CN103471830B - A kind of spatial axes system drive system test unit - Google Patents

A kind of spatial axes system drive system test unit Download PDF

Info

Publication number
CN103471830B
CN103471830B CN201310405951.2A CN201310405951A CN103471830B CN 103471830 B CN103471830 B CN 103471830B CN 201310405951 A CN201310405951 A CN 201310405951A CN 103471830 B CN103471830 B CN 103471830B
Authority
CN
China
Prior art keywords
shaft
bevel gear
driving
gear housing
tubular shaft
Prior art date
Application number
CN201310405951.2A
Other languages
Chinese (zh)
Other versions
CN103471830A (en
Inventor
张辉
朱厚玲
由国静
殷永刚
钱焜
周浩
刘云
Original Assignee
武汉船用机械有限责任公司
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 武汉船用机械有限责任公司 filed Critical 武汉船用机械有限责任公司
Priority to CN201310405951.2A priority Critical patent/CN103471830B/en
Publication of CN103471830A publication Critical patent/CN103471830A/en
Application granted granted Critical
Publication of CN103471830B publication Critical patent/CN103471830B/en

Links

Abstract

The invention discloses a kind of spatial axes system drive system test unit, this device comprises driving mechanism, the synchronism axial system be connected between driving mechanism is unified for the frock frame of support driving mechanism and synchronous shaft system, driving mechanism is symmetrical between two inwardly to be arranged, and synchronous shaft system is the high plane axis system in same center.Instant invention overcomes large space axle system debugging place and the strict limitation of equipment requirement, adopt frock frame will treat that test system all devices center is high and be arranged in sustained height, reduce equipment center high, difference of elevation h2 only has 2.48 meters, decrease the frock quantities raising plant equipment, convenient installation, debugging, maintenance, greatly reduce process costs and potential safety hazard, and the appearance test being specially adapted to large scale ship spatial axes system drive system uses.

