CN203035264U - Mini air power engine - Google Patents
Mini air power engine Download PDFInfo
- Publication number
- CN203035264U CN203035264U CN 201320050043 CN201320050043U CN203035264U CN 203035264 U CN203035264 U CN 203035264U CN 201320050043 CN201320050043 CN 201320050043 CN 201320050043 U CN201320050043 U CN 201320050043U CN 203035264 U CN203035264 U CN 203035264U
- Authority
- CN
- China
- Prior art keywords
- exhaust
- air
- air inlet
- power engine
- engine
- 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
Links
Images
Landscapes
- Valve-Gear Or Valve Arrangements (AREA)
Abstract
The utility model relates to an engine, in particular to a mini air power engine with compressed air as power. The mini air power engine comprises an engine body (10), a control system (100), a crank system (200), a chain wheel (11), an air inlet cavity (12), an engine body casing (13), a fixed frame (14), a main air inlet pipeline (15), an engine body end cover (16), a branch air inlet pipe (19) and an exhaust pipe (20). Pistons in the mini air power engine are radially and evenly distributed in an annular mode. Compared with other air engines, the mini air power engine is high in starting torque, simple in structure, convenient to operate, fast to lift, small in impact and low in air consumption.
Description
Technical field
The utility model relates to a kind of motor, in particular to a kind of be the miniature air power engine of power with pressurized air.
Background technique
Motor is widely used in all trades and professions, the Modern Traffic means of transportation such as automobile, steamer etc. in, generally adopt with the piston internal-combustion engine of fuel oil as power source.This employing fuel oil is insufficient because of oil inflame on the one hand as the motor of power source, contain a large amount of harmful matters and befouling environment in the feasible gas of discharging, because the fuel oil that uses is to refine to obtain from oil, the in short supply day by day of petroleum resources makes the development of fuel engine and utilization be subjected to increasing restriction on the other hand.Therefore develop new, clean, free of contamination alternative energy source, perhaps reduce fuel consume as much as possible, reduce discharging and become urgent problem in the motor development, just in time satisfied this requirement with pressurized air as the air-powered motor of power source.
The application's claimant discloses a kind of air power engine assembly that can be used for transport facility in its patent documentation CN101413403 A (its international application of the same clan is WO2010051668 A1), this motor comprises gas holder, air distributor, engine body, clutch, clutch, automatic transmission, differential mechanism and places the interior vane motor of exhaust chamber.This motor utilizes compressed air to do work and does not use any fuel, does not therefore have toxic emission, realized " zero-emission ", and recycling waste gas generates electricity, and has saved the energy, has reduced cost.But this motor is based on traditional four stroke engine, 720 ° of the every rotations of bent axle, and piston does work once.And can promote the piston acting as the pressurized air of power source can be in entering cylinder the time, and discharging then, namely the stroke of compressed air engine is actual is air inlet-expansion stroke and discharge stroke.Obviously, the disclosed this four-stroke compressed air engine of patent documentation CN101413403 A has been wasted effective expansion stroke greatly, has limited the efficient of motor.And the tail gas of this motor is failed recycling well, needs enough big gas holder deposit pressurized air could work the sufficiently long time.
Based on the existing problem of patent application CN101413403 A, the application's claimant is to disclose a kind of compressed air engine assembly with tail gas recycle loop in the application of China of 201110331809.9 at its application number, and this motor comprises cylinder, cylinder cap system, air inlet pipeline, gas exhaust piping, piston, connecting rod, bent axle, exhaust cam shaft, admission cam shaft, front gear box system and rear gear box.This motor utilizes compressed air to do work and does not use any fuel, does not therefore have toxic emission, realized " zero-emission ", and recycling waste gas does work, and has saved the energy, has reduced cost.But this motor is In-line multi-cylinder engine, in each the controller valve port in the controller controller valve only is installed, and under the certain situation of motor overall length, has limited cylinder cylinder number, thereby has limited the gross output of motor.Obviously, No. 201110331809.9 the disclosed this in-line multi-cylinder air-powered motor gross output of application is not high, and the configuration of motor still is worth exploring.
