CN2497044Y - Rotary piston rotor engine - Google Patents

Rotary piston rotor engine Download PDF

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Publication number
CN2497044Y
CN2497044Y CN 01247276 CN01247276U CN2497044Y CN 2497044 Y CN2497044 Y CN 2497044Y CN 01247276 CN01247276 CN 01247276 CN 01247276 U CN01247276 U CN 01247276U CN 2497044 Y CN2497044 Y CN 2497044Y
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China
Prior art keywords
rotor
cylinder body
grooves
piston
air
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Expired - Fee Related
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CN 01247276
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Chinese (zh)
Inventor
胡念国
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Individual
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Individual
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Priority to CN 01247276 priority Critical patent/CN2497044Y/en
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Publication of CN2497044Y publication Critical patent/CN2497044Y/en
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Abstract

The utility model provides a rotary piston rotor engine, and belongs to the field of heat energy power machine. The utility model includes a cylinder body; and a rotor, air blocking wheels and an air change channel arranged in the cylinder body. A piston whose outer end extends to the wall surface of the inner column in the cylinder body is arranged on the periphery of the rotor, a flute is arranged on the air blocking wheel, two grooves are arranged on the side wall of the rotor axially, the piston is connected fixedly on the periphery of the grooves, the air blocking wheels are respectively arranged in the two grooves through an air blocking wheel shaft. The air change channel is formed by air change grooves, and are connected with respective grooves, and arranged on the side wall of the rotor body, and air change cavities which can be connected with the two air change groove, and are correspondingly arranged on the inner wall of the cylinder body. A pair of meshing gears is arranged on the rotor shaft and on the end of the air blocking wheel shaft extending out of the cylinder body. The engine completes the process of air suction and compressing in an air compressing chamber, and completes the process of combustion and exhaust in a combustion chamber. The utility model has compact and simply structure, high work reliability, and can replace the present compound gear type internal-combustion engine.

