CN203717781U - Inner-equilibrium flywheel - Google Patents
Inner-equilibrium flywheel Download PDFInfo
- Publication number
- CN203717781U CN203717781U CN201320778418.6U CN201320778418U CN203717781U CN 203717781 U CN203717781 U CN 203717781U CN 201320778418 U CN201320778418 U CN 201320778418U CN 203717781 U CN203717781 U CN 203717781U
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- China
- Prior art keywords
- flywheel
- inner equilibrium
- rotating disk
- slide block
- equilibrium
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- Withdrawn - After Issue
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Abstract
The utility model discloses an inner-equilibrium flywheel. The inner-equilibrium flywheel comprises a flywheel main body, variable-inertia sliding blocks and an inner-equilibrium turntable, wherein the quantity of the variable-inertia sliding blocks is at least two, and the variable-inertia sliding blocks are uniformly distributed around a rotating shaft of the flywheel main body; each variable-inertia sliding block is radially connected with the flywheel main body in a sliding manner; the inner-equilibrium turntable is coaxially connected with the flywheel main body in a rotating manner, and in sliding fit with the variable-inertia sliding blocks through planar slide rails; the planar slide rails are deflected in the peripheral direction of the turntable to form a certain included angle with the corresponding sliding direction of the sliding blocks. According to the inner-equilibrium flywheel disclosed by the utility model, the rotational inertia can be changed along with change of engine speed within a certain range, in order to ensure the stability in high-speed running of an engine; the inner-equilibrium flywheel can enlarge the rated speed range of the engine, can promote the frequently accelerant flexibility of the engine, improves the comprehensive usage performance of the engine, and meets the demand for social development.
Description
Technical field
The utility model relates to a kind of flywheel, relates in particular to a kind of inner equilibrium flywheel.
Background technique
Flywheel is mounted in the colyliform accumulator compared with large rotating inertia that has on engine crankshaft, and when engine speed increases, the kinetic energy of flywheel increases, and energy is stored up, when engine speed reduces, flywheel energy reduces, energy is discharged, can be used for reducing the speed fluctuation of machine operation process, the portion of energy of motor expansion space stroke can be stored, to overcome the resistance of other strokes, make bent axle Rotating with Uniform, the rotary inertia of flywheel is larger, its accumulation of energy ability is stronger, be beneficial to motor smooth running, but in startup or speed-change process, need to consume the energy of being used to that more energy overcomes flywheel, reduced the flexibility of motor, in prior art, flywheel is generally fixed disk-shaped structure, its rotary inertia immobilizes, conventionally select the weight of middle setting flywheel, can not effectively guarantee the stationarity of high engine speeds running, limited rated engine speed scope, also affect the flexibility of motor busy shift, cause motor Integrated using poor performance, can not meet the needs of social development.
Therefore, need a kind of inner equilibrium flywheel, to guarantee the stationarity of high engine speeds running, expand rated engine speed scope, promote the flexibility of motor busy shift, improve motor Integrated using performance, meet the needs of social development.
Model utility content
In view of this, the utility model provides a kind of inner equilibrium flywheel, can guarantee the stationarity of high engine speeds running, be beneficial to and expand rated engine speed scope, promote the flexibility of motor busy shift, improve motor Integrated using performance, can meet the needs of social development.
Inner equilibrium flywheel of the present utility model, comprises flywheel body, becomes inertia slide block and inner equilibrium rotating disk; Described change inertia slide block is at least two and the wheel body rotating shaft of being diversion and is evenly arranged, and each becomes inertia slide block and all radially slides and be connected in flywheel body; Inner equilibrium rotating disk is connected with flywheel body coaxial rotation; Described inner equilibrium rotating disk is slidably matched by plane slideway with change inertia slide block; Described plane slideway makes it in a certain angle with respective slide glide direction along rotating disk circumferencial direction deflection;
Further, described plane slideway and the corresponding setting one by one of change inertia slide block; The reverse deflection that plane slideway radially turns to inner equilibrium rotating disk from inside to outside along inner equilibrium rotating disk;
Further, when change inertia slide block radially slides from inside to outside along flywheel body, plane slideway diminishes gradually with the angle of phase strain inertia slide block glide direction;
Further, also comprise that the inner equilibrium rotating disk that is used to being connected between flywheel body and inner equilibrium rotating disk provides the elastic component of reverse elastic force;
Further, described elastic component is the torsion spring with flywheel body and the coaxial setting of inner equilibrium rotating disk.
