CN107676417A - A kind of silicon oil shock absorber - Google Patents
A kind of silicon oil shock absorber Download PDFInfo
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- CN107676417A CN107676417A CN201710919270.6A CN201710919270A CN107676417A CN 107676417 A CN107676417 A CN 107676417A CN 201710919270 A CN201710919270 A CN 201710919270A CN 107676417 A CN107676417 A CN 107676417A
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- 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
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/3207—Constructional features
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- 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
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/10—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using liquid only; using a fluid of which the nature is immaterial
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
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Abstract
A kind of silicon oil shock absorber, including housing and inertia ring, the inertia ring are arranged at enclosure interior；The inertia ring is cyclic structure, rectangular in cross-section structure of the inertia ring along its radial direction, and n damping tooth is evenly equipped with the excircle of the inertia ring, and n is the integer more than or equal to 2；12 or 16 damping teeth are evenly equipped with the excircle of the inertia ring；The damping area intersects with the outer circumference surface of inertia ring, and the damping area and the section at inertia ring intersection and damping area are perpendicular.The design, which is not only simple in structure, to be easy to machine, and effectively improves damping and the rigidity of silicon oil shock absorber, reduces the installing space of silicon oil shock absorber, beneficial to the arrangement of the other trains of motor head.
Description
Technical field
The present invention relates to silicon oil shock absorber, more particularly to a kind of silicon oil shock absorber, it is particularly applicable to increase silicon oil shock absorber
Rigidity and damping, reduce the volume of silicon oil shock absorber.
Background technology
With the development of commercial vehicle market, more and more higher is required to HP, hp/litre and detonation pressure, is same power
Engine, volume is smaller more to have the market competitiveness, so that engine structure design requirement is compacter, and engine
Front end wheel train arrangement requirement is high, and the appearance of multilayer train have impact on the arrangement space of shock absorber axially and radially, and engine rises work(
The lifting of rate requirement, increase is required to the stiffness and damping of shock absorber, if using conventional damper, to reach design requirement, space
Difficult arrangement, while the top of shock absorber, sideshake are small, risk be present in reliability.
In existing silicon oil damper, by the shear stress of silicone oil shock absorber casing and inertia loop coupling, tradition
Shock absorber in, be the face of cylinder on the outside of inner walls and inertia ring, wherein housing is connected with bent axle, and both cause silicon at relative motion
The work(of oily shear stress consumption is finally translated into heat, so as to play torsional oscillation damping effect.
China Patent Publication No. is CN105156543A, and publication date discloses one for the patent of invention on December 16th, 2015
The silicone oil torsional vibration damper of kind high rigidity high-damping, including housing, inertia ring and the side cover being arranged concentrically, the housing include same
Inner wall, shell wall and the side shell wall that the heart is set, the shell wall both sides both sides phase through side shell wall, side cover and inner wall respectively
Connect, noted in the space in the inner chamber that side cover, shell wall, side shell wall, inner wall are surrounded between the inertia ring of sliding sleeve and inner chamber
Entering has silicone oil, side cover anchor ring, apical ring face, side girdle face and side cover, shell wall in inertia ring, is set between the inwall of side shell wall
There are multiple tooth socket fits to increase the fluid area between two relative motion objects, so as to increase the rigidity of silicone oil and damping.
Although the invention can increase the damping of silicon oil shock absorber, it still suffers from following defect：
1st, the damper of the invention can be more complicated with inertia ring structure, between the two with matching relationship, to its size essence
The requirement of degree is higher, is unfavorable for applying to industrialized production.
The content of the invention
The purpose of the present invention is to overcome the problem of production and processing is difficult present in prior art, there is provided one kind is easy to add
Work, the silicon oil shock absorber suitable for industrialized production.
To realize object above, technical solution of the invention is：
A kind of silicon oil shock absorber, including housing and inertia ring, the inertia ring are arranged at enclosure interior；
The inertia ring is cyclic structure, rectangular in cross-section structure of the inertia ring along its radial direction, the inertia ring
N damping tooth is evenly equipped with excircle, n is the integer more than or equal to 2.
12 or 16 damping teeth are evenly equipped with the excircle of the inertia ring.
The distance of crown to the inertia ring outer circumference surface of the damping tooth is h, and h span is 2 millimeters -15 millimeters,
The both sides of the damping tooth are tangent formed with damping area and buffering suface, the buffering suface and inertia ring outer circumference surface.