Description

The rotary-piston rotator motor
Technical field:
The utility model relates to a kind of thermal power machine.What be particularly related to is a kind of rotary-piston type rotary engine.
Technical background:
Chinese patent CN2400574Y discloses a kind of " composite gear type internal-combustion engine ", is made of the complex wheel-tooth type gas compressor and the working machine of analog structure, and the high-pressure gas circuit passage of gas compressor is by the high-pressure gas circuit channel connection of one-way valve and working machine.The formation of its gas compressor comprises the closed shell of bringing gas port and high-pressure gas circuit passage into, be loaded on central gear and follower in the closed shell, be equipped with the little tooth of conjugation engagement on central gear and follower, also be provided with intermeshing canine tooth and big teeth groove on central gear and follower, canine tooth is separated into air-inlet cavity and compression chamber with closed shell; The formation of working machine comprise band high-pressure gas circuit passage and relief opening closed shell, be loaded on central gear and side wheel in the closed shell, on central gear and side wheel, be provided with intermeshing canine tooth and big teeth groove, canine tooth is separated into closed shell and fires chamber and exhaust cavity, also is provided with to lead to fluid fuel passage and the ignition mechanism that fires the chamber on closed shell.Its working principle is: the fresh charge that is entered by suction port is after the compression chamber compression of gas compressor, import the chamber that fires of working machine again through one-way valve, in firing the chamber, the fuel of being sent into by the fluid fuel passage fires under the effect of ignition mechanism, and the pressurized gas after firing promote the central gear rotation outputting power of working machine.The shortcoming one of the internal-combustion engine of this structural type is to fire the compressed gas in chamber respectively by failing " fresh charge " of the compression that comes from compression chamber and mixing formation by " fluid fuel " that the fluid fuel passage is sent into during firing the chamber, make its complex structure, make difficulty; The 2nd, the division surface sealing that the little tooth that is being rotated by the conjugation engagement between the compression chamber of compressor and the air-inlet cavity constitutes is not strong, makes the compression ratio of the gas in the compression chamber be difficult to reach requirement.In addition, the load mode by the one-way valve transmission is difficult to guarantee period of intake, easy break-down.
Summary of the invention:
The purpose of this utility model is that the internal-combustion engine to the said structure form improves, provide a kind of simple in structure, manufacture easily, rotary-piston rotator motor that Energy Efficiency Ratio is high.
The rotary-piston rotator motor of realizing the utility model purpose comprises and is provided with ignition mechanism, the cylinder body of combustion gas inlet hole and exhaust port, be located at rotor and retaining turbine and scavenge duct in the cylinder body, on the rotor periphery, be provided with at least one its outer end and stretch piston at cylinder body inner cylindrical wall face place, on the retaining turbine, have the groove that when rotating, passes through for piston, it is characterized in that described rotor the sidewall upper edge its axially have two grooves, described piston is fixed on the periphery of groove, described retaining turbine is installed in respectively in described two grooves by a retaining turbine axle parallel with rotor shaft, and retaining turbine surface and the surface of groove and airtight the touching of internal surface of cylinder body, described scavenge duct is equipped with pair of engaged gears by constituting with ventilation groove and the corresponding ventilation lumen that is communicated with two ventilation grooves that is located on the inboard wall of cylinder block that its groove communicates separately on the rotor body sidewall between two grooves that are arranged on rotor at a rotor shaft and an end that stretches out outside the cylinder body that keeps off the turbine axle.
The working principle of this rotary-piston rotator motor is as follows: two airtight chambers of inwall formation of the surface of the surface of epitrochanterian two grooves and two retaining turbines and two pistons and cylinder body, one of them is as compression air chamber, and another is as the burning air chamber.The combustion gas inlet hole then communicates with compression air chamber, and ignition mechanism and exhaust port then communicate with the burning air chamber.Rotor rotation during work, drive piston rotation, engaging gear on the rotor shaft drives the retaining turbine and rotates, the epitrochanterian piston that is in the compression air chamber meet with the groove that is docked at the retaining turbine in compression air chamber's groove and be able to by, after this piston turns over inlet hole, along with the rotation of piston towards compression air chamber's part of rotor steering direction, the volume of this part compression air chamber is reduced gradually, carry out compression process; Meanwhile, the volume of that part of compression air chamber of the another side of this piston then increases gradually, forms vacuum, and combustion gas is sucked in the compression air chamber, carries out breathing process; When meeting the requirements of compression ratio, epitrochanterian two ventilation grooves just in time go to the position of docking with the air-exchanging chamber of cylinder body, connect two ventilation grooves by air-exchanging chamber, and compressed gas then enters the burning air chamber through air-exchanging chamber, carries out gas exchange process; Rotation along with rotor, two ventilation grooves leave air-exchanging chamber, pathway closure between compression air chamber and the burning air chamber, gas exchange process finishes, ignition mechanism igniting this moment, produce high temperature and high pressure gas and promote the piston rotation in the fuel chamber and drive affixed with it rotor shaft to rotate, thereby realize the work by combustion process; The groove that is docked at the shelves turbine in the groove of burning air chamber in rotation process be in the piston of burning in the air chamber and meet and guarantee that it passes through.Along with the piston in the burning air chamber turns over relief opening, the burning air chamber and the relief opening that have before fired acting are connected, and waste gas is discharged from exhaust port, have realized exhaust process.Finish a work cycle.
Principle with existing multicylinder engine is the same, and being located at epitrochanterian piston can be uniform a plurality of piston.In such cases, divide the rotating ratio that is located at the engaging gear between rotor shaft and the retaining turbine axle then to be corresponding relation for number with piston.That is: when piston was two, the rotating ratio of engaging gear was 2: 1 then, made rotor rotation one circle, and the retaining turbine then rotates two circles, and two pistons all can be met with the groove of retaining turbine and pass through.The rest may be inferred by analogy.This is a sight of establishing a plurality of working rooms in a cylinder body, forms the single cylinder multiplex (MUX) and makes the cell structure form.Also can the high-power multicylinder engine of a plurality of such element of construction formation in parallel.Being arranged side by side a plurality of single cylinder multiplex (MUX)s on rotor sidewall makes chamber unit and can form many working rooms of multi-cylinder motor.
