CN101265964A - Double-speed superposition effect constrained fluid inertia energy accumulating booster unit - Google Patents
Double-speed superposition effect constrained fluid inertia energy accumulating booster unit Download PDFInfo
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- CN101265964A CN101265964A CNA2007100851899A CN200710085189A CN101265964A CN 101265964 A CN101265964 A CN 101265964A CN A2007100851899 A CNA2007100851899 A CN A2007100851899A CN 200710085189 A CN200710085189 A CN 200710085189A CN 101265964 A CN101265964 A CN 101265964A
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- 239000012530 fluid Substances 0.000 title claims abstract description 22
- 230000000694 effects Effects 0.000 title claims description 21
- 239000003921 oil Substances 0.000 claims description 33
- 238000007789 sealing Methods 0.000 claims description 13
- 239000010721 machine oil Substances 0.000 claims description 8
- 239000000314 lubricant Substances 0.000 claims description 5
- 235000015927 pasta Nutrition 0.000 claims description 4
- 230000008676 import Effects 0.000 claims description 2
- 230000000977 initiatory effect Effects 0.000 claims description 2
- 239000007788 liquid Substances 0.000 claims description 2
- 230000009969 flowable effect Effects 0.000 claims 2
- 238000003860 storage Methods 0.000 abstract description 3
- 239000007787 solid Substances 0.000 abstract description 2
- 230000005540 biological transmission Effects 0.000 abstract 4
- 239000010687 lubricating oil Substances 0.000 abstract 2
- 230000005611 electricity Effects 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 2
- 238000005461 lubrication Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000002195 synergetic effect Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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Abstract
A restraint fluid inertia storage power assisting device with double-speed superposition action comprises a base, a housing, a main shaft, a main inertia wheel, transmission gears, auxiliary shafts, an auxiliary inertia wheel, a driving gear, a restricted baffle, a flowing solid object, a front end face cover and a rear end face cover , and bearings. The upper part of the base is connected with the bottom part of the housing, the central holes of the front and the rear end faces are respectively with the bearing, the transmission gears with bearings inside the central holes are respectively fixed to the inner sides of the front and the rear end face covers, the middle part of the main shaft is connected with the central hole of the main inertia wheel, a plurality of auxiliary shafts are fixed to longitudinal holes formed on the end face of the main inertia wheel at uniform angles by the bearings, lubricating oil is sealed inside an adding layer, the two sides of auxiliary shafts are connected with the auxiliary inertia wheel and the central holes of the driving gear, the restricted baffle is fixed inside the adding layer of the auxiliary inertia wheel to seal lubricating oil, the outer diameter of the two sides of the main shaft are respectively connected with the inner diameter of the bearing of the transmission gear and the inner diameter of the bearing of the front and the rear end face covers, the driving gear engages with the transmission gear, and the front and the rear end face covers are fixed on the two ends of the housing through screws.
Description
Technical field
The present invention relates to a kind of power assisting device that utilizes the double-speed superposition effect that retrains the real object that flows to carry out inertial energy-accumulating, rotate the inertial energy-accumulating power assisting device that replaces the real object flying wheel to carry out double speed stack rotation by the constraint of fluid specifically, this device is applicable to mechanical and power equipment manufacturing field.
Background technique
At present, the structure of inertial energy-accumulating power assisting device known to the public such as punch press, angle bender, inertial energy-accumulating electricity generating device etc. all is to connect external power source by the flying wheel that a dead axle rotates to form.Flying wheel storage and release kinetic energy that these inertial energy-accumulating power apparatus mainly rely on dead axle to rotate, because the size of the flying wheel that dead axle rotates storage kinetic energy numerical value is directly proportional with the rotary inertia and the rotational velocity of flying wheel, therefore, the rotary inertia numerical value of the flying wheel of increase dead axle rotation or the rotational kinetic energy that rotational velocity numerical value can both obtain bigger numerical.Yet; the rotary inertia and the rotational velocity that increase flying wheel in actual application simultaneously are very difficult; because; existing manufacturing processing technic inevitably trueness error can occur, and the flying wheel of big numerical value rotary inertia operation under big numerical value rotational velocity state will causing dynamic balancing imbalance generation vibration causes shuts down and security incident.Therefore the rotational velocity numerical value of the flying wheel in the inertial energy-accumulating power assisting device of manufacturing at present is approximately all about 3000 rev/mins.The deficiency that its technology exists is that the flying wheel in the existing inertial energy-accumulating power assisting device can not regulate dynamic balancing automatically, thereby causes flying wheel can not improve rotational velocity and finally can't store and discharge the bigger kinetic energy of numerical value.