Be 201110331809.9 existing problems based on application number, the application's claimant is to disclose a kind of V-type multi-cylinder air-powered motor in the application of China of 201210063546.2 at its application number, comprising: multicylinder engine body, multicolumn body power distribution device, power equipment, controller system, air inlet control series flow control valve, compression gas tank group, constant voltage jar, electronic control unit ECU, pressurized air heating plant and the selectable second air feed loop.Be intended to solve output power problem and the recycling problem of tail gas of air-powered motor, thereby realize new type of compression air engine economic, efficient, zero-emission.But this motor is not high to compressed-air actuated utilization, and is bigger to compressed-air actuated demand during the piston cylinder acting.
The model utility content
Based on the problems referred to above, the utility model provides a kind of miniature air power engine, and it is slow to be intended to solve raising speed, and impact is bigger, the problem that air consumption is big.For this reason, the utility model adopts following technological scheme.
A kind of miniature air power engine, it comprises: engine body, control system, crankshaft system, sprocket wheel, body shell, body end cap, main admission line, a suction tude, outlet pipe, cylinder body.This miniature air power engine also comprises air-inlet cavity, when the throttle of motor is opened, pressurized air enters air-inlet cavity through heating plant heating back by main admission line, pressurized air in the air-inlet cavity is through a suction tude metering-in control system, and then the moving up and down of control piston cylinder inner carrier, the bent axle that drives simultaneously in the crankshaft system rotates.
Preferably, described engine body is installed on the fixing frame.
Preferably, described cylinder body is four in the such scheme, and the radial equipartition arrangement ringwise of main relatively admission line.
Preferably, described main admission line is connected on the air-inlet cavity in the such scheme, and air-inlet cavity is provided with four suction tude.
Preferably, an end of described suction tude is connected on the air-inlet cavity in the such scheme, and the other end is connected the top of cylinder body.
Preferably, described outlet pipe is arranged on the side of cylinder body in the such scheme.
Preferably, described control system comprises gas handling system, vent systems, intake and exhaust fixed base in the such scheme.
Preferably, described gas handling system comprises air inlet tappet, air inlet driving member, intake valve, admission line and air inlet controlling rod in the such scheme.
Preferably, described vent systems comprises exhaust controlling rod, exhaust tappet, exhaust rocker arm, exhaust duct and exhaust valve in the such scheme.
Preferably, described crankshaft system comprises bent axle, positioning bearing, intake cam, exhaust cam and crank in the such scheme.
Preferably, be provided with lubrication system in the described engine body in the such scheme.
Preferably, described lubrication system comprises in the such scheme, oil input channel, oil road, upwards oil duct, connecting rod lubrication oil duct, crankshaft lubrication oil duct, return tube, fine cleaner and oil sump.
In the such scheme preferably, be provided with jerk fuel injection pump in the described lubrication system, when motor begins air inlet work, bent axle in the crankshaft system rotates counterclockwise, jerk fuel injection pump is lubricated the cavity to control system, crankshaft system and piston in the suction of the lubricant oil in the oil sump pump housing, finally finishes lubricated lubricant oil and gets back in the oil sump by return tube.
Description of drawings
To describe now according to preferred but non-restrictive example of the present utility model, these and other features of the present utility model, aspect and advantage will become apparent when reading following detailed description with reference to the accompanying drawings, wherein:
Fig. 1 is miniature air power engine structural representation of the present utility model;
Fig. 2 is the structural representation according to the other direction of the miniature air power engine of Fig. 1 of the present utility model;
Fig. 3 is the plan view according to the miniature air power engine of Fig. 1 of the present utility model;
Fig. 4 is the plan view according to miniature air power engine among Fig. 1 of the present utility model;
Fig. 5 is the stereogram according to crankshaft system among Fig. 1 of the present utility model;
Fig. 6 is the sectional view according to Fig. 5 of the present utility model;
Fig. 7 is the left hand view according to Fig. 5 of the present utility model;
Fig. 8 is the right part of flg according to Fig. 5 of the present utility model;
Fig. 9 is the structural representation according to control system among Fig. 1 of the present utility model;
Figure 10 is the sectional view according to Fig. 9 of the present utility model;
Figure 11 is the sectional view according to intake valve assembly among Fig. 9 of the present utility model;
Figure 12 is the side view according to Fig. 9 of the present utility model;
Figure 13 is the plan view according to Fig. 9 of the present utility model;
Figure 14 is the air inlet phase diagram according to 1# piston cavity in the cylinder body among Fig. 1 of the present utility model;
Figure 15 is for beginning the phase diagram of air inlet according to 4# piston cavity in the cylinder body among Fig. 1 of the present utility model;
Figure 16 is for beginning the phase diagram of air inlet according to 3# piston cavity in the cylinder body among Fig. 1 of the present utility model;
Figure 17 is for beginning the phase diagram of air inlet according to 2# piston cavity in the cylinder body among Fig. 1 of the present utility model;
Figure 18 is the structural representation according to the preferred embodiment of the oil-way system of miniature air power engine of the present utility model;
Figure 19 is the sectional view according to the preferred embodiment of jerk fuel injection pump in the oil-way system of Figure 18.
