CN106931057A - A kind of separable Retarder work cavity configuration of rotor - Google Patents
A kind of separable Retarder work cavity configuration of rotor Download PDFInfo
- Publication number
- CN106931057A CN106931057A CN201710178888.1A CN201710178888A CN106931057A CN 106931057 A CN106931057 A CN 106931057A CN 201710178888 A CN201710178888 A CN 201710178888A CN 106931057 A CN106931057 A CN 106931057A
- Authority
- CN
- China
- Prior art keywords
- rotor
- splined shaft
- separable
- retarder
- cavity configuration
- 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
Links
- 238000005516 engineering process Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000013019 agitation Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000979 retarding effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D57/00—Liquid-resistance brakes; Brakes using the internal friction of fluids or fluid-like media, e.g. powders
- F16D57/007—Liquid-resistance brakes; Brakes using the internal friction of fluids or fluid-like media, e.g. powders with variable brake geometry, e.g. axially movable rotor or stator
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Braking Arrangements (AREA)
Abstract
The invention discloses a kind of separable Retarder work cavity configuration of rotor, including housing, rotor, stator and splined shaft;Rotor is connected by helical teeth internal spline with the helical teeth external splines of splined shaft, and stator is installed on housing, and rotor cut spring is installed in the left side of rotor, and spring base is installed on right side, and spring base left side is by the shaft shoulder positioning at the oblique spline of splined shaft;The front-end and back-end of splined shaft are arranged the first cone bearing and the second cone bearing respectively.The present invention realizes the axial movement of rotor using the inside and outside oblique spline of a pair of mutual cooperations by the axial force that oblique spline is produced, and the distance between rotor and stator is increased under non-brake state when retarder reduces the purpose of idling loss to play.
Description
【Technical field】
The present invention relates to a kind of separable Retarder work cavity configuration of rotor.
【Background technology】
The method of current Retarder reduction idle capacity loss has following several:The 1st, flow-disturbing is installed inside working chamber
Device, reduce idling loss by upsetting in working chamber airflow circulating.The 2nd, moveable spoiler is installed in working chamber,
Spoiler is opened or closed by hydraulic control or automatically controlled mode, is substantially to reduce the relative area in rotor section to subtract
Small working chamber effectively plays the purpose for reducing idle capacity loss.The conventional two kinds technologies for reducing empty damage are needed in structure at present
Install hydraulic pressure or automatically controlled executing agency, complex structure additional.If disturbing flow device comes off will to cause to damage to retarder in working chamber
It is bad, increase trouble point.
【The content of the invention】
A kind of shortcoming it is an object of the invention to overcome above-mentioned prior art, there is provided separable hydrodynamic retarding of rotor
Device work cavity configuration.
To reach above-mentioned purpose, the present invention is achieved using following technical scheme:
A kind of separable Retarder work cavity configuration of rotor, including housing, rotor, stator and splined shaft;
Rotor is connected by helical teeth internal spline with the helical teeth external splines of splined shaft, and stator is installed on housing, and the left side of rotor is installed and turned
Spring base is installed on sub- cut spring, right side, and spring base left side is by the shaft shoulder positioning at the oblique spline of splined shaft;Before splined shaft
End and rear end are arranged the first cone bearing and the second cone bearing respectively.
The present invention is further improved:
Stator is secured by bolts on housing.
The oblique spline of splined shaft is to be coordinated using gap between dextrorotation involute profile, interior external splines.
Bearing adjust pad, cone bearing, platen and cushion block are sequentially installed with the right side of spring base, and by bolt Strain lock
Extremely.
The inner ring of the first cone bearing is interference fit with splined shaft, and by shaft shoulder positioning, left side is provided with slowly on inner ring right side
Device drive gear, retarder drive gear is by spline connection on axle.
The right-hand member of gear is fixed by pad and bolt.
Compared with prior art, the invention has the advantages that:
The present invention realizes the axle of rotor using the inside and outside oblique spline of a pair of mutual cooperations by the axial force that oblique spline is produced
To motion, the distance between rotor and stator is increased under non-brake state when retarder reduces the mesh of idling loss to play
's.
【Brief description of the drawings】
Fig. 1 is overall structure diagram of the invention;
Fig. 2 is oblique spline form figure of the invention;
Fig. 3 is oblique spline form figure of the invention.
Wherein:1- splined shafts;2- stators;3- rotor cut springs;4- rotors;5- bolts;6- housings;7- spring bases;8-
Bearing adjust pad;The cone bearings of 9- second;10- platens;11- cushion blocks;12- bolts;41- helical teeth internal splines, flower outside 42- helical teeth
Key.