Description

A kind of spatial axes system drive system test unit
Technical field
The present invention relates to a kind of test unit, particularly a kind of spatial axes system drive system test unit.
Background technology
In mechanical system testing and measuring technology, be a difficult point in mechanical system testing and measuring technology when mechanical system contains larger spatial axes system of spatial axes system, particularly difference of elevation.
Existing spatial axes system drive system test unit, as Fig. 1, shown in Fig. 2, wait try drive system four cover driving mechanisms 1 between two symmetric transverse outwards arrange, bevel gear housing 11 respectively by driving mechanism 1 is connected with synchronous shaft system 2, synchronous shaft system 2 is not concentricity high spatial axes system, its difference of elevation h1 being vertically arranged on the tubular shaft 27 between bevel gear housing 26 and 28 is up to 6.3 meters, need to build very high stand, not only Installation and Debugging difficulty is large, experimentation cost is high, personal height operation, there is larger potential safety hazard in personnel and equipment, and the four cover driving mechanisms 1 laterally outwards arranged need wider test site, distance d1 between the horizontal center line of the bevel gear housing 11 of its driving mechanism 1 and the bevel gear housing 24 of synchronous shaft system 2 is the length sum of tubular shaft 25 and intermediate shaft 29.Also have and the tubular shaft 27 vertically arranged in synchronous shaft system 2 is cancelled, spatial axes system is converted to plane axis system, although reduce difference of elevation, reduce experimentation cost, improve the safety coefficient of personnel and equipment, but due to not all plant equipment all participate in test, affect the accuracy of test figure.
Summary of the invention
The object of the invention is to overcome the deficiencies in the prior art, a kind of needs is provided to build very high stand, do not need to cancel the tubular shaft vertically arranged, and save process costs, personnel equipment's safety, test figure spatial axes system drive system test unit accurately yet.
The object of the present invention is achieved like this: a kind of spatial axes system drive system test unit, comprise driving mechanism, frock frame that the synchronism axial system be connected between driving mechanism is unified for support driving mechanism and synchronous shaft system, described driving mechanism is four covers, be symmetrical arranged between two, it is characterized in that: described driving mechanism is symmetrical between two inwardly to be arranged, described synchronous shaft system is the high plane axis system in same center, and described driving mechanism and synchronous shaft system are supported on same level by frock frame.
Described synchronous shaft system comprises the first tubular shaft, first symmetrically arranged first bevel gear housing in tubular shaft two ends, the second tubular shaft that first bevel gear housing symmetria bilateralis is arranged, second bevel gear housing, 3rd tubular shaft, triconodont roller box, 4th tubular shaft, 4th bevel gear housing and intermediate shaft, second tubular shaft is laterally outwards arranged between the first bevel gear housing and the second bevel gear housing, 3rd tubular shaft is longitudinally outwards arranged between the second bevel gear housing and triconodont roller box, 4th tubular shaft is laterally outwards arranged between triconodont roller box and the 4th bevel gear housing, intermediate shaft is longitudinally inwardly arranged between the 4th bevel gear housing and driving mechanism bevel gear housing.
Distance d2 between the horizontal center line of described driving mechanism bevel gear housing and the horizontal center line of synchronous shaft system triconodont roller box is the difference of the length of the 3rd tubular shaft and intermediate shaft.
Compared with prior art, instant invention overcomes prior art to large space axle system debugging place and the strict limitation of equipment requirement, adopt frock frame will treat that test system all devices center is high and be arranged in sustained height, reduce equipment center high, difference of elevation h2 only has 2.48 meters, decrease the frock quantities raising plant equipment, convenient installation, debugging and maintenance, greatly reduce experimentation cost and potential safety hazard.Transversely outwards arrange four cover driving mechanisms are inwardly arranged by the present invention simultaneously, the distance d2 of the horizontal center line of driving mechanism bevel gear housing and the horizontal center line of synchronous shaft system triconodont roller box is the difference of the 3rd length between tubular shaft and intermediate shaft, substantially reduces the width in the required place of test.In addition, the tubular shaft vertically arranged is converted to and is horizontally disposed with by the present invention, also do not need like this to cancel the tubular shaft vertically arranged on the basis not needing to build very high stand, make all plant equipment all take part in test, the test figure drawn is accurate and effective.
Accompanying drawing explanation
Fig. 1 is existing space axle system drive system test unit floor plan.
Fig. 2 be in Fig. 1 A to structure enlarged diagram.
Fig. 3 is floor plan of the present invention.
Fig. 4 is E place enlarged drawing in Fig. 3.
Fig. 5 is the front elevation of Fig. 4.
In figure: driving mechanism 1, driving mechanism bevel gear housing 11, reductor 12, synchronous shaft system 2, first tubular shaft 21, first bevel gear housing 22, second tubular shaft 23, bearing seat 23A, the second bevel gear housing 24, the 3rd tubular shaft 25, triconodont roller box 26, the 4th tubular shaft 27, the 4th bevel gear housing 28, intermediate shaft 29, frock frame 3.
Embodiment
Below in conjunction with accompanying drawing, the present invention is described in further detail.
See Fig. 3: a kind of spatial axes system drive system test unit, comprise driving mechanism 1, be connected to synchronous shaft system 2 between driving mechanism 1 and for the frock frame 3 of support driving mechanism 1 with synchronous shaft system 2.Driving mechanism 1 is four covers, symmetrically between two inwardly arranges, and synchronous shaft system 2 be the high plane axis system in same center, and driving mechanism 1 and synchronous shaft system 2 are supported on same level by frock frame 3.
See Fig. 3, Fig. 4: synchronous shaft system 2 comprises the second tubular shaft 23, second bevel gear housing 24, the 3rd tubular shaft 25, triconodont roller box 26, the 4th tubular shaft 27, the 4th bevel gear housing 28 and the intermediate shaft 29 that symmetrically arranged first bevel gear housing 22, first bevel gear housing 22 symmetria bilateralis in the first tubular shaft 21, first tubular shaft 21 two ends is arranged.First tubular shaft 21 is longitudinally arranged between two the first bevel gear housinges 22 between two parties, second tubular shaft 23 is laterally outwards arranged between the first bevel gear housing 22 and the second bevel gear housing 24,3rd tubular shaft 25 is longitudinally outwards arranged between the second bevel gear housing 24 and triconodont roller box 26,4th tubular shaft 27 is laterally outwards arranged between triconodont roller box 26 and the 4th bevel gear housing 28, and intermediate shaft 29 is longitudinally inwardly arranged between the 4th bevel gear housing 28 and driving mechanism bevel gear housing 11.Second tubular shaft 23 is three joints, is connected between every two joints by bearing.Intermediate shaft 29 is band brake dish shaft coupling intermediate shaft.
See Fig. 4, Fig. 5: the reductor 12 of driving mechanism 1 and with bevel gear housing 11, the bevel gear housing 22,24,26 and 28 in synchronous shaft system 2 and bearing seat 23A are supported on same level by frock frame 3, and difference of elevation h2 is 2.48 meters.The distance d2 of the horizontal center line of driving mechanism bevel gear housing 11 and the horizontal center line of synchronous shaft system second bevel gear housing 24 is the difference of the length of the 3rd tubular shaft 25 and intermediate shaft 29.