The beneficial effects of the utility model are: inner equilibrium flywheel of the present utility model, its rotary inertia can be within the specific limits changes with the change of engine speed, can guarantee the stationarity of high engine speeds running, be beneficial to and expand rated engine speed scope, promote the flexibility of motor busy shift, improve motor Integrated using performance, can meet the needs of social development.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is further described:
Fig. 1 is structural representation of the present utility model.
Embodiment
Fig. 1 is structural representation of the present utility model, as shown in the figure: inner equilibrium flywheel of the present utility model, comprises flywheel body 1, becomes inertia slide block 2 and inner equilibrium rotating disk 3; Described change inertia slide block 2 is at least two and wheel body 1 rotating shaft of being diversion and is evenly arranged, and each becomes inertia slide block 2 and all radially slides and be connected in flywheel body 1; Inner equilibrium rotating disk 3 is connected with flywheel body 1 coaxial rotation; Described inner equilibrium rotating disk 3 is slidably matched by plane slideway 4 with change inertia slide block 2; Described plane slideway 4 makes it in a certain angle with respective slide glide direction along rotating disk circumferencial direction deflection; In Fig. 1, the A place direction of arrow is turning to of flywheel body 1, and plane slideway 4 is sliding groove structure, is located on inner equilibrium rotating disk 3, becomes corresponding flat slideway 4 on inertia slide block 2 and is fixed with the slip guide block for being slidably matched with plane slideway 4; Each becomes inertia slide block 2 along the 1 place planar slide of flywheel body, plane slideway 4 and flywheel body 1 place plane parallel, and plane slideway 4 can be that linear ramp can be also curve slideway; When plane slideway 4 is curve slideway, be designed to inside and outside two end part and pointed to inner equilibrium rotating disk 3 sense of rotation, middle part is to the cambered way of the reverse protrusion of inner equilibrium rotating disk 3 sense of rotation, that can when flywheel body 1 accelerates to rotate, utilize inner equilibrium rotating disk 3 is used to can hinder the 2 radially outwards slips of change inertia slide block, avoid whole Rotary Inertia of Flywheel to become large, realize and in the short time, complete acceleration; At flywheel body 1, slow down while rotating, can utilize inner equilibrium rotating disk 3 be used to can promote radially inwardly slip of change inertia slide block 2, the rotary inertia of whole flywheel is diminished, realize and in the short time, complete deceleration.
In the present embodiment, described plane slideway 4 and the 2 corresponding settings one by one of change inertia slide block; The reverse deflection that plane slideway 4 radially turns to inner equilibrium rotating disk 3 from inside to outside along inner equilibrium rotating disk 3; While making to become the 2 radially outwards slip of inertia slide block, inner equilibrium rotating disk 3 need to surmount in the rotation of flywheel body 1, when change inertia slide block 2 radially inwardly slides, inner equilibrium rotating disk 3 need to lag behind the rotation of flywheel body 1, therefore at flywheel body 1, accelerate in rotation process, because the effect of inertia of inner equilibrium rotating disk 3 can be to the certain obstruction of change inertia slide block 2 radially outwards slip formation, and then the rotary inertia change that hinders whole flywheel is large, realizes flywheel body and completes speed-raising in 1 short time.
In the present embodiment, when change inertia slide block 2 radially slides from inside to outside along flywheel body 1, plane slideway 4 becomes large gradually with the angle of phase strain inertia slide block 2 glide directions; This angle minimum value is not more than 45 degree, maximum value is not more than 90 degree and is not less than 60 degree, elastic member can be installed between inner equilibrium rotating disk 3 and flywheel body 1 and provide reverse elastic force for inner equilibrium rotating disk 3, therefore can under reverse resilient force, by inner equilibrium rotating disk 3, promote to become inertia slide block 2 returning quicklies, reduce the rotary inertia of whole flywheel, realize and in the short time, complete deceleration.
