successively to output flange, guarantees when realizing transferring power, and that improves coupling axially, radially reaches the angular displacement compensation ability, reduces the workload when installing, and is convenient to the daily observation and the maintenance of diaphragm.

Claims (4)

1. the elastic coupling flexible coupling of a major axis type multimembrane chip architecture, comprise left flange (1) and right flange (4), jack shaft (3), diaphragm unit (2), diaphragm seat (7), the central ring (6) of jack shaft (3) both sides, it is characterized in that: also comprise first inner pressure ring (9) and second inner pressure ring (9A), diaphragm in the described diaphragm unit (2) is a ring, between described left flange (1) and first inner pressure ring (9), be respectively arranged with one group of diaphragm unit (2) between right flange (4) and first inner pressure ring (9), be respectively arranged with another group diaphragm unit (2) between the two ends of described jack shaft (3) and two ends second inner pressure rings (9A), the both ends of the surface of the central ring (6) of described jack shaft (3) both sides connect by first bolt (5) respectively and between two groups of diaphragm units (2) and the diaphragm seat (7).
2. the elastic coupling flexible coupling of major axis type multimembrane chip architecture according to claim 1 is characterized in that: be connected by second bolt (8) respectively with the one group of diaphragm unit (2) that is provided with between described left flange (1) and first inner pressure ring (9) with between the one group of diaphragm unit (2), right flange (4) and first inner pressure ring (9) that are provided with.
3. the elastic coupling flexible coupling of major axis type multimembrane chip architecture according to claim 1 is characterized in that: be connected by second bolt (8) with another group diaphragm unit (2) that is provided with respectively between the two ends of described jack shaft (3) and two ends second inner pressure rings (9A).
4. the elastic coupling flexible coupling of major axis type multimembrane chip architecture according to claim 1 is characterized in that: the diaphragm number that described diaphragm unit (2) is every group is two.
CN2011201736739U 2011-05-26 2011-05-26 Long-shaft type elastic coupling with multi-diaphragm structure Expired - Fee Related CN202073947U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011201736739U CN202073947U (en) 2011-05-26 2011-05-26 Long-shaft type elastic coupling with multi-diaphragm structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011201736739U CN202073947U (en) 2011-05-26 2011-05-26 Long-shaft type elastic coupling with multi-diaphragm structure

Publications (1)

Publication Number Publication Date
CN202073947U true CN202073947U (en) 2011-12-14

Family

ID=45112052

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011201736739U Expired - Fee Related CN202073947U (en) 2011-05-26 2011-05-26 Long-shaft type elastic coupling with multi-diaphragm structure

Country Status (1)

Country Link
CN (1) CN202073947U (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102767578A (en) * 2012-08-01 2012-11-07 无锡创明传动工程有限公司 Laminated membrane coupling capable of expanding compensation
CN103821833A (en) * 2014-02-26 2014-05-28 无锡创明传动工程有限公司 Quick installation type lamination flexible coupling
CN109538646A (en) * 2019-01-04 2019-03-29 中国船舶重工集团公司第七0三研究所 A kind of diaphragm type large compensation shaft coupling
CN110005724A (en) * 2019-05-07 2019-07-12 哈尔滨广瀚动力传动有限公司 It is a kind of for connecting the diaphragm coupling of BPRT speed change clutch
CN110542553A (en) * 2019-09-25 2019-12-06 北京工业大学 Input fixing structure of RV reducer comprehensive performance test equipment
CN110578755A (en) * 2019-10-09 2019-12-17 中国船舶重工集团公司第七一一研究所 flexible transmission member

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102767578A (en) * 2012-08-01 2012-11-07 无锡创明传动工程有限公司 Laminated membrane coupling capable of expanding compensation
CN103821833A (en) * 2014-02-26 2014-05-28 无锡创明传动工程有限公司 Quick installation type lamination flexible coupling
CN103821833B (en) * 2014-02-26 2016-08-17 无锡创明传动工程有限公司 Quick mounting type laminated flexible coupling
CN109538646A (en) * 2019-01-04 2019-03-29 中国船舶重工集团公司第七0三研究所 A kind of diaphragm type large compensation shaft coupling
CN110005724A (en) * 2019-05-07 2019-07-12 哈尔滨广瀚动力传动有限公司 It is a kind of for connecting the diaphragm coupling of BPRT speed change clutch
CN110542553A (en) * 2019-09-25 2019-12-06 北京工业大学 Input fixing structure of RV reducer comprehensive performance test equipment
CN110578755A (en) * 2019-10-09 2019-12-17 中国船舶重工集团公司第七一一研究所 flexible transmission member
CN110578755B (en) * 2019-10-09 2024-06-04 中国船舶集团有限公司第七一一研究所 Flexible transmission component

Similar Documents

Publication Publication Date Title
CN202073947U (en) Long-shaft type elastic coupling with multi-diaphragm structure
CN201236898Y (en) Diaphragm coupling with low additional bending moment
CN104061251A (en) Multi-corrugated diaphragm disc coupling
CN203641308U (en) Elastic coupling
CN103671602A (en) Novel film plate type coupler
CN203868165U (en) Multi-corrugated membranous disc coupler
CN201461754U (en) Connecting flange type barreled tooth coupling
CN203421078U (en) Cutting type diaphragm coupling
CN202065369U (en) Freely-detachable high-elasticity coupling
CN203374682U (en) Elastic coupling
CN101922519A (en) Universal flexible multi-functional coupling
CN202118145U (en) High-elasticity coupling capable of being detached integrally
CN204152998U (en) A kind of ringfeder diaphragm type coupler
CN202326801U (en) Limiting double-membrane coupling
CN103737968A (en) Hydraulic machine with buffer mechanism
CN202732753U (en) Buffering durable coupler
CN102644674A (en) Coupling device
CN203500318U (en) Gantry machine tool coupler
CN201779169U (en) Universal flexible multifunctional coupling
CN202579886U (en) Single-turbine torque converter
CN210196297U (en) Short structure external double-diaphragm type coupling
CN214063605U (en) Multi-section diaphragm coupling
CN203612216U (en) Staggered connecting piece for power transmission shaft
CN202659756U (en) Novel axial compensating silicone cushion structure
CN209195993U (en) A kind of double diaphragm couplings

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
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: 20111214

Termination date: 20180526