The damping area intersects with the outer circumference surface of inertia ring, the damping area and the section at inertia ring intersection and damping
Face is perpendicular.
Silicon oil shock absorber is as follows by the calculation formula for damping the increased rigidity of toothing：
Silicon oil shock absorber is as follows by the calculation formula for damping the increased damping of toothing：
Wherein：Cr=R2-R1；
In above-mentioned formula；Cr is the clearance distance between the inertia ring of shock absorber and the outer annular shell of housing, and R2 is outer annular shell
Inner periphery radius, R1 be inertia ring excircle radius, R be shock absorber casing exradius, L is shock absorber thickness, and μ is
Silicon oil viscosity, ω are the speed of related movement of shock absorber casing and inertia ring, ε1For the eccentricity of single damping tooth, h is damping
The crown of tooth is to the distance of inertia ring outer circumference surface, and n is the number that tooth is damped in inertia ring, and r1 is crown, the buffering for damping tooth
The radius of the 3 points of circles surrounded in face point of contact and inertia ring center.
The damping area is the cambered surface of indent.
The damping area intersects with inertia ring outer circumference surface, the damping area and the section at inertia ring intersection and damping area
Angle be acute angle.
The housing includes outer annular shell, interior toroidal shell and the side plate being coaxially disposed, and the outer annular shell passes through side plate and interior toroidal shell
It is connected, the interior toroidal shell and inertia ring rotatable engagement, is uniformly distributed with m housing along the circumference on the inside of the outer annular shell and damps tooth, m
For the integer more than or equal to 2.
The distance of crown to the outer annular shell inner peripheral surface of the housing damping tooth is j, and j span is 2 millimeter of -15 milli
Rice, the radius of the outer annular shell inner periphery is R2, and the both sides of the housing damping tooth form damping area and tooth buffering suface with teeth, institute
The section that tooth buffering suface is tooth periphery is stated, the tooth periphery is using the center of circle of outer annular shell as the center of circle, using R2-j as radius
Periphery；
The tooth damping area intersects with the inner peripheral surface of outer annular shell, the tooth damping area 31 and the inner peripheral surface of outer annular shell 11
Intersection at section and tooth damping area it is perpendicular.
The calculation formula that silicon oil shock absorber damps the increased rigidity of toothing by housing is as follows：
The calculation formula that silicon oil shock absorber damps the increased damping of toothing by housing is as follows：
Wherein：Cr=R2-R1；ε2=r2/R=R2/2R；
In above-mentioned formula；Cr is the clearance distance between the inertia ring of shock absorber and the outer annular shell of housing, and R2 is outer annular shell
Inner periphery radius, R1 be inertia ring excircle radius, R be shock absorber casing exradius, L is shock absorber thickness, and μ is
Silicon oil viscosity, ω are the speed of related movement of shock absorber casing and inertia ring, ε2The eccentricity of tooth is damped for single housing, j is
The crown of housing damping tooth is to the distance of outer annular shell inner peripheral surface, and m is the number that outer annular shell upper shell damps tooth, and r2 is housing resistance
Crown, the radius of tooth buffering suface and 3 points of circles surrounded of outer annular shell inner periphery intersection point and the outer annular shell center of circle of Buddhist nun's tooth.
Compared with prior art, beneficial effects of the present invention are：
1st, damping tooth is set in the inertia ring of silicon oil shock absorber in a kind of silicon oil shock absorber of the present invention, be effectively increased used
Measure the rotational resistance of ring, so as to improve the damping of silicon oil shock absorber and rigidity, the design under same damping and rigidity requirement
Silicon oil shock absorber volume is smaller, weight is lighter.Therefore, the design can effectively improve damping and the rigidity of silicon oil shock absorber,
Reduce the installing space of silicon oil shock absorber, beneficial to the arrangement of the other trains of motor head.
2nd, the damping number of teeth mesh in a kind of silicon oil shock absorber of the present invention in inertia ring is 12 or 16, and such quantity is to the greatest extent
While increase inertia ring that may be big damps, it is easy to the machining of inertia ring.Therefore, the damping tooth of the design inertia ring
Reasonable quantity, it is easy to actual machining.