Summary of the invention
Have the deficiency that the flying wheel in the inertial energy-accumulating power assisting device can not be regulated dynamic balancing automatically and can't improve rotational velocity now in order to overcome, the invention provides a kind of constrained fluid inertia energy accumulating booster unit of double-speed superposition effect, but the flying wheel that the dead axle in this inertial energy-accumulating power assisting device rotates can not only utilize constrain fluids to regulate dynamic balancing automatically, and can utilize the double-speed superposition effect of flying wheel to improve the kinetic energy that rotational velocity increases flying wheel.
The technical solution adopted for the present invention to solve the technical problems is: at first the single flying wheel structural change with former inertial energy-accumulating power assisting device is the structure of several flying wheels, be vertically to fixedly mount several secondary flying wheels by equal equal angles along axle on the wheel body of the single flying wheel in the former inertial energy-accumulating power assisting device, and several secondary flying wheels are rotated simultaneously on both direction relative to earth inertial coodinate system in mechanically operated mode, utilize two angular velocity components of several secondary flying wheels to form synergistic effect, improve the rotational velocity of several secondary flying wheels thus; Next changes the interior shape of several flying wheels, several flying wheels are manufactured inside have the hollow flying wheel that adds layer of the cylinder bodily form, add the flowed real object that layer injects 2/3 capacity to the flying wheel boring, and with screw sealed oil-filling hole, utilize hollow hollow several restricted baffles constraints that layer inner circumference outer rim install by the impartial fixed angle real object that flows that adds of layer and flying wheel that adds of flying wheel, reach the real object that when several flying wheel wheel shafts of extraneous drive power source rotate, can flow and be subjected to the inertial centrifugal force even action to be distributed in the hollow layer inner circumferential edge that add to regulate flying wheel rotation dynamic balancing automatically.
The invention has the beneficial effects as follows, can rotate with several flying wheels in constrain fluids and regulate automatically under the dynamically balanced situation of several flying wheels, and several flying wheels form under the state of double-speed superposition effect, thereby improve the ideal that several flying wheel rotational angular realize increasing flying wheel kinetic energy, simple in structure.
Description of drawings
Fig. 1 is the vertical A-A generalized section of structure of the constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect of the present invention.
Fig. 2 is the horizontal B-B generalized section of structure of the constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect of the present invention.
1. input flange dishes among the figure, 2. main shaft oil sealing is fixedly fastened before 3., 4. front end cover, 5. retaining screw, 6. secondary flying wheel, 7. lubricant oil, 8. restricted baffle, 9. oil hole screw, 10. countershaft oil sealing, 11. main flying wheels, 12. pasta positioning hole screws, 13. countershaft, 14. actuation gears, 15. countershaft hold-doun nuts, 16. the rear end cover, 18. output flanges are fixedly fastened in 17. backs, 19. main shaft bearing, 20. electronic oil pumps, 21. driving gears, 22. machine oil pipe, 23. counter shaft bearing, 24. main shafts, 25. casings, 26. guide bearing, 27. bases.
Embodiment
The invention will be further described by embodiment below in conjunction with accompanying drawing: as Fig. 1, shown in Figure 2, base among the figure (27) is a rectangular slot steelframe, casing among the figure (25) is a hollow cylindrical metal construction, the bottom of casing (25) external diameter is connected surely with the top electricity consumption solid welding of base (27), front end cover (4) among the figure, rear end cover (16) is metal circular plate, front end cover (4), rear end cover (16) center portion is drilled with a hole respectively, the internal diameter in hole is fixedlyed connected with the external diameter of main shaft bearing (19) respectively, front end cover (4), (3) are fixedly fastened by several respectively in rear end cover (16) inboard, (17) a fixedly connected driving gear that does not rotate (21), driving gear (21) center hole internal diameter is fixedlyed connected with the external diameter of guide bearing (26), main shaft among the figure (24) is the cylindrical body oblique crank Z of being made by metallic material, main shaft (24) passes its external diameter middle part of main flying wheel (11) center hole fixedlys connected with the center hole internal diameter of main flying wheel (11), main flying wheel (11) is that an inside has the cylinder bodily form wheel that a hollow metallic material that adds layer of the cylinder bodily form is made among the figure, the front-end face of main flying wheel (11) near the position of outer rim at interval all equal angles vertically bore several along axle and penetrate the circular port of main flying wheel (11) wheel body to ear end face, the center line of each circular port internal diameter equates apart from the center line numerical value of main shaft (24), each circular port internal diameter is fixedlyed connected with the external diameter of two counter shaft bearings (23) respectively, the internal diameter of per two counter shaft bearings (23) is fixedly connected to form the axle group of main flying wheel (11) respectively with the external diameter middle part of a countershaft (13) that penetrates main flying wheel (11) wheel body, seal by countershaft oil sealing (10) between the wheel body both ends of the surface of main flying wheel (11) and several countershafts (13) external diameter, the outer rim of main flying wheel (11) wheel body has a pasta positioning hole, add the fluid lubrication oil that layer injects 2/3 capacity by the pasta positioning hole to main flying wheel (11) boring, positioning hole tightens up sealing with screw (12), the diameter of axle that every countershaft (13) stretches out the external both sides of main flying wheel (11) wheel all passes the center hole of a secondary flying wheel (6) and is fixedly connected to form the rotatable subsystem of several secondary flying wheels (6) with the center hole internal diameter, secondary flying wheel (6) among the figure is that an inside of being made by metallic material has the hollow cylinder bodily form wheel that adds layer of the cylinder bodily form, the hollow layer impartial fixed angle in inner circumferential edge interval that add at secondary flying wheel (6) installed several restricted baffles (8), have oil hole on secondary flying wheel (6) end face, add the fluid lubrication oil that layer injects 2/3 capacity by oil hole to secondary flying wheel (6) boring, oil hole tightens up sealing with screw (9), the two end axles external diameter of several countershafts (13) passes the center hole of an actuation gear (14) respectively and fixedlys connected with the internal diameter of actuation gear (14) center hole among the figure, the fixedly connected countershaft hold-doun nut of the two axial ends external diameter of several countershafts (13) (15), by main shaft (24), main flying wheel (11), several counter shaft bearings (23), several countershafts (13), several secondary flying wheels (6), the rotatable system that several actuation gears (14) assemble vertically is placed in casing (25) housing, the length of designing requirement main shaft (24) is greater than the length of casing (25), the two side shaft external diameters that stretch out the outer main shaft (24) of casing (25) housing respectively with front end cover (4), inboard fixedly connected interior bearing (26) internal diameter and the front end cover (4) of driving gear (21) center hole of rear end cover (16), bearing (19) internal diameter in rear end cover (16) center hole is fixedly connected, several actuation gears (14) by with front end cover (4), fixing driving gear (21) engagement realizes that power connects on rear end cover (16) inboard, front end cover (4), fixedly connected by screw (5) between rear end cover (16) and the casing (25), the fixing input flange dish (1) of main shaft (24) external diameter front end that stretches out casing (25) is fixedlyed connected with the external power source output shaft, the fixing output flange (18) in main shaft (24) external diameter rear end that stretches out casing (25) is fixedlyed connected with the load input shaft, front end cover (4), the outside, rear end cover (16) center portion fixed main shaft oil sealing (2), the external diameter sliding contact of the internal diameter of main shaft oil sealing (2) and main shaft (24), electronic oil pump among the figure (20) is fixed on rear end cover (16) exterior bottom by screw, the machine oil pipe (22) of electronic oil pump (20) is fixed on casing (25) housing inside bottom by screw, the liquid level height of casing (25) housing inside bottom filling lubricant oil must not contact several secondary flying wheels (6), by main shaft (24), main flying wheel (11), several counter shaft bearings (23), several countershafts (13), several secondary flying wheels (6), leaving suitable gap between rotatable system that several actuation gears (14) assemble and casing (25) the housing inboard can keep rotatable system freely to rotate.Should connect power initiation electronic oil pump (20) when external power source drive main spindle (24) is rotated, electronic oil pump (20) sucks the lubricant oil of casing (25) inside bottom filling by machine oil pipe (22) import and is directly injected on the flank of tooth of several actuation gears (14) by machine oil pipe (22) outlet.
