CN201187565Y - Inertia booster structure - Google Patents
Inertia booster structure Download PDFInfo
- Publication number
- CN201187565Y CN201187565Y CNU2008201106817U CN200820110681U CN201187565Y CN 201187565 Y CN201187565 Y CN 201187565Y CN U2008201106817 U CNU2008201106817 U CN U2008201106817U CN 200820110681 U CN200820110681 U CN 200820110681U CN 201187565 Y CN201187565 Y CN 201187565Y
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- China
- Prior art keywords
- power
- clutch
- power output
- power input
- input shaft
- 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
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- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The utility model discloses an inertial boosting structure which is invented for solving the problem in the prior art that some minor force or discontinuous force can not be utilized. The inertial boosting structure is composed of a speed reducing mechanism provided with a power input shaft and a power output shaft, an inertia wheel as well as a clutch provided with a power input shaft and a power output shaft; the wheel shaft of the inertia wheel is connected with the power output shaft of the speed reducing mechanism and the power output shaft of the clutch through a transmission way. By adopting the structure, minor force or discontinuous force input by the power input shaft of the speed reducing mechanism is accumulated as rotating inertia in virtue of the feature of larger mass of the inertia wheel after being transferred to the inertia wheel through a speed changing mechanism, and the accumulated rotating inertia can be output through the power output shaft of the clutch through operating a handle by the clutch, thereby the inertial boosting structure can be applied for power mechanisms of bicycles, vehicles, planes and steamships, and can be further applied in the fields of electricity generation.
Description
Technical field
The utility model relates to a kind of inertial booster structure.
Background technique
Along with the raising of people's living standard, various dynamic power machines are widely used in each corner in the life.Existing various dynamic power machine such as bicycle, automobile even aircraft etc. often have many less power or the bigger power of being interrupted output slatterns because of being utilized in the course of the work, thereby cause the energy to waste hugely.
The model utility content
For overcoming above-mentioned defective, it is a kind of simple in structure that the purpose of this utility model is to provide, and can will be interrupted the inertial booster structure of the lasting output of power.
For achieving the above object, inertial booster structure of the present utility model is by having a power input shaft and pto reducing gear, a flying wheel and having a power input shaft and a PTO clutch is formed; Wherein, the power input shaft of the pto of the wheel shaft of flying wheel and reducing gear and clutch is in transmission connection.
Further, above-mentioned reducing gear is made up of power input gear and power output gear, wherein, and described flying wheel and the coaxial setting of power output gear.
After adopting said structure, after the less power of the power input shaft input of reducing gear or the power of interruption pass to flying wheel by gear, by the big characteristics of flying wheel quality, as being accumulated of rotary inertia, the rotary inertia that is accumulated then can be exported its pto by clutch by the control of clutch control handle, this rotary inertia can come out its instantaneous burst by the control of clutch, also can as required it be continued output.
Description of drawings
Fig. 1 is the utility model embodiment's a structural representation.
Embodiment
The utility model is further described below in conjunction with drawings and Examples.
As shown in Figure 1, inertial booster structure of the present utility model is by having a power input shaft and pto reducing gear (Fig. 1 medium power input gear 1 and power output gear 2 are formed), flying wheel 3 and having a power input shaft and a PTO clutch is formed; Wherein, the power input shaft of the pto of the wheel shaft of flying wheel and reducing gear and clutch is in transmission connection.Like this, after passing to flying wheel from the power of the less power of the power input shaft of reducing gear input or interruption by gear, by the big characteristics of flying wheel quality, as being accumulated of rotary inertia, the rotary inertia that is accumulated then can be exported its pto by clutch by the control of clutch control handle 5.As shown in the figure, rotary inertia is output shaft 7 (can be the power input shaft of the generator) output by belt 6.
Above-mentioned reducing gear can be selected various suitable speed reducers as required, and the reducing gear among Fig. 1 is made up of power input gear 1 and power output gear 2, wherein, and described flying wheel 3 and power output gear 2 coaxial settings.This structure is comparatively simple, and volume is less, is beneficial to manufacturing.
The size of above-mentioned flying wheel and quality can be according to the differences of used place and power input condition and difference.Above-mentioned clutch also can be selected existing various clutch as required, all can as clutch used on automobile, the motorcycle.
In summary, above-mentioned structure can be with the less power of input shaft input or the power of interruption, accumulate by flying wheel, by the contacted time of solenoidoperated cluthes power input shaft and pto, and the control rotary inertia instantaneous burst that flying wheel accumulated is come out or as required it is continued output, so that save and utilize the energy.Above-mentioned structure can be applicable to power mechanisms such as bicycle, automobile, aircraft and steamer, more can be applicable to fields such as generating.
Claims (2)
1, a kind of inertial booster structure is characterized in that: by having a power input shaft and pto reducing gear, a flying wheel and having a power input shaft and a PTO clutch is formed; Wherein, the power input shaft of the pto of the wheel shaft of flying wheel and reducing gear and clutch is in transmission connection.
2, inertial booster structure as claimed in claim 1, it is characterized in that: described reducing gear is made up of power input gear and power output gear, wherein, described flying wheel and the coaxial setting of power output gear.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201106817U CN201187565Y (en) | 2008-04-30 | 2008-04-30 | Inertia booster structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201106817U CN201187565Y (en) | 2008-04-30 | 2008-04-30 | Inertia booster structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201187565Y true CN201187565Y (en) | 2009-01-28 |
Family
ID=40310586
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008201106817U Expired - Fee Related CN201187565Y (en) | 2008-04-30 | 2008-04-30 | Inertia booster structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201187565Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103227076A (en) * | 2013-04-12 | 2013-07-31 | 东莞市三友联众电器有限公司 | Rectangular rotary armature component for increasing rotatory inertia for magnetic latching relay |
| CN106828627A (en) * | 2017-04-06 | 2017-06-13 | 桂林理工大学 | Flying wheel and bicycle machines people |
-
2008
- 2008-04-30 CN CNU2008201106817U patent/CN201187565Y/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103227076A (en) * | 2013-04-12 | 2013-07-31 | 东莞市三友联众电器有限公司 | Rectangular rotary armature component for increasing rotatory inertia for magnetic latching relay |
| CN106828627A (en) * | 2017-04-06 | 2017-06-13 | 桂林理工大学 | Flying wheel and bicycle machines people |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090128 Termination date: 20130430 |