In the present embodiment, also comprise that the inner equilibrium rotating disk 3 that is used to being connected between flywheel body 1 and inner equilibrium rotating disk 3 provides the elastic component 5 of reverse elastic force, can under reverse resilient force, by inner equilibrium rotating disk 3, effectively control the motion that becomes inertia slide block 2, make the rotary inertia of whole flywheel carry out adaptations according to engine crankshaft rotating speed.
In the present embodiment, described elastic component 5 is the torsion spring with flywheel body 1 and the coaxial setting of inner equilibrium rotating disk 3.
Finally explanation is, above embodiment is only unrestricted in order to the technical solution of the utility model to be described, although the utility model is had been described in detail with reference to preferred embodiment, those of ordinary skill in the art is to be understood that, can modify or be equal to replacement the technical solution of the utility model, and not departing from aim and the scope of technical solutions of the utility model, it all should be encompassed in the middle of claim scope of the present utility model.
Claims (5)
1. an inner equilibrium flywheel, is characterized in that: comprise flywheel body, become inertia slide block and inner equilibrium rotating disk; Described change inertia slide block is at least two and the wheel body rotating shaft of being diversion and is evenly arranged, and each becomes inertia slide block and all radially slides and be connected in flywheel body; Inner equilibrium rotating disk is connected with flywheel body coaxial rotation; Described inner equilibrium rotating disk is slidably matched by plane slideway with change inertia slide block; Described plane slideway makes it in a certain angle with respective slide glide direction along rotating disk circumferencial direction deflection.
2. inner equilibrium flywheel according to claim 1, is characterized in that: described plane slideway and the corresponding setting one by one of change inertia slide block; The reverse deflection that plane slideway radially turns to inner equilibrium rotating disk from inside to outside along inner equilibrium rotating disk.
3. inner equilibrium flywheel according to claim 2, is characterized in that: when change inertia slide block radially slides from inside to outside along flywheel body, plane slideway becomes large gradually with the angle of phase strain inertia slide block glide direction.
4. inner equilibrium flywheel according to claim 3, is characterized in that: also comprise that the inner equilibrium rotating disk that is used to being connected between flywheel body and inner equilibrium rotating disk provides the elastic component of reverse elastic force.
5. inner equilibrium flywheel according to claim 4, is characterized in that: described elastic component is the torsion spring with flywheel body and the coaxial setting of inner equilibrium rotating disk.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201320778418.6U CN203717781U (en) | 2013-11-29 | 2013-11-29 | Inner-equilibrium flywheel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201320778418.6U CN203717781U (en) | 2013-11-29 | 2013-11-29 | Inner-equilibrium flywheel |
Publications (1)
Publication Number | Publication Date |
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CN203717781U true CN203717781U (en) | 2014-07-16 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201320778418.6U Withdrawn - After Issue CN203717781U (en) | 2013-11-29 | 2013-11-29 | Inner-equilibrium flywheel |
Country Status (1)
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CN (1) | CN203717781U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103629302A (en) * | 2013-11-29 | 2014-03-12 | 东风小康汽车有限公司重庆分公司 | Inner balance flywheel |
CN104389947A (en) * | 2014-11-19 | 2015-03-04 | 青岛海之冠汽车配件制造有限公司 | Rotational inertia-adjustable flywheel |
-
2013
- 2013-11-29 CN CN201320778418.6U patent/CN203717781U/en not_active Withdrawn - After Issue
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103629302A (en) * | 2013-11-29 | 2014-03-12 | 东风小康汽车有限公司重庆分公司 | Inner balance flywheel |
CN103629302B (en) * | 2013-11-29 | 2015-10-28 | 东风小康汽车有限公司重庆分公司 | Inner balance flywheel |
CN104389947A (en) * | 2014-11-19 | 2015-03-04 | 青岛海之冠汽车配件制造有限公司 | Rotational inertia-adjustable flywheel |
CN104389947B (en) * | 2014-11-19 | 2016-08-24 | 青岛海之冠汽车配件制造有限公司 | A kind of adjustable flywheel of rotary inertia |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20140716 Effective date of abandoning: 20151028 |
|
C25 | Abandonment of patent right or utility model to avoid double patenting |