The constrained fluid inertia energy accumulating booster unit embodiment's of a kind of double-speed superposition effect of the present invention base (27) is the rectangular slot steelframe of 900mm * 800mm * 80mm, embodiment's casing (25) is the hollow cylindrical housing that steel plate is made, outer diameter Φ=500mm, inner diameter Φ=498mm, length L=308mm, embodiment's main shaft (24) largest diameter=32mm, length L=458mm, diameter of phi=the 404mm of embodiment's main flying wheel (11), length L=70mm, mass M=12.80kg (gross masses of main flying wheel and several secondary flying wheels), quantity is 1, diameter of phi=the 148mm of embodiment's secondary flying wheel (6), length L=30mm, mass M=3.895kg, quantity is 2, external diameter Φ=the 65mm of several actuation gears (14) of embodiment, the number of teeth is 42 teeth, external diameter Φ=the 195mm of 2 driving gears (21) of embodiment, the number of teeth is 128 teeth, actuation gear (14) is about 3: 1 with the rotating ratio of driving gear (21), and the exterior power source power is the two-phase motor of 0.37kw, and motor speed is 1450 rev/mins.Motoring embodiment's main shaft (24) thus rotate and to drive main flying wheel (11) and rotate around main shaft (24) center, 2 countershafts (13), 2 secondary flying wheels (6), 2 actuation gears (14) are followed main flying wheel (11) and are rotated around main shaft (24) center.At this moment, 2 secondary flying wheels (6) obtain first rotational angular velocity ω as the part of main flying wheel
1Component forms inertial energy-accumulating for the first time, because the engagement of 2 actuation gears (14) and driving gear (21), main shaft (24) passes to 2 actuation gears (14) by driving gear (21) with driving force, 2 actuation gears (14) rotate around 2 countershafts (13) center around rotation 2 secondary flying wheels of drive (6) of driving gear (21), like this, 2 secondary flying wheels (6) itself obtain second angular velocity omega
2Component forms inertial energy-accumulating for the second time.So, the constrained fluid inertia energy accumulating booster unit embodiment's of a kind of double-speed superposition effect of the present invention the main flying wheel (11) and the angular velocity omega of 2 secondary flying wheels (6)
1+ ω
2Produce synergistic effect.When the rotational velocity of main flying wheel (11) and 2 secondary flying wheels (6) increases gradually, the rotational angular velocity numerical value of 2 secondary flying wheels (6) is all the time greater than the rotational angular velocity numerical value of main flying wheel (11), main flying wheel (11) and 2 secondary flying wheels (6) are hollow add in the layer mobile real object (7)---lubricant oil is subjected to the inertial centrifugal force effect can both be evenly distributed on the hollow layer inner circumferential edge that add and regulates dynamic balancing automatically, make main flying wheel (11) and 2 secondary flying wheels (6) steadily quicken rotation.Its angular velocity omega when the rotational velocity of the main flying wheel (11) in the embodiment of the invention reaches 1450 rev/mins
1=48.3 π radian per seconds; Its angular velocity omega when the rotational velocity of 2 secondary flying wheels (6) reaches 4350 rev/mins
2=145 radian per seconds.The angular velocity sum ω of main flying wheel (11) and 2 secondary flying wheels (6)
1+ ω
2=193.3 π radian per seconds.The increase of the angular velocity sum numerical value of main flying wheel (11) and 2 secondary flying wheels (6) causes the rotational kinetic energy numerical value of main flying wheel (11) and 2 secondary flying wheels (6) to increase the total kinetic energy E of main flying wheel (11) and 2 secondary flying wheels (6)
tCan try to achieve by following formula:
E
t=1/2 (I
1+ I
2) * (ω
1+ ω
2)
2(I in the formula
1Be the rotary inertia of main flying wheel (11), ω
1Be the angular velocity of main flying wheel (11), I
2Be the rotary inertia of 2 secondary flying wheels (6), ω
2Be the angular velocity of 2 secondary flying wheels (6)).
2 driving gears (21) if dismantle in embodiments of the present invention do not rotate 2 secondary flying wheels (6), and 2 secondary flying wheels (6) can only obtain a rotational angular velocity ω as the part of main flying wheel (11)
1Component forms an inertial energy-accumulating, the total kinetic energy E of main flying wheel (11) and 2 secondary flying wheels (6) savings
p=1/2I
1ω
1 2, because E
t＞E
p, therefore, under the situation that same external power source drives, adopt main flying wheel (11) and the stack of several secondary flying wheel (6) angular velocity to rotate the kinetic energy that can obtain bigger numerical.
The main flying wheel (11) in the embodiment of the invention and the total kinetic energy E of 2 secondary flying wheels (6)
tEngagement by 2 actuation gears (14) and driving gear (21) finally passes to main shaft (24), when the external power source in the embodiment of the invention---behind the two-phase motor powered-down circuit of 0.37kw, the output flange (18) of main shaft (24) axle head can be to coupled load main shaft output kinetic energy E
t
The present invention uses inner hollow of main flying wheel (11) and several secondary flying wheels (6) to add layer, the restricted baffle constraint real object (7) that flows and regulates dynamic balancing automatically, utilize the double-speed superposition effect of main flying wheel (11) and several secondary flying wheels (6) to improve rotational velocity, resulting beneficial effect is that the two dimensional motion kinetic energy that causes is rotated in the angular velocity stack that has obtained main flying wheel (11) and several secondary flying wheels (6), thereby realizes utilizing main flying wheel (11) and several secondary flying wheels (6) to store and discharging the ideal that big numerical value kinetic energy carries out power compensation.
The constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect of the present invention can mate between the gearbox that is installed to agricultural tools, automobile, motorcycle, naval vessels boats and ships etc. and the load as power compensation device, also can be installed between the fan blade wheel shaft of wind-driven generator and the generator as the wind speed stabilizer, can also mate and be installed between generator and the motor as the inertial energy-accumulating generator set, set inertial energy-accumulating generator set in batches is equipped with the electricity consumption peak valley accumulation of energy that heat energy power-generating factory can satisfy the power station.