3rd, damped in the inertia ring in a kind of silicon oil shock absorber of the present invention tooth damping area can be designed as concave surface arc or
The angle of indent, such design is further to increase the resistance that tooth is damped in inertia ring, optimizes and tooth is damped in inertia ring
Structure.Therefore, the damping tooth in the design inertia ring has various structures design, effectively improves damping.
4th, set housing to damp tooth on housing in a kind of silicon oil shock absorber of the present invention, make the damping and just of silicon oil shock absorber
Degree is doubled and redoubled, and further optimizes the mechanical structure of silicon oil shock absorber.Therefore, the design is reasonable in design, damping
Good, silicon oil shock absorber rigidity is high.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the structural representation of inertia ring in Fig. 1.
Fig. 3 is the size marking figure of the present invention.
Fig. 4 is embodiments of the invention 1.
Fig. 5 is embodiments of the invention 3.
Fig. 6 is embodiments of the invention 4.
Fig. 7 is embodiments of the invention 5.
Fig. 8 is the structural representation of housing in Fig. 7.
In figure：Housing 1, outer annular shell 11, interior toroidal shell 12, side plate 13, inertia ring 2, damping tooth 21, damping area 22, buffering suface
23rd, housing damping tooth 3, tooth damping area 31, tooth buffering suface 32.
Embodiment
Below in conjunction with brief description of the drawings, the present invention is further detailed explanation with embodiment.
Referring to Fig. 1 to Fig. 8, a kind of silicon oil shock absorber, including housing 1 and inertia ring 2, the inertia ring 2 are arranged at housing 1
It is internal；
The inertia ring 2 is cyclic structure, rectangular in cross-section structure of the inertia ring 2 along its radial direction, the inertia ring 2
Excircle on be evenly equipped with n damping tooth 21, n is integer more than or equal to 2.
12 or 16 damping teeth 21 are evenly equipped with the excircle of the inertia ring 2.
The distance of crown to the outer circumference surface of inertia ring 2 of the damping tooth 21 is h, and h span is 2 millimeter of -15 milli
Rice, the both sides of the damping tooth 21 are formed with damping area 22 and buffering suface 23, the buffering suface 23 and the outer circumference surface phase of inertia ring 2
Cut.
The damping area 22 intersects with the outer circumference surface of inertia ring 2, the damping area 22 and the section at the intersection of inertia ring 2
It is perpendicular with damping area 22.
Silicon oil shock absorber is as follows by the calculation formula for damping the increased rigidity of the structure of tooth 21：
Silicon oil shock absorber is as follows by the calculation formula for damping the increased damping of the structure of tooth 21：
Wherein：Cr=R2-R1；
In above-mentioned formula；Cr is the clearance distance between the inertia ring 2 of shock absorber and the outer annular shell 11 of housing 1, and R2 is outer
The inner periphery radius of toroidal shell 11, R1 are the excircle radius of inertia ring 2, and R is the exradius of shock absorber casing, and L is shock absorber
Thickness, μ are silicon oil viscosity, and ω is shock absorber casing and the speed of related movement of inertia ring, ε1For the bias of single damping tooth 21
Rate, h are to damp the crown of tooth 21 to the distance of the outer circumference surface of inertia ring 2, and for n to damp the number of tooth 21 in inertia ring 2, r1 is resistance
The radius of the crown of Buddhist nun's tooth 21, the point of contact of buffering suface 23 and the 3 points of circles surrounded in the center of circle of inertia ring 2.
The damping area 22 is the cambered surface of indent.
The damping area 22 intersects with the outer circumference surface of inertia ring 2, the section at the damping area 22 and the intersection of inertia ring 2 with
The angle of damping area 22 is acute angle.
The housing 1 includes outer annular shell 11, interior toroidal shell 12 and the side plate 13 being coaxially disposed, and the outer annular shell 11 passes through side plate
13 are connected with interior toroidal shell 12, and the interior toroidal shell 12 and the rotatable engagement of inertia ring 2, the inner side of the outer annular shell 11 is uniformly distributed along the circumference
There is m housing damping tooth 3, m is the integer more than or equal to 2.
The distance of crown to the inner peripheral surface of outer annular shell 11 of housing damping tooth 3 is j, j span is 2 millimeters-
15 millimeters, the radius of the inner periphery of outer annular shell 11 is R2, and the both sides of the housing damping tooth 3 form damping area 31 and tooth with teeth
Buffering suface 32, the tooth buffering suface 32 be tooth periphery section, the tooth periphery be using the center of circle of outer annular shell 11 as the center of circle,
Periphery using R2-j as radius；
The tooth damping area 31 intersects with the inner peripheral surface of outer annular shell 11, the tooth damping area 31 and the inner circle of outer annular shell 11
Section and tooth damping area 31 at the intersection of side face is perpendicular.