The utility model advantage compared with prior art is that air-breathing, compression work process are finished in compression air chamber, will burn and the exhaust work process in the firing chamber, finish.Simple and compact for structure, to manufacture easily, rate of fault is low, and compression ratio is realized easily, the functional reliability height.Alternative existing composite gear type internal-combustion engine uses.
Below in conjunction with drawings and Examples the utility model is described in further details.But content of the present utility model is not limited in the following example.
Description of drawings:
Fig. 1 structural representation of the present utility model
The left view of Fig. 2 Fig. 1
The A-A view of Fig. 3 Fig. 1
The B-B view of Fig. 4 Fig. 1
The C-C view of Fig. 5 Fig. 1
The structural representation of Fig. 6 cylinder body
The E-E view of Fig. 7 Fig. 6
The D-D view of Fig. 8 Fig. 6
The structural representation of Fig. 9 rotor
The F-F view of Figure 10 Fig. 9
Figure 11 air inlet station schematic representation
Figure 12 station schematic representation of taking a breath
Figure 13 ventilation finishing station schematic representation
Figure 14 burning, exhaust station schematic representation
Figure 15 embodiment 2 structural representation
The G-G view of Figure 16 Figure 15
The H-H view of Figure 17 Figure 15
Referring to Fig. 1-10, the formation of this rotary-piston rotator motor comprises the cylinder body 10 that is provided with ignition mechanism 15, combustion gas inlet hole 20 and exhaust port 17 and is located at the rotor 12 in the cylinder body 10 and keeps off turbine 16,29, it axially has two grooves 27,30 in the sidewall upper edge of rotor, piston 14 and 21 is fixed in respectively on the periphery of groove 27 and 30, and stretch at cylinder body inner cylindrical wall face place its outer end; Retaining turbine 16,29 is installed in respectively in groove 27 and 30 by a retaining turbine axle 3 parallel with rotor shaft 1, and surface and the surface of groove and airtight the touching of internal surface of cylinder body of retaining turbine, on the retaining turbine, have the groove 22,23 that when rotating, passes through, pair of engaged gears 7 and 6 are installed at a rotor shaft 1 and an end that stretches out outside the cylinder body that keeps off turbine axle 3 for piston 14,21.Described scavenge duct is constituted with ventilation groove 19,28 and the corresponding ventilation lumen 18 that is communicated with its two ventilations groove 19,28 that is located on the inboard wall of cylinder block that its groove communicates separately by two on the rotor body sidewall between two grooves that are arranged on rotor.2 and 9 is the left and right end cap of cylinder body among the figure, the 4th, and lid is connected on the top cover on the cylinder body 10, mainly plays to be involved in when protection retaining turbine does not adhere to dust or rotation other foreign material.8 for being installed in the driving wheel on the rotor shaft, and 31 for driving the cooling bath on rotor body.The groove of retaining on the turbine established by igniting, exhaust, the air-breathing working condition requirement several angle row that interlaces.The air chamber 13 that communicates with ignition mechanism 15 and exhaust port 17 is compression air chamber for burning air chamber, the air chamber 11 that communicates with inlet hole 20.Ignition mechanism 15 is spark plug in the present embodiment.
The working procedure of this motor is described below in conjunction with accompanying drawing:
One, intake process:
After compression air chamber's piston 21 turns over inlet hole 20 along with rotor, referring to Figure 11, compression air chamber is separated into two sealed space I and II by piston 21 and retaining turbine 29, along with rotating counterclockwise of piston 21, the volume of the space I of compression air chamber 11 increases and promptly produces negative pressure, combination gas in inlet hole 20 inspiration space I, meanwhile, the volume of space II reduces, and combustion gas wherein is compressed.What promptly carry out in the I of the space of compression air chamber 11 is the combustion gas breathing process, and what carry out in the II of space is the gas pressure compression process.
Two, gas exchange process:
Rotation along with rotor, on the rotor body two ventilation groove 19 and 28 goes to ventilation lumen 18 positions of cylinder body, the space II of compression air chamber communicates with burning air chamber 13, referring to Figure 12, two ventilation grooves leave ventilation lumen 18 after replacing the compressed gas among the II of space in the burning air chamber 13, passage between compression air chamber and the burning air chamber is closed, and referring to Figure 13, gas exchange process finishes.
Three, burning and gas-exhausting process:
The same with compression air chamber, rotation along with rotor, after burning air chamber piston 14 keeps off turbine groove 22 by the burning air chamber, the burning air chamber promptly is separated into two space III and IV by piston 14 and retaining turbine 16, referring to Figure 14, wherein space III is a sealed mode space that communicates with ignition mechanism 15, and space IV is an open type space that communicates with exhaust port 17.After compressed gas among the space I of compression air chamber is changed in the confined space III of burning air chamber, the ignition mechanism igniting, light the burning mixture among the III of space, produce high temperature and high pressure gas and promote 14 rotations in the counterclockwise direction of burning air chamber piston, thereby drive rotor shaft and rotate work done, realize the work by combustion process; The air chamber piston 14 that burns simultaneously will burn waste gas among the IV of air chamber space by exhaust port 17 discharges when rotating, realized exhaust process.
Along with the burning work done promotes the rotation that piston drives rotor shaft, gear on the rotor shaft 7 drives the gear 6 on the retaining turbine axle 3 of being installed in that is engaged with thereupon rotating, make retaining turbine axle drive the retaining turbine and rotate with the rotation of rotor.So go round and begin again, make motor constantly finish the internal combustion engine circulation of air-breathing, compression, ventilation, work by combustion, exhaust.
Embodiment 2:
Referring to Figure 15-17, present embodiment and preceding embodiment's structure is basic identical, different is in the burning air chamber uniform two pistons 32 and 33; Also uniform two pistons 34 and 35 in compression air chamber.Also be four in this corresponding ventilation groove.The velocity ratio of engaging gear 36,37 also corresponds to 2: 1.Working procedure is identical with preceding embodiment, repeats no more here.