Claims (8)
1. the constrained fluid inertia energy accumulating booster unit of a double-speed superposition effect comprises input flange dish (1), main shaft oil sealing (2), preceding fixedly fasten (3), front end cover (4), retaining screw (5), several secondary flying wheels (6), real object (7) flows, several restricted baffles (8), oil hole screw (9), countershaft oil sealing (10), main flying wheel (11), pasta positioning hole screw (12), several countershafts (13), several actuation gears (14), countershaft hold-doun nut (15), rear end cover (16), (17) are fixedly fastened in the back, output flange (18), main shaft bearing (19), electronic oil pump (20), driving gear (21), machine oil pipe (22), counter shaft bearing (23), main shaft (24), casing (25), guide bearing (26), base (27), it is characterized in that: fixedly connected with the external diameter bottom of casing (25) in the top of above-mentioned base (27), above-mentioned front end cover (4), the internal diameter of rear end cover (16) center hole is fixedlyed connected with the external diameter of main shaft bearing (19) respectively, front end cover (4), (3) are fixedly fastened by several respectively in rear end cover (16) inboard, (17) a fixedly connected driving gear that does not rotate (21), driving gear (21) center hole internal diameter is fixedlyed connected with the external diameter of guide bearing (26), above-mentioned main shaft (24) passes its external diameter middle part of main flying wheel (11) center hole fixedlys connected with the center hole internal diameter of main flying wheel (11), the front-end face of above-mentioned main flying wheel (11) vertically is drilled with several near the at interval equal equal angles in the position of wheel body outer rim along axle and penetrates the circular port of main flying wheel (11) wheel body to ear end face, each circular port internal diameter is fixedlyed connected with the external diameter of two counter shaft bearings (23) respectively, the internal diameter of per two counter shaft bearings (23) is fixedlyed connected with an external diameter middle part that penetrates the countershaft (13) of main flying wheel (11) wheel body respectively, seal by countershaft oil sealing (10) between the external diameter of the wheel body both ends of the surface of main flying wheel (11) and countershaft (13), main flying wheel (11) boring adds layer and is closed with flowable real object (7) by screw (12), above-mentioned several countershafts (13) stretch out the diameter of axle outside main flying wheel (11) the wheel body both sides and all pass the center hole of a secondary flying wheel (6) and fixedly connected with the center hole internal diameter of secondary flying wheel (6), the secondary flying wheel of above-mentioned several (6) is that inside has a hollow cylinder bodily form wheel that adds layer of the cylinder bodily form, the hollow layer impartial fixed angle in inside circumference outer rim interval that add installed several restricted baffles (8), hollow adding in the layer, be closed with flowable real object (7) by screw (9), the two end axles external diameter of above-mentioned several countershafts (13) passes the center hole of an actuation gear (14) respectively and fixedlys connected with the internal diameter of actuation gear (14) center hole, the fixedly connected countershaft hold-doun nut of the two axial ends external diameter of several countershafts (13) (15), main shaft (24) stretch out two outer side shaft external diameters of casing (25) housing respectively with front end cover (4), the internal diameter and the front end cover (4) of the bearing (26) of driving gear (21) the center hole internal fixation that rear end cover (16) inboard is fixedly connected, the internal diameter of the bearing (19) of rear end cover (16) center hole internal fixation is fixedly connected, above-mentioned several actuation gears (14) by with front end cover (4), the inboard fixing driving gear that does not rotate (21) engagement of rear end cover (16) realizes that power connects, front end cover (4), fixedly connected by screw (5) between rear end cover (16) and the casing (25), the fixing input flange dish (1) of main shaft (24) external diameter front end that stretches out casing (25) housing is fixedlyed connected with the external power source output shaft, the fixing output flange (18) in main shaft (24) external diameter rear end that stretches out casing (25) housing is fixedlyed connected with the load input shaft, front end cover (4), the outside, rear end cover (16) center portion fixed main shaft oil sealing (2), the external diameter sliding contact of the internal diameter of main shaft oil sealing (2) and main shaft (24), electronic oil pump (20) is fixed on rear end cover (16) exterior bottom by screw, the machine oil pipe (22) of electronic oil pump (20) is fixed on casing (25) housing inside bottom by screw, can the flow liquid level height of real object of casing (25) housing inside bottom filling does not contact several secondary flying wheels (6), leave suitable gap between several secondary flying wheels (6) and casing (25) the housing inboard, connect power initiation electronic oil pump (20) and be directly injected on the flank of tooth of several actuation gears (14) by machine oil pipe (22) import suction lubricant oil and by machine oil pipe (22) outlet.
2. the constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect according to claim 1 is characterized in that: described main flying wheel (11) center hole internal diameter is fixedlyed connected with main shaft (24) external diameter middle part.