Embodiment
The following description only is exemplary and be not in order to limit the disclosure, application or purposes in essence.Should be understood that in whole accompanying drawings, corresponding reference character is represented identical or corresponding components and feature.
With reference now to accompanying drawing,, Fig. 1, Fig. 2 are the structural representation of miniature air power engine of the present invention.As Fig. 1, shown in Figure 2, the miniature air power engine, it comprises: engine body 10, control system 100, crankshaft system 200, sprocket wheel 11, body shell 13, body end cap 16, main admission line 15, prop up suction tude 19, outlet pipe 20, cylinder body 21, when the throttle of motor is opened, pressurized air enters air-inlet cavity 12 through heating plant heating back by main admission line 15, pressurized air in the air-inlet cavity 12 is through suction tude 19 metering-in control system 100, and then the moving up and down of control piston cylinder inner carrier 18, the bent axle 211 that drives simultaneously in the crankshaft system 200 rotates, thus outputting power.
Further with reference to figure 1-Fig. 4, engine body 10 is mounted on the fixing frame 14 by bolt, wherein crankshaft system 200 links together by body end cap 16 sealings with the outside of cylinder body 21, and is provided with positioning bearing 17 between body end cap 16 and bent axle 211.Pressurized air in the gas holder feeds in the main admission line 15 in heating equipment heating back, enter pressurized air behind the admission line 15 and can enter in the air-inlet cavity 12 temporaryly, the pressurized air in the air-inlet cavity 12 can enter in the cylinder body 21 by a suction tude 19 according to the control of control system 100 and crankshaft system 200 subsequently.Air-inlet cavity 12 is connected the outside of cylinder body 21 by body shell 13 sealings, and sees shown in Figure 10 by a suction tude 19 with the piston cavity 105(of piston 18) communicate.Wherein control system 100 and a suction tude 19 are 4, and each control system 100 is installed one suction tude 19 and two outlet pipes 20.
With reference now to Fig. 5-Fig. 8,, Fig. 5 has described the structural representation according to crankshaft system 200 of the present invention.
Next with reference to figure 9-Figure 13, Fig. 9 is the structural representation of control system 100.Described control system 100 comprises: gas handling system, vent systems, intake and exhaust fixed base 132.Gas handling system comprises, air inlet tappet 133, air inlet driving member 134, intake valve 142, admission line 144 and air inlet controlling rod 145; Vent systems comprises, exhaust controlling rod 112, exhaust tappet 114, exhaust rocker arm 115, exhaust duct 116 and exhaust valve 118.
Introduce the working procedure of control system 100 in detail below with reference to Figure 10, Figure 12 and 13.The side of cylinder cap 103 is provided with admission line 144, and this admission line 144 and a suction tude 19(are as shown in Figure 3) be tightly connected.After engine start, bent axle 211 rotates, thereby the intake cam 216 and the exhaust cam 215 that drive on the bent axle 211 rotate thereupon.When intake cam 216 contacts with air inlet control bearing 130, air inlet controlling rod 145 on the air inlet control bearing 130 promotes air inlet tappets 133 and upwards rotates and then promote air inlet driving member 134 and promote intake valves 142 and leave intake valve cover for seat 143, the valve port of intake valve 142 is opened, pressurized air in the admission line 144 enters in the piston cavity 105, piston 18 compressed air push in the piston cavity 105, piston 18 in piston cavity 105 to lower slider, intake valve 142 is resisted against on the intake valve cover for seat 143 under the effect of air inlet little spring 139 and air inlet big spring 140 when air inlet control bearing 130 separates with intake cam 216, thereby the valve port of intake valve 142 is closed, and piston cavity 105 stops to feed pressurized air.