The calculation formula that silicon oil shock absorber damps the increased rigidity of the structure of tooth 3 by housing is as follows：
The calculation formula that silicon oil shock absorber damps the increased damping of the structure of tooth 3 by housing is as follows：
Wherein：Cr=R2-R1；ε2=r2/R=R2/2R；
In above-mentioned formula；Cr is the clearance distance between the inertia ring 2 of shock absorber and the outer annular shell 11 of housing 1, and R2 is outer
The inner periphery radius of toroidal shell 11, R1 are the excircle radius of inertia ring 2, and R is the exradius of shock absorber casing, and L is shock absorber
Thickness, μ are silicon oil viscosity, and ω is shock absorber casing and the speed of related movement of inertia ring, ε2The inclined of tooth 3 is damped for single housing
Heart rate, j are that the crown of housing damping tooth 3 damps tooth 3 to the distance of the inner peripheral surface of outer annular shell 11, m for the upper shell of outer annular shell 11
Number, r2 are that crown, the tooth buffering suface 32 of housing damping tooth 3 enclose with 3 points of the inner periphery intersection point of outer annular shell 11 and 11 center of circle of outer annular shell
Into circle radius.
The principle of the present invention is described as follows：
Hand engine rotation is clockwise direction, when the rotary speed of housing 1 is less than the rotary speed of inertia ring 2,
Damping tooth 21 and/or housing damping tooth 3 inside increased silicon oil damper, that is, add the rotational resistance of shock absorber；Work as shell
When the rotary speed of body 1 is higher than the rotary speed of inertia ring 1, damping tooth 21 and/or housing inside increased silicon oil damper
Tooth 3 is damped, in the case of the original rigidity of shock absorber and damping is not changed, is reached by using damping toothing to extrude silicone oil
The rigidity of extra increase shock absorber and damping.
Covering of the fan arc corresponding to each damping toothing, equivalent on the basis of the covering of the fan arc of no damping toothing
Certain eccentricity is added, the increase of eccentricity, improves rigidity and the damping of shock absorber, is folded by multiple damping toothings
The effect added, it can effectively increase rigidity and the damping of silicon oil damper.
Embodiment 1：
Referring to Fig. 1-Fig. 4, a kind of silicon oil shock absorber, including housing 1 and inertia ring 2, the inertia ring 2 are arranged at housing 1
It is internal；The inertia ring 2 is cyclic structure, rectangular in cross-section structure of the inertia ring 2 along its radial direction, the inertia ring 2
N damping tooth 21 is evenly equipped with excircle, n is the integer more than or equal to 2；The crown of the damping tooth 21 is cylindrical to inertia ring 2
The distance of side face is h, and h span is 2 millimeters -15 millimeters, and the both sides of the damping tooth 21 are gentle formed with damping area 22
Impulse face 23, the buffering suface 23 and the outer circumference surface of inertia ring 2 are tangent；The damping area 22 intersects with the outer circumference surface of inertia ring 2,
The damping area 22 and the section at the intersection of inertia ring 2 and damping area 22 are perpendicular.
Silicon oil shock absorber is as follows by the calculation formula for damping the increased rigidity of the structure of tooth 21：
Silicon oil shock absorber is as follows by the calculation formula for damping the increased damping of the structure of tooth 21：
Wherein：Cr=R2-R1；
In above-mentioned formula；Cr is the clearance distance between the inertia ring 2 of shock absorber and the outer annular shell 11 of housing 1, and R2 is outer
The inner periphery radius of toroidal shell 11, R1 are the excircle radius of inertia ring 2, and R is the exradius of shock absorber casing, and L is shock absorber
Thickness, μ are silicon oil viscosity, and ω is shock absorber casing and the speed of related movement of inertia ring, ε1For the bias of single damping tooth 21
Rate, h are to damp the crown of tooth 21 to the distance of the outer circumference surface of inertia ring 2, and for n to damp the number of tooth 21 in inertia ring 2, r1 is resistance
The radius of the crown of Buddhist nun's tooth 21, the point of contact of buffering suface 23 and the 3 points of circles surrounded in the center of circle of inertia ring 2.