Claims (2)

1. a spatial axes system drive system test unit, comprise driving mechanism (1), be connected to synchronous shaft system (2) between driving mechanism (1) and for the frock frame (3) of support driving mechanism (1) with synchronous shaft system (2), described driving mechanism (1) is four covers, be symmetrical arranged between two, it is characterized in that: described driving mechanism (1) is symmetrical between two inwardly to be arranged, described synchronous shaft system (2) is the high plane axis system in same center, described driving mechanism (1) and synchronous shaft system (2) are supported on same level by frock frame (3), described synchronous shaft system (2) comprises the first tubular shaft (21), symmetrically arranged first bevel gear housing (22) in first tubular shaft (21) two ends, the second tubular shaft (23) that first bevel gear housing (22) symmetria bilateralis is arranged, second bevel gear housing (24), 3rd tubular shaft (25), triconodont roller box (26), 4th tubular shaft (27), 4th bevel gear housing (28) and intermediate shaft (29), second tubular shaft (23) is laterally outwards arranged between the first bevel gear housing (22) and the second bevel gear housing (24), 3rd tubular shaft (25) is longitudinally outwards arranged between the second bevel gear housing (24) and triconodont roller box (26), 4th tubular shaft (27) is laterally outwards arranged between triconodont roller box (26) and the 4th bevel gear housing (28), intermediate shaft (29) is longitudinally inwardly arranged between the 4th bevel gear housing (28) and driving mechanism bevel gear housing (11).
2. a kind of spatial axes system according to claim 1 drive system test unit, the distance d2 that it is characterized in that between the horizontal center line of described driving mechanism bevel gear housing (11) and the horizontal center line of synchronous shaft system second bevel gear housing (24) is the 3rd tubular shaft (25) and the difference of the length of intermediate shaft (29).
CN201310405951.2A 2013-09-09 2013-09-09 A kind of spatial axes system drive system test unit CN103471830B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310405951.2A CN103471830B (en) 2013-09-09 2013-09-09 A kind of spatial axes system drive system test unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310405951.2A CN103471830B (en) 2013-09-09 2013-09-09 A kind of spatial axes system drive system test unit

Publications (2)

Publication Number Publication Date
CN103471830A CN103471830A (en) 2013-12-25
CN103471830B true CN103471830B (en) 2015-12-23

Family

ID=49796772

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310405951.2A CN103471830B (en) 2013-09-09 2013-09-09 A kind of spatial axes system drive system test unit

Country Status (1)

Country Link
CN (1) CN103471830B (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102288393A (en) * 2011-04-26 2011-12-21 哈尔滨三迪工控工程有限公司 Pneumatic servo type automobile part testing machine
CN202468928U (en) * 2012-01-20 2012-10-03 第一拖拉机股份有限公司 Transmission case arranged in space shaft system of middle-power wheeled tractor

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07318456A (en) * 1994-05-25 1995-12-08 Riyoosen Engineers:Kk High speed spin testing device

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102288393A (en) * 2011-04-26 2011-12-21 哈尔滨三迪工控工程有限公司 Pneumatic servo type automobile part testing machine
CN202468928U (en) * 2012-01-20 2012-10-03 第一拖拉机股份有限公司 Transmission case arranged in space shaft system of middle-power wheeled tractor

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
带胀套的鼓形齿式联轴器的设疑和应用;朱厚玲等;《船海工程》;20090430;第38卷(第2期);第50页第1部分问题的提出,图1 *
用于空间交叉轴系传动的磁性齿轮研制;张静等;《机械制造》;20080331;第46卷(第523期);第32-34页 *

Also Published As

Publication number Publication date
CN103471830A (en) 2013-12-25

Similar Documents

Publication Publication Date Title
GB2509008A (en) Monitoring structural shape or deformations with helical-core optical fiber
CN203094739U (en) Multipurpose liquid containing device
CN102878943B (en) The multiple sensing system of fiber strain integration calibrating installation of large scale and method
CN201941656U (en) Distance measurement device for electrified water washing vehicle
Chatrchyan et al. Measurement of the production cross section for pairs of isolated photons in pp collisions at $\sqrt {s}= 7\; TeV$
CN102564777B (en) Centering adjustment method for wheel sets of locomotive test stand and traction force meter stand thereof
US20150129324A1 (en) Weighing Trolley Case
CN205099246U (en) Cam elevating platform
CN205607360U (en) Outer lane detection device in bearing of plain type
CN202831637U (en) Support frame for manufacturing steel girder
CN201666786U (en) Height measuring device of room space
WO2014186121A3 (en) Optical coherence tomography optical probe systems and methods to reduce artifacts
BR112015006315A2 (en) damping arrangement for a power transmission device
CN104637418A (en) Outdoor lifting advertising board
CN205607303U (en) Outer lane combination detection device in bearing
CN203157764U (en) Child seat of bus
CN204316005U (en) A kind of wire traveling car
CN203874318U (en) Novel climbing-assisting device
CN204286340U (en) Shaft coupling calibrating installation
CN206533233U (en) A kind of straight line module with water proof and dust proof
CN105675910A (en) Wind speed measuring device
CN203519771U (en) On-line detection positioning system for partial discharging of high-voltage switch
CN205808331U (en) A kind of inner bore of part coaxality measuring mechanism
CN203345187U (en) Steel pipe squirrel cage type rack of deep-sea photographing towed body
CN202164068U (en) Lifting mechanism of gantry crane

Legal Events

Date Code Title Description
PB01 Publication
C06 Publication
SE01 Entry into force of request for substantive examination
C10 Entry into substantive examination
GR01 Patent grant
C14 Grant of patent or utility model