When bent axle 211 turns an angle exhaust cam 215 and exhaust control bearing 110 when contacting, exhaust control bearing 110 is installed on the exhaust controlling rod 112, exhaust tappet 114 is installed in the exhaust controlling rod 112, exhaust controlling rod 112 was pushed upwards and rotates when exhaust cam 215 contacted with exhaust control bearing 110, upwards rotated thereby promote exhaust tappet 114.When exhaust tappet 114 upwards rotates, exhaust rocker arm 115 on the exhaust tappet 114 is pressed the end of the valve stem of exhaust valve 118 downwards, exhaust valve 118 leaves exhaust valve cover for seat 117, the valve port of exhaust valve 118 is opened, piston 18 upwards slides, thereby the pressurized air in the piston cavity 105 is discharged from the valve port of exhaust valve 118, finally discharge by exhaust duct 116.When the piston 18 in the piston cavity 105 slides into peak, pressurized air in the piston cavity 105 is discharged from, exhaust cam 215 is separated with exhaust control bearing 110, exhaust valve 118 is got back in the exhaust valve cover for seat 117 under the effect of exhaust little spring 120 and exhaust big spring 121, vent closure on the exhaust valve 118, piston cavity 105 stops exhaust.Piston 18 is just according to above-mentioned process periodic duty.
Further with reference to Figure 10 and Figure 11, the internal structure of description control system 100 in further detail now.Control system 100 of the present invention comprises gas handling system, vent systems, intake and exhaust fixed base 132.
Gas handling system comprises: air inlet tappet 133, air inlet driving member 134, intake valve 142, admission line 144 and air inlet controlling rod 145.Air inlet controlling rod 145 places the square hole of exhaust controlling rod 112, and can slide up and down in the square hole of exhaust controlling rod 112; The lower end of air inlet controlling rod 145 is provided with air inlet control bearing 130, and air inlet control bearing 130 is by air inlet Control Shaft 131 lower ends that are installed in air inlet controlling rod 145 of consigning; The upper end of air inlet controlling rod 145 has circular groove.Air inlet tappet 133 has the rectangle of circular hole for the central position of upper end, the lower end is cylindrical body, hemisphere is processed in cylindrical end, and this hemisphere places in the circular groove of air inlet controlling rod 145 upper ends, and can sliding up and down and rotate with air inlet controlling rod 145 in circular groove.The upper end of air inlet tappet 133 is arranged in the square groove of air inlet driving member 134 lower ends, and link together by pivot pin and air inlet driving member 134, when air inlet controlling rod 145 upwards slides, meeting drive air inlet tappet 133 rotates and then can promote air inlet driving member 134 in the circular groove of air inlet controlling rod 145 and is offset to the right, air inlet driving member 134 can cover 135 with air inlet control and contacts when being displaced to certain position, thereby press the valve stem of intake valve 142, promote intake valve 142 and leave intake valve cover for seat 143, the valve port of intake valve 142 is opened feeding pressurized air.Intake valve 142 places cylinder cap 103, is connected with admission line 144 on the cylinder cap 103, and admission line 144 is provided with cylinder cap air inlet end cap 104 with the joint of cylinder cap 103.Cylinder cap 103 communicates with piston cavity 105, so when the valve port of intake valve 142 was opened, the pressurized air in the cylinder cap 103 can enter and promote piston 18 in the piston cavity 105 to lower slider.
The valve end of intake valve 142 is provided with air inlet locker sheet 137, and valve stem places in air inlet little spring 139 and the air inlet big spring 140, and air inlet little spring 139 and air inlet big spring 140 place in the air inlet spring seat 138; Air inlet locker sheet 137 is fixed on the air inlet end cap 136; The assembly body of air inlet locker sheet 137, valve stem, air inlet little spring 139 and air inlet big spring 140 places air inlet control to cover in 135.Wherein, valve stem and intake valve 142 joints are provided with air inlet oil sealing 141, and intake valve 142 is installed in the intake valve cover for seat 143.
Vent systems comprises: exhaust controlling rod 112,2 exhaust tappets 114,2 exhaust rocker arms 115,2 exhaust ducts 116 and 2 exhaust valves 118.Exhaust controlling rod 112 is the inner cylindrical body that has square through hole, two boards shape body is processed in its lower end, the middle part of tabular body has circular hole, be provided with exhaust control bearing 110 in the circular hole, exhaust control bearing 110 is consigned by the exhaust Control Shaft and 113 is installed in the circular hole of tabular body of exhaust controlling rod 112 lower ends; The end face symmetry on exhaust controlling rod 112 tops has two half slots.Exhaust tappet 114 is processed into hemispheroidal rod member for the bottom, and hemisphere places in the half slot on exhaust controlling rod 112 tops, and rotates along with swinging up and down of exhaust controlling rod 112; The top of exhaust tappet 114 is provided with exhaust rocker arm 115.The middle part of each exhaust rocker arm 115 is equipped with circular hole, and 2 exhaust rocker arms 115 link together by rocker-arm roller pin 101, and is fixed on the top of cylinder cap 103 by rocking arm fixed base 102; Exhaust rocker arm 115 is that an end has circular hole, and the other end is the plate that has circular arc, and by the upper end of circle hole sleeve at exhaust tappet 114, the arc surface that has the plate of circular arc contacts with the valve end of exhaust valve 118.