Claims (1)

1, the rotary-piston rotator motor, comprise and be provided with ignition mechanism, the cylinder body of combustion gas inlet hole and exhaust port, be located at rotor and retaining turbine and scavenge duct in the cylinder body, on the rotor periphery, be provided with at least one its outer end and stretch piston at cylinder body inner cylindrical wall face place, on the retaining turbine, have the groove that when rotating, passes through for piston, it is characterized in that described rotor the sidewall upper edge its axially have two grooves, described piston is fixed on the periphery of groove, described retaining turbine is installed in respectively in described two grooves by a retaining turbine axle parallel with rotor shaft, and retaining turbine surface and the surface of groove and airtight the touching of internal surface of cylinder body, described scavenge duct is equipped with pair of engaged gears by constituting with ventilation groove and the corresponding ventilation lumen that is communicated with two ventilation grooves that is located on the inboard wall of cylinder block that its groove communicates separately on the rotor body sidewall between two grooves that are arranged on rotor at a rotor shaft and an end that stretches out outside the cylinder body that keeps off the turbine axle.
CN 01247276 2001-08-13 2001-08-13 Rotary piston rotor engine Expired - Fee Related CN2497044Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 01247276 CN2497044Y (en) 2001-08-13 2001-08-13 Rotary piston rotor engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 01247276 CN2497044Y (en) 2001-08-13 2001-08-13 Rotary piston rotor engine

Publications (1)

Publication Number Publication Date
CN2497044Y true CN2497044Y (en) 2002-06-26

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 01247276 Expired - Fee Related CN2497044Y (en) 2001-08-13 2001-08-13 Rotary piston rotor engine

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110159421A (en) * 2019-07-03 2019-08-23 吕国良 Piston, rotor internal-combustion engine, vehicle, aircraft and ship

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110159421A (en) * 2019-07-03 2019-08-23 吕国良 Piston, rotor internal-combustion engine, vehicle, aircraft and ship

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C19 Lapse of patent right due to non-payment of the annual fee
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