3. the constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect according to claim 1 is characterized in that: described main flying wheel (11) wheel body end face at interval all equal angles connect the middle part of several countershafts (13) external diameter by bearing fixing along vertical several the circular port internal diameters that penetrate main flying wheel (11) wheel body that are drilled with of axle.
4. the constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect according to claim 1 is characterized in that: the center hole of described several secondary flying wheels (6) and several actuation gears (14) is fixedly connected to form several rotatable subsystems of several secondary flying wheels (6), several actuation gears (14) respectively with the axle external diameter of several countershafts (13).
5. the constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect according to claim 1 is characterized in that: described several countershafts (13) and several secondary flying wheels (6) are to accept the rotation that driving force that main shaft (24) transmits obtains two angular velocity components by fixing several actuation gears (14) of several countershafts (13) axle head and driving gear (21) engagement of not rotating.
6. the constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect according to claim 1 is characterized in that: the total kinetic energy E of described main flying wheel (11) and several secondary flying wheels (6)
tBy formula E
t=1/2 (I
1+ I
2) * (ω
1+ ω
2)
2Calculate.
7. the constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect according to claim 1, it is characterized in that: the boring of described main flying wheel (11) and several secondary flying wheels (6) adds layer to be injected less than the mobile real object (7) that adds layer capacity by oil hole, and oil hole tightens up sealing with screw (9), screw (12).
8. the constrained fluid inertia energy accumulating booster unit of a kind of double-speed superposition effect according to claim 7 is characterized in that: described main flying wheel (11) and several secondary flying wheels (6) hollow add layer inner circumferential edge at interval an impartial fixed angle several restricted baffles (8) are installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2007100851899A CN101265964B (en) | 2007-03-18 | 2007-03-18 | Double-speed superposition effect constrained fluid inertia energy accumulating booster unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2007100851899A CN101265964B (en) | 2007-03-18 | 2007-03-18 | Double-speed superposition effect constrained fluid inertia energy accumulating booster unit |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101265964A true CN101265964A (en) | 2008-09-17 |
| CN101265964B CN101265964B (en) | 2011-11-16 |
Family
ID=39988569
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2007100851899A Expired - Fee Related CN101265964B (en) | 2007-03-18 | 2007-03-18 | Double-speed superposition effect constrained fluid inertia energy accumulating booster unit |
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|---|---|
| CN (1) | CN101265964B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2481514C1 (en) * | 2011-12-05 | 2013-05-10 | Андрей Викторович Тимофеев | Method of increasing inertia drive of revolution and power drive to this end |
| CN103925334A (en) * | 2014-05-08 | 2014-07-16 | 南京工程学院 | Epicyclic gear train type inertia variable flywheel |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1307137A2 (en) * | 1985-12-23 | 1987-04-30 | И.М.Данильченко | Lag-pulse transmission |
| SU1665127A2 (en) * | 1989-04-11 | 1991-07-23 | И.М Данильченко | Inertial torque converter |
| CN1031219C (en) * | 1993-09-24 | 1996-03-06 | 刘起华 | Dynamic power transmission device |
| CN2663966Y (en) * | 2003-11-07 | 2004-12-15 | 中国第一汽车集团公司 | Inertia flywheel set |
| CN201013829Y (en) * | 2007-03-18 | 2008-01-30 | 董长军 | Restricting liquid inertia energy storage power compensating mechanism with double-speed additive effect |
-
2007
- 2007-03-18 CN CN2007100851899A patent/CN101265964B/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2481514C1 (en) * | 2011-12-05 | 2013-05-10 | Андрей Викторович Тимофеев | Method of increasing inertia drive of revolution and power drive to this end |
| CN103925334A (en) * | 2014-05-08 | 2014-07-16 | 南京工程学院 | Epicyclic gear train type inertia variable flywheel |
| CN103925334B (en) * | 2014-05-08 | 2016-08-17 | 南京工程学院 | Cyclic gear train type inertia variable fly wheel |
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| Publication number | Publication date |
|---|---|
| CN101265964B (en) | 2011-11-16 |
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