The valve end of exhaust valve 118 is provided with exhaust locker sheet 123, and valve stem places in exhaust little spring 120 and the exhaust big spring 121, and exhaust little spring 120 and exhaust big spring 121 place in the exhaust spring seat 122; The assembly body of exhaust locker sheet 123, valve stem, exhaust little spring 120 and exhaust big spring 121 is deflated rocking arm 115 and pushes down.Wherein, valve stem and exhaust valve 118 joints are provided with exhaust oil sealing 119, and exhaust valve 118 is installed in the exhaust valve cover for seat 117.The valve port of exhaust valve 118 communicates with exhaust duct 116, piston cavity 105, when exhaust valve 118 leaves exhaust valve cover for seat 117, the valve port of exhaust valve 118 is opened, piston cavity 105 inner carriers 18 upwards slide, thereby the pressurized air in the piston cavity 105 is extruded, discharged from exhaust duct 116 at last.
Introduce the working procedure of piston 18, i.e. the air inlet state of piston cavity with reference to figure 14-Figure 18 and in conjunction with Fig. 1, Fig. 5, Fig. 9.Intake cam 216 during engine body 10 startings on the bent axle 211 is controlled bearing 130 with the air inlet in the 1# piston cylinder and is contacted promotion air inlet controlling rod 145, and then promote air inlet tappet 133 and promote air inlet driving members 134 and press air inlet control and cover 135 and make intake valve 142 leave intake valve cover for seat 143, the valve port of intake valve 142 is opened gradually, and 20 degree that originally bent axle 211 rotates are the buffering course of piston 18.As shown in figure 14, the piston cavity 105 of 1# piston cylinder began to enter pressurized air after bent axle 211 turned over 20 degree, and when bent axle 211 turns over 70 when spending again, the intake valve 142 in the 1# piston cylinder is in full open position during this period, and piston cavity 105 enters pressurized air.The piston cavity of 1# piston cylinder only is in the air inlet state during bent axle 211 turns to 20 degree-90 degree in this process, and preceding 20 degree are in buffer status, 2 exhaust cams 215 contact with 2 exhaust control bearings 110 in this process, 2 exhaust tappets 114 are pushed, exhaust rocker arm 115 on 2 exhaust tappets 114 is pressed the valve stem of exhaust valve 118 downwards, 2 exhaust valves 118 are opened gradually, and the 3# piston cylinder is prepared exhaust.
As shown in figure 15, when bent axle 211 turns over 90 when spending again, bent axle 211 has rotated 180 degree.Intake valve 142 in the 1# piston cylinder is closed, piston cavity 105 stops to enter pressurized air, the piston cavity of 1# piston cylinder only is in the air inlet state during bent axle 211 turns to 90 degree-140 degree in this process, and the piston 18 in the 1# piston cylinder is in expansion acting state during 140 degree-160 degree, not air inlet, the 3# piston cylinder still is in exhaust condition.During 160 degree-180 degree, intake cam 216 is controlled bearing 130 with the air inlet in the 4# piston cylinder and is contacted promotion air inlet controlling rod 145, and then promote air inlet tappet 133 and promote air inlet driving members 134 and press air inlet control and cover 135 and make intake valve 142 leave intake valve cover for seat 143, the valve port of intake valve 142 is opened gradually, and 4# piston cylinder intake valve 142 in 180 degree is opened the preparation air inlet; During 160 degree-180 degree, 2 exhaust cams 215 contact with 2 exhaust control bearings 110,2 exhaust tappets 114 are pushed, exhaust rocker arm 115 on 2 exhaust tappets 114 is pressed the valve stem of exhaust valve 118 downwards, 2 exhaust valves 118 are opened gradually, and 2# piston cylinder exhaust valve 118 in 180 degree is opened the preparation exhaust.