【Specific embodiment】
The present invention is described in further detail below in conjunction with the accompanying drawings:
Referring to Fig. 1-3, the separable Retarder work cavity configuration of rotor of the present invention, including it is housing 6, rotor 4, fixed
Son 2 and splined shaft 1;Rotor 4 is connected by helical teeth internal spline 41 with the helical teeth external splines 42 of splined shaft 1, and oblique spline form is such as
It is to be coordinated using gap between dextrorotation involute profile, interior external splines shown in Fig. 2 and Fig. 3, flexible relative motion need to be ensured.It is fixed
Son 2 is fixed on housing 6 by bolt 5, and rotor cut spring 3 is installed in the left side of rotor 4, and the right-hand member of rotor cut spring 3 is bullet
Spring abutment 7, by the shaft shoulder positioning at the oblique spline of splined shaft 4, right side is sequentially installed with bearing adjust pad 8, the to the left side of spring base 7
Two cone bearings 9, platen 10, cushion block 11, tense locked eventually through bolt 12.The inner ring of the first cone bearing 13 is with splined shaft 1
Interference fit, by shaft shoulder positioning, left side is provided with retarder drive gear 14 on inner ring right side, and retarder drive gear passes through spline
It is connected on axle 1, the moment of torsion of retarder can be passed to gearbox by gear 14, and the right-hand member of gear 14 passes through pad 15 and bolt 16
It is fixed.
Principle of the invention:
When the axial force to the right of rotor 4 is sufficiently large, rotor 4 will compression rotor cut spring 3 move right, near fixed
Son 2, when axial force is not enough to overcome the elastic force of rotor cut spring 3, rotor 4 is played and reduces idling loss away from stator
Purpose.Program simple structure, reliability is high.As shown in figure 1, looking at from left to right, rotor 4 is rotated counterclockwise with splined shaft 1.
Because rotor 4 is connected by helical spline with splined shaft 1 so splined shaft 1 can produce axial force to the right to rotor 4, when being more than
In Fig. 1 during the elastic force of rotor cut spring 3, rotor will be made to left movement;Producing another component simultaneously makes rotor 4 relative to spline
Axle 1 rotates.
The course of work of the invention:
When retarder works, the cavity between rotor 4 and stator 2 is oil-filled, and retarder produces resistance, the work on oblique spline
Firmly increase, helical teeth also increases therewith to the axial thrust load to the right of rotor 4, now compressible rotor cut spring 3 moves right
It is dynamic, rotor 4 is close to stator 2, be conducive to retarder to produce larger moment of torsion.After retarder is released to be braked, rotor 4 with it is fixed
The fluid in cavity between son 2 is drained, and the fluid in working chamber is changed into air, the resistance ratios that retarder agitation air is produced
The resistance stirred produced by oil can be much smaller, so the axial force for tiltedly being produced between spline 1 and rotor 4 corresponding can also reduce, this
When axial force be not enough to overcome elastic force, under spring force, rotor 4 will be moved to the left, pull open between stator 2 away from
From, play reduce idle capacity loss purpose.
Above content is only explanation technological thought of the invention, it is impossible to limit protection scope of the present invention with this, every to press
According to technological thought proposed by the present invention, any change done on the basis of technical scheme each falls within claims of the present invention
Protection domain within.
Claims (6)
1. a kind of rotor separable Retarder work cavity configuration, it is characterised in that including housing (6), rotor (4),
Stator (2) and splined shaft (1);Rotor (4) is connected by helical teeth internal spline with the helical teeth external splines of splined shaft (1), stator (2)
It is installed on housing (6), rotor cut spring (3) is installed in the left side of rotor (4), and spring base (7), spring base (7) are installed in right side
Left side is by the shaft shoulder positioning at the oblique spline of splined shaft (4);The front-end and back-end of splined shaft (1) are arranged the first cone bearing respectively
And the second cone bearing (9) (13).
2. rotor according to claim 1 separable Retarder work cavity configuration, it is characterised in that stator
(2) it is fixed on housing (6) by bolt (5).
3. rotor according to claim 1 separable Retarder work cavity configuration, it is characterised in that splined shaft
(4) oblique spline is to be coordinated using gap between dextrorotation involute profile, interior external splines.
4. rotor according to claim 1 separable Retarder work cavity configuration, it is characterised in that spring base
(7) bearing adjust pad (8), cone bearing (9), platen (10) and cushion block (11) are sequentially installed with the right side of, and by bolt
(12) tense locked.
5. rotor according to claim 1 separable Retarder work cavity configuration, it is characterised in that the first cone
The inner ring of bearing (13) is interference fit with splined shaft (1), and by shaft shoulder positioning, left side is provided with retarder sliding tooth on inner ring right side
Wheel (14), retarder drive gear is by spline connection on axle (1).
6. rotor according to claim 5 separable Retarder work cavity configuration, it is characterised in that gear
(14) right-hand member is fixed by pad (15) and bolt (16).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710178888.1A CN106931057A (en) | 2017-03-23 | 2017-03-23 | A kind of separable Retarder work cavity configuration of rotor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710178888.1A CN106931057A (en) | 2017-03-23 | 2017-03-23 | A kind of separable Retarder work cavity configuration of rotor |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106931057A true CN106931057A (en) | 2017-07-07 |
Family
ID=59424877
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710178888.1A Pending CN106931057A (en) | 2017-03-23 | 2017-03-23 | A kind of separable Retarder work cavity configuration of rotor |
Country Status (1)
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CN (1) | CN106931057A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111043198A (en) * | 2020-02-22 | 2020-04-21 | 富奥汽车零部件股份有限公司 | Stator preposed hydrodynamic retarder |
CN111075868A (en) * | 2020-02-22 | 2020-04-28 | 富奥汽车零部件股份有限公司 | Rotor detachable hydraulic retarder |
CN111963589A (en) * | 2020-08-26 | 2020-11-20 | 一汽解放汽车有限公司 | Structure for reducing no-load loss of hydraulic retarder |
CN113586631A (en) * | 2021-08-02 | 2021-11-02 | 山东泰鑫汽车科技有限公司 | Power transmission mechanism on reinforced hydraulic retarder |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103047322A (en) * | 2013-01-25 | 2013-04-17 | 重庆杰里安科技有限公司 | Hydraulic retarder |
CN104154202A (en) * | 2014-08-29 | 2014-11-19 | 广西柳工机械股份有限公司 | Double-turbine hydraulic torque converter |
CN104482078A (en) * | 2014-12-10 | 2015-04-01 | 陕西法士特齿轮有限责任公司 | Parallel hydrodynamic retarder structure supported by double cone bearings |
CN105673734A (en) * | 2016-03-01 | 2016-06-15 | 宁波华盛联合制动科技有限公司 | Hydrodynamic retarder and application method thereof |
CN106090076A (en) * | 2016-07-26 | 2016-11-09 | 宁波华盛汽车部件有限公司 | A kind of for Retarder elastic device in parallel |
CN106246707A (en) * | 2016-08-30 | 2016-12-21 | 宁波华盛汽车部件有限公司 | A kind of Retarder and rotor stator separating method thereof |
CN207005141U (en) * | 2017-03-23 | 2018-02-13 | 陕西法士特齿轮有限责任公司 | A kind of separable Retarder work cavity configuration of rotor |
-
2017
- 2017-03-23 CN CN201710178888.1A patent/CN106931057A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103047322A (en) * | 2013-01-25 | 2013-04-17 | 重庆杰里安科技有限公司 | Hydraulic retarder |
CN104154202A (en) * | 2014-08-29 | 2014-11-19 | 广西柳工机械股份有限公司 | Double-turbine hydraulic torque converter |
CN104482078A (en) * | 2014-12-10 | 2015-04-01 | 陕西法士特齿轮有限责任公司 | Parallel hydrodynamic retarder structure supported by double cone bearings |
CN105673734A (en) * | 2016-03-01 | 2016-06-15 | 宁波华盛联合制动科技有限公司 | Hydrodynamic retarder and application method thereof |
CN106090076A (en) * | 2016-07-26 | 2016-11-09 | 宁波华盛汽车部件有限公司 | A kind of for Retarder elastic device in parallel |
CN106246707A (en) * | 2016-08-30 | 2016-12-21 | 宁波华盛汽车部件有限公司 | A kind of Retarder and rotor stator separating method thereof |
CN207005141U (en) * | 2017-03-23 | 2018-02-13 | 陕西法士特齿轮有限责任公司 | A kind of separable Retarder work cavity configuration of rotor |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111043198A (en) * | 2020-02-22 | 2020-04-21 | 富奥汽车零部件股份有限公司 | Stator preposed hydrodynamic retarder |
CN111075868A (en) * | 2020-02-22 | 2020-04-28 | 富奥汽车零部件股份有限公司 | Rotor detachable hydraulic retarder |
CN111963589A (en) * | 2020-08-26 | 2020-11-20 | 一汽解放汽车有限公司 | Structure for reducing no-load loss of hydraulic retarder |
CN113586631A (en) * | 2021-08-02 | 2021-11-02 | 山东泰鑫汽车科技有限公司 | Power transmission mechanism on reinforced hydraulic retarder |
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PB01 | Publication | ||
PB01 | Publication | ||
CB03 | Change of inventor or designer information |
Inventor after: Sun Bo Inventor after: Wang Weijian Inventor after: Yan Jianbo Inventor after: Liu Yi Inventor after: Nie Xingfu Inventor before: Sun Bo Inventor before: Wang Weijian |
|
CB03 | Change of inventor or designer information | ||
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SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170707 |
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RJ01 | Rejection of invention patent application after publication |