Embodiment 2：
Embodiment 2 is substantially the same manner as Example 1, and its difference is：
12 or 16 damping teeth 21 are evenly equipped with the excircle of the inertia ring 2.
Embodiment 3：
Embodiment 3 is substantially the same manner as Example 2, and its difference is：
Referring to Fig. 5, the damping area 22 is the cambered surface of indent.
Embodiment 4：
Embodiment 4 is substantially the same manner as Example 2, and its difference is：
Referring to Fig. 6, the damping area 22 intersects with the outer circumference surface of inertia ring 2, at the damping area 22 and the intersection of inertia ring 2
The angle of section and damping area 22 be acute angle.
Embodiment 5：
Embodiment 5 is substantially the same manner as Example 2, and its difference is：
Referring to Fig. 7, Fig. 8, the housing 1 includes outer annular shell 11, interior toroidal shell 12 and the side plate 13 being coaxially disposed, the outer shroud
Shell 11 is connected by side plate 13 with interior toroidal shell 12, the interior toroidal shell 12 and the rotatable engagement of inertia ring 2, the outer annular shell 11 it is interior
Side is uniformly distributed with m housing damping tooth 3 along the circumference, and m is the integer more than or equal to 2.
The distance of crown to the inner peripheral surface of outer annular shell 11 of housing damping tooth 3 is j, j span is 2 millimeters-
15 millimeters, the radius of the inner periphery of outer annular shell 11 is R2, and the both sides of the housing damping tooth 3 form damping area 31 and tooth with teeth
Buffering suface 32, the tooth buffering suface 32 be tooth periphery section, the tooth periphery be using the center of circle of outer annular shell 11 as the center of circle,
Periphery using R2-j as radius；
The tooth damping area 31 intersects with the inner peripheral surface of outer annular shell 11, the tooth damping area 31 and the inner circle of outer annular shell 11
Section and tooth damping area 31 at the intersection of side face is perpendicular.
The calculation formula that silicon oil shock absorber damps the increased rigidity of the structure of tooth 3 by housing is as follows：
The calculation formula that silicon oil shock absorber damps the increased damping of the structure of tooth 3 by housing is as follows：
Wherein：Cr=R2-R1；ε2=r2/R=R2/2R；
In above-mentioned formula；Cr is the clearance distance between the inertia ring 2 of shock absorber and the outer annular shell 11 of housing 1, and R2 is outer
The inner periphery radius of toroidal shell 11, R1 are the excircle radius of inertia ring 2, and R is the exradius of shock absorber casing, and L is shock absorber
Thickness, μ are silicon oil viscosity, and ω is shock absorber casing and the speed of related movement of inertia ring, ε2The inclined of tooth 3 is damped for single housing
Heart rate, j are that the crown of housing damping tooth 3 damps tooth 3 to the distance of the inner peripheral surface of outer annular shell 11, m for the upper shell of outer annular shell 11
Number, r2 are that crown, the tooth buffering suface 32 of housing damping tooth 3 enclose with 3 points of the inner periphery intersection point of outer annular shell 11 and 11 center of circle of outer annular shell
Into circle radius.
Claims (10)
1. a kind of silicon oil shock absorber, including housing (1) and inertia ring (2), the inertia ring (2) is arranged at housing (1) inside, its
It is characterised by：
The inertia ring (2) is cyclic structure, rectangular in cross-section structure of the inertia ring (2) along its radial direction, the inertia ring
(2) n damping tooth (21) is evenly equipped with excircle, n is the integer more than or equal to 2.
A kind of 2. silicon oil shock absorber according to claim 1, it is characterised in that：
12 or 16 damping teeth (21) are evenly equipped with the excircle of the inertia ring (2).
A kind of 3. silicon oil shock absorber according to claim 1 or 2, it is characterised in that：
The distance of crown to inertia ring (2) outer circumference surface of the damping tooth (21) is h, and h span is 2 millimeter of -15 milli
Rice, the both sides of the damping tooth (21) are formed with damping area (22) and buffering suface (23), the buffering suface (23) and inertia ring (2)
Outer circumference surface is tangent.
A kind of 4. silicon oil shock absorber according to claim 3, it is characterised in that：
The damping area (22) is intersected with the outer circumference surface of inertia ring (2), at the damping area (22) and inertia ring (2) intersection
Section and damping area (22) are perpendicular.
A kind of 5. silicon oil shock absorber according to claim 4, it is characterised in that：
Silicon oil shock absorber is as follows by the calculation formula for damping the increased rigidity of tooth (21) structure：
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Silicon oil shock absorber is as follows by the calculation formula for damping the increased damping of tooth (21) structure：
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Wherein：Cr=R2-R1；
In above-mentioned formula；Cr is the clearance distance between the inertia ring (2) of shock absorber and the outer annular shell (11) of housing (1), and R2 is
The inner periphery radius of outer annular shell (11), R1 are the excircle radius of inertia ring (2), and R is the exradius of shock absorber casing, and L is
Shock absorber thickness, μ are silicon oil viscosity, and ω is shock absorber casing and the speed of related movement of inertia ring, ε1For single damping tooth
(21) eccentricity, h are that the crown of damping tooth (21) arrives the distance of inertia ring (2) outer circumference surface, and n is damps in inertia ring (2)
The number of tooth (21), r1 are crown, buffering suface (23) point of contact and inertia ring (2) 3 points of center of circle circle surrounded for damping tooth (21)
Radius.
A kind of 6. silicon oil shock absorber according to claim 3, it is characterised in that：
The damping area (22) is the cambered surface of indent.
A kind of 7. silicon oil shock absorber according to claim 3, it is characterised in that：
The damping area (22) is intersected with inertia ring (2) outer circumference surface, the damping area (22) and cutting at inertia ring (2) intersection
Face and the angle of damping area (22) are acute angle.
A kind of 8. silicon oil shock absorber according to claim 1 or 2, it is characterised in that：
The housing (1) includes outer annular shell (11), interior toroidal shell (12) and the side plate (13) being coaxially disposed, and the outer annular shell (11) is logical
Cross side plate (13) with interior toroidal shell (12) to be connected, the interior toroidal shell (12) and inertia ring (2) rotatable engagement, the outer annular shell (11)
Inner side be uniformly distributed with m housing damping tooth (3) along the circumference, m is the integer more than or equal to 2.
A kind of 9. silicon oil shock absorber according to claim 8, it is characterised in that：
The distance of crown to outer annular shell (11) inner peripheral surface of housing damping tooth (3) is j, j span is 2 millimeters-
15 millimeters, the radius of outer annular shell (11) inner periphery is R2, and the both sides of the housing damping tooth (3) form damping area with teeth
(31) and tooth buffering suface (32), the tooth buffering suface (32) are the section of tooth periphery, and the tooth periphery is with outer annular shell
(11) the center of circle is the center of circle, the periphery using R2-j as radius；
The tooth damping area (31) is intersected with the inner peripheral surface of outer annular shell (11), the tooth damping area (31) and outer annular shell (11)
Section and tooth damping area (31) at the intersection of inner peripheral surface is perpendicular.
A kind of 10. silicon oil shock absorber according to claim 9, it is characterised in that：
The calculation formula that silicon oil shock absorber damps the increased rigidity of tooth (3) structure by housing is as follows：
<mrow>
<msub>
<mi>K</mi>
<mn>2</mn>
</msub>
<mo>=</mo>
<mn>24</mn>
<msup>
<mi>R</mi>
<mn>3</mn>
</msup>
<msub>
<mi>L&mu;&omega;&epsiv;</mi>
<mn>2</mn>
</msub>
<mi>m</mi>
<mo>/</mo>
<mo>&lsqb;</mo>
<msup>
<mi>Cr</mi>
<mn>3</mn>
</msup>
<mrow>
<mo>(</mo>
<mn>2</mn>
<mo>+</mo>
<msubsup>
<mi>&epsiv;</mi>
<mn>2</mn>
<mn>3</mn>
</msubsup>
<mo>)</mo>
</mrow>
<mrow>
<mo>(</mo>
<mn>1</mn>
<mo>-</mo>
<msubsup>
<mi>&epsiv;</mi>
<mn>2</mn>
<mn>2</mn>
</msubsup>
<mo>)</mo>
</mrow>
<mo>&rsqb;</mo>
</mrow>
The calculation formula that silicon oil shock absorber damps the increased damping of tooth (3) structure by housing is as follows：
<mrow>
<msub>
<mi>C</mi>
<mn>2</mn>
</msub>
<mo>=</mo>
<mn>12</mn>
<msup>
<mi>&pi;R</mi>
<mn>3</mn>
</msup>
<mi>L</mi>
<mi>&mu;</mi>
<mi>m</mi>
<mo>/</mo>
<mo>&lsqb;</mo>
<msup>
<mi>Cr</mi>
<mn>3</mn>
</msup>
<mrow>
<mo>(</mo>
<mn>2</mn>
<mo>+</mo>
<msubsup>
<mi>&epsiv;</mi>
<mn>2</mn>
<mn>3</mn>
</msubsup>
<mo>)</mo>
</mrow>
<msup>
<mrow>
<mo>(</mo>
<mn>1</mn>
<mo>-</mo>
<msubsup>
<mi>&epsiv;</mi>
<mn>2</mn>
<mn>2</mn>
</msubsup>
<mo>)</mo>
</mrow>
<mn>0.5</mn>
</msup>
<mo>&rsqb;</mo>
</mrow>
Wherein：Cr=R2-R1；ε2=r2/R=R2/2R；
In above-mentioned formula；Cr is the clearance distance between the inertia ring (2) of shock absorber and the outer annular shell (11) of housing (1), and R2 is
The inner periphery radius of outer annular shell (11), R1 are the excircle radius of inertia ring (2), and R is the exradius of shock absorber casing, and L is
Shock absorber thickness, μ are silicon oil viscosity, and ω is shock absorber casing and the speed of related movement of inertia ring, ε2Damped for single housing
The eccentricity of tooth (3), j be housing damp tooth (3) crown to the distance of outer annular shell (11) inner peripheral surface, m is outer annular shell (11)
The number of upper shell damping tooth (3), r2 are the crown of housing damping tooth (3), tooth buffering suface (32) and outer annular shell (11) inner periphery
The radius of 3 points of circles surrounded of intersection point and outer annular shell (11) center of circle.
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2701183A1 (en) * | 1976-01-23 | 1977-07-28 | Geislinger Dr Ing Leonard | ROTARY VIBRATION DAMPER OR VIBRATION-DAMPING AND TORSO-ELASTIC COUPLING |
| US4392751A (en) * | 1980-06-04 | 1983-07-12 | Hitachi, Ltd. | Damped bearing device |
| CN202001549U (en) * | 2011-03-16 | 2011-10-05 | 天津大学 | Shock absorber of diesel engine |
| US20140260782A1 (en) * | 2013-03-13 | 2014-09-18 | Trd U.S.A., Inc. | Dampers For Crankshafts Of Reciprocating Engines and Reciprocating Engines Comprising The Same |
| CN104696431A (en) * | 2015-02-13 | 2015-06-10 | 柳州金鸿橡塑有限公司 | Rubber torsional shock absorber |
| CN207500380U (en) * | 2017-09-30 | 2018-06-15 | 东风商用车有限公司 | Silicon oil shock absorber structure |
| CN207569134U (en) * | 2017-09-30 | 2018-07-03 | 东风商用车有限公司 | A kind of silicon oil shock absorber |
-
2017
- 2017-09-30 CN CN201710919270.6A patent/CN107676417B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2701183A1 (en) * | 1976-01-23 | 1977-07-28 | Geislinger Dr Ing Leonard | ROTARY VIBRATION DAMPER OR VIBRATION-DAMPING AND TORSO-ELASTIC COUPLING |
| US4392751A (en) * | 1980-06-04 | 1983-07-12 | Hitachi, Ltd. | Damped bearing device |
| CN202001549U (en) * | 2011-03-16 | 2011-10-05 | 天津大学 | Shock absorber of diesel engine |
| US20140260782A1 (en) * | 2013-03-13 | 2014-09-18 | Trd U.S.A., Inc. | Dampers For Crankshafts Of Reciprocating Engines and Reciprocating Engines Comprising The Same |
| CN104696431A (en) * | 2015-02-13 | 2015-06-10 | 柳州金鸿橡塑有限公司 | Rubber torsional shock absorber |
| CN207500380U (en) * | 2017-09-30 | 2018-06-15 | 东风商用车有限公司 | Silicon oil shock absorber structure |
| CN207569134U (en) * | 2017-09-30 | 2018-07-03 | 东风商用车有限公司 | A kind of silicon oil shock absorber |
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| CN107676417B (en) | 2023-05-30 |
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