As shown in figure 16, when bent axle 211 turns over 90 when spending again, bent axle 211 has rotated 270 degree.Intake cam 216 is controlled bearing 130 with the air inlet in the 3# piston cylinder and is contacted promotion air inlet controlling rod 145, and then promote air inlet tappet 133 and promote air inlet driving members 134 and press air inlet control and cover 135 and make intake valve 142 leave intake valve cover for seat 143, the valve port of intake valve 142 is opened gradually, the piston cavity 105 of 3# piston cylinder is in buffer status between 250 degree-270 degree, 3# piston cylinder exhaust valve 118 when 250 spend is closed and is stopped exhaust, and the intake valve 142 of 3# piston cylinder begins to open the preparation air inlet simultaneously.
As shown in figure 17, when bent axle 211 turns over 90 when spending again, bent axle 211 has rotated 360 degree.Intake cam 216 is controlled bearing 130 with the air inlet in the 2# piston cylinder and is contacted promotion air inlet controlling rod 145, and then promote air inlet tappet 133 and promote air inlet driving members 134 and press air inlet control and cover 135 and make intake valve 142 leave intake valve cover for seat 143, the valve port of intake valve 142 is opened gradually, the piston cavity 105 of 2# piston cylinder is in buffer status between 340 degree-360 degree, 2# piston cylinder intake valve 142 when 360 spend begins to open the preparation air inlet, 2# piston cylinder exhaust valve 118 when 360 spend is closed and is stopped exhaust, and the exhaust valve 118 of 4# piston cylinder begins to open the preparation exhaust simultaneously.
According to above-mentioned cyclic process, bent axle 211 constantly rotates, 1#, 2#, 3#, the periodic duty of 4# piston cylinder.
Last with reference to shown in the figure 18-19, Figure 18 is the structural representation of the lubrication system of motor of the present invention.
(the filled arrows direction is the direction that lubricant oil flows to Figure 18; The hollow arrow direction is the parts sense of rotation), it shows the structural representation of a preferred embodiment of the oil-way system of miniature air power engine.This oil-way system comprises: the control system 100 of motor, crankshaft system 200, intake cam 216, exhaust cam 215, piston 18, air-inlet cavity 12, oil sump 317, this oil-way system also comprise with crankshaft system 200 on be connected jerk fuel injection pump 400, utilize the pressure difference of air with the lubricant oil sucking-off in the oil sump 317, then from oil road 311 ejections, and then the cavity of control system 100, crankshaft system 200 and the piston 18 of motor is lubricated, the control system 100 directly over the body shell of jerk fuel injection pump 400 and motor is 45 degree directions and places.
Next consult Figure 19, it shows the sectional view of a preferred embodiment of jerk fuel injection pump 400 in the oil-way system of the present invention.Jerk fuel injection pump 400 comprises upper pump casing 411, lower pump body 417, filler opening 413, oil outlet 412, outlet valve 415, outlet valve valve seat 410 and plunger 420.Be provided with right side cavity 421 and left side cavity 422 in the upper pump casing 411; Upper pump casing 411 links together by joint 416 and lower pump body 417; Joint 416 is provided with seal ring with upper pump casing 411 and lower pump body 417 joints.Be equipped with outlet valve 415 in right side cavity 421 and the left side cavity 422, outlet valve 415 is resisted against in the outlet valve valve seat 410 by oil outlet valve spring 414; Right side cavity 421 communicates with filler opening 413, and left side cavity 422 communicates with oil outlet 412.Described lower pump body 417 is the inner housing that has cavity, and plunger 420 places in the cavity of lower pump body 417; Oil pump spring 418 is installed in the cavity of lower pump body 417, and is resisted against the top of the cavity of lower pump body 417 by plunger 420; The lower end of described plunger 420 is provided with roller 419.
When motor enters pressurized air and starts working from air-inlet cavity 12, bent axle on the crankshaft system 200 rotates counterclockwise, the intake cam 216 that connects by key on the bent axle is also along with rotating counterclockwise of bent axle 211 rotated, turn over 75 when spending at bent axle, lower pump body 417 upper rollers 419 of jerk fuel injection pump 400 slide into the basic circle disc of intake cam 216, owing to be provided with oil pump spring 418 in the plunger 420, so the elastic force lower plunger 420 at oil pump spring 419 moves downward, air in the upper pump casing 411 is drawn out of, the upper pump casing 411 inner pressure differences that produce, and then the outlet valve under the filler opening 413 415 presses to the inner chamber of outlet valve valve seat 410, and the lubricant oil in the oil sump 317 enters in the right side cavity 421 of upper pump casing 411 by oil input channel 310 sucking-off in the oil sump 317 filler opening 413 of flowing through after fine cleaner 316 removal of impurities.
After intake cam 216 rotates 240 degree, protruding disc and roller 419 on the intake cam 216 are inconsistent, make plunger 420 move upward, oil pump spring 418 is compressed, and the extruding force of oil pump spring 418 is pressed to the lubricant oil in the right side cavity 421 rapidly in the left side cavity 422 of upper pump casing 411.The outlet valve 415 that lubricant oil on the left of entering in the cavity 422 back down under the oil outlet 412 is opened, and the lubricant oil in the left side cavity 422 spray through oil road 311 from oil outlet 412 discharge currents rapidly.
It is logical that lubricant oil in the oil road 311 is divided into two path flow: the one tunnel is the oil duct 312 that makes progress, and another road is crankshaft lubrication oil duct 314.The oil duct 312 valve end in the lubricating engine control system 100 at first upwards, the lubricant oil that gets off from the valve end enters exhaust rocker arm 115, flows to exhaust tappet 114, air inlet tappet 133, intake cam 216, exhaust cam 215 and air inlet control bearing 130, exhaust control bearing 110 etc. successively along exhaust rocker arm subsequently.
The oil channel hole of lubricant oil in bent axle 211 in the crankshaft lubrication oil duct 314 enters 313 pairs of piston rods of connecting rod lubrication oil duct (not mark) and is lubricated, and the lubricant oil of the piston rod of flowing through is lubricated piston rod and bent axle 211 surface of contact simultaneously; The piston cavity that the lubricant oil that gets off from piston rod enters piston 18 is lubricated piston cavity.
Lubricant oil in the oil road 310 are flowed through after upwards each component lubrication of oil duct 312 and 314 pairs of motors of crankshaft lubrication oil duct is finished, and final lubricant oil falls in the engine body shell 13, gets back in the oil sump by the return tube 315 of body shell 13 bottoms again.When motor back and forth rotates, oil-way system to each parts of motor according to above-mentioned greasing circulating lubrication.
Although at length disclose the utility model with reference to the accompanying drawings, it should be understood that these descriptions only are exemplary, be not to limit application of the present utility model.Protection domain of the present utility model is limited by accessory claim, and can be included in various modification, remodeling and the equivalents of doing at the utility model under the situation that does not break away from the utility model protection domain and spirit.
Claims (13)
1. miniature air power engine, it comprises:
Engine body (10), control system (100), crankshaft system (200), sprocket wheel (11), body shell (13), body end cap (16), main admission line (15), prop up suction tude (19), outlet pipe (20), cylinder body (21), it is characterized in that: also comprise air-inlet cavity (12), when the throttle of motor is opened, pressurized air enters air-inlet cavity (12) through heating plant heating back by main admission line (15), pressurized air in the air-inlet cavity (12) is through suction tude (a 19) metering-in control system (100), and then the moving up and down of control piston cylinder inner carrier (18), the bent axle (211) that drives simultaneously in the crankshaft system (200) rotates.
2. miniature air power engine as claimed in claim 1, it is characterized in that: described engine body (10) is installed on the fixing frame (14).
3. miniature air power engine as claimed in claim 1, it is characterized in that: described cylinder body (21) is four, and main relatively admission line (15) ringwise radial equipartition arrange.
4. miniature air power engine as claimed in claim 1, it is characterized in that: described main admission line (15) is connected on the air-inlet cavity (12), and air-inlet cavity (12) is provided with four suction tude (19).
5. as claim 1 or 4 described miniature air power engines, it is characterized in that: an end of described suction tude (19) is connected on the air-inlet cavity (12), and the other end is connected the top of cylinder body (21).
6. miniature air power engine as claimed in claim 1, it is characterized in that: described outlet pipe (20) is arranged on the side of cylinder body (21).
7. miniature air power engine as claimed in claim 1, it is characterized in that: described control system (100) comprises gas handling system, vent systems, intake and exhaust fixed base (132).
8. miniature air power engine as claimed in claim 7, it is characterized in that: described gas handling system comprises air inlet tappet (133), air inlet driving member (134), intake valve (142), admission line (144) and air inlet controlling rod (145).
9. miniature air power engine as claimed in claim 7, it is characterized in that: described vent systems comprises exhaust controlling rod (112), exhaust tappet (114), exhaust rocker arm (115), exhaust duct (116) and exhaust valve (118).
10. miniature air power engine as claimed in claim 1, it is characterized in that: described crankshaft system (100) comprises bent axle (211), positioning bearing (213), intake cam (216), exhaust cam (215) and crank (219).
11. as claim 1-4, each described miniature air power engine among the 6-10, it is characterized in that: described engine body is provided with lubrication system in (10).
12. miniature air power engine as claimed in claim 11 is characterized in that: described lubrication system comprises: oil input channel (310), oil road (311), upwards oil duct (312), connecting rod lubrication oil duct (313), crankshaft lubrication oil duct (314), return tube (315), fine cleaner (316) and oil sump (317).
13. miniature air power engine as claimed in claim 11, it is characterized in that: be provided with jerk fuel injection pump (400) in the described lubrication system, when motor begins air inlet work, bent axle (211) in the crankshaft system (200) rotates counterclockwise, jerk fuel injection pump (400) is lubricated the cavity to control system (100), crankshaft system (200) and piston (18) in the suction of the lubricant oil in the oil sump (317) pump housing, finally finishes lubricated lubricant oil and gets back in the oil sump (317) by return tube (315).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320050043 CN203035264U (en) | 2013-01-30 | 2013-01-30 | Mini air power engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320050043 CN203035264U (en) | 2013-01-30 | 2013-01-30 | Mini air power engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203035264U true CN203035264U (en) | 2013-07-03 |
Family
ID=48687397
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320050043 Expired - Fee Related CN203035264U (en) | 2013-01-30 | 2013-01-30 | Mini air power engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203035264U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103967525A (en) * | 2013-01-30 | 2014-08-06 | 祥天控股（集团）有限公司 | Micro aerodynamic engine |
| CN114673561A (en) * | 2022-04-25 | 2022-06-28 | 重庆螺旋线科技发展有限公司 | Circumferential array type multi-cylinder pneumatic engine |
-
2013
- 2013-01-30 CN CN 201320050043 patent/CN203035264U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103967525A (en) * | 2013-01-30 | 2014-08-06 | 祥天控股（集团）有限公司 | Micro aerodynamic engine |
| CN114673561A (en) * | 2022-04-25 | 2022-06-28 | 重庆螺旋线科技发展有限公司 | Circumferential array type multi-cylinder pneumatic engine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| KR20140077806A (en) | Two-stroke air-powered engine assembly | |
| CN201262098Y (en) | Air power engine | |
| CN103244285A (en) | Control of engine with active fuel management | |
| CN203035264U (en) | Mini air power engine | |
| CN203035265U (en) | Control mechanism for mini air power engine | |
| CN203035266U (en) | Control mechanism for mini air power engine | |
| CN103216269B (en) | Control system of miniature air power engine | |
| CN101676538A (en) | Engine with multiple-level gas displacement | |
| CN103967525A (en) | Micro aerodynamic engine | |
| CN203978608U (en) | Asynchronous twin cylinder engine | |
| CN202467933U (en) | Valve timing mechanism for two-stroke aerodynamic V-shaped eight-cylinder engine | |
| CN202560383U (en) | Cylinder cover air valve distribution structure of air power engine | |
| CN203335166U (en) | Variable valve lift mechanism of automobile engine air distribution system | |
| CN104454158A (en) | Variable-stroke pneumatic internal combustion hybrid power engine and running method thereof | |
| CN103216268B (en) | The control mechanism of miniature air power engine | |
| CN204152573U (en) | A kind of novel twin cylinder engine distribution device | |
| CN103233779B (en) | Air intake and exhaust structure of rotary type engine | |
| JP6235152B2 (en) | Multifunctional variable valve drive system modularized for use in a 4-cylinder internal combustion engine | |
| CN203214115U (en) | Air intake and exhaust system of rotating engine | |
| CN202810948U (en) | Swing type variable multi-cylinder air power engine | |
| CN202810946U (en) | Air cylinder for variable multi-cylinder aerodynamic engine | |
| CN103291396B (en) | Air intake and exhaust system for rotary engine | |
| CN202811806U (en) | Link mechanism of engine | |
| CN103206278B (en) | The air distribution system of air-powered motor | |
| CN203962069U (en) | Synchronous twin cylinder engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130703 Termination date: 20170130 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |