CN101994566B - Double-blade rotary motor - Google Patents
Double-blade rotary motor Download PDFInfo
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- CN101994566B CN101994566B CN2009100701142A CN200910070114A CN101994566B CN 101994566 B CN101994566 B CN 101994566B CN 2009100701142 A CN2009100701142 A CN 2009100701142A CN 200910070114 A CN200910070114 A CN 200910070114A CN 101994566 B CN101994566 B CN 101994566B
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- rotor
- double leaf
- leaf chip
- rotary engine
- blade
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Motor Or Generator Cooling System (AREA)
Abstract
The invention provides a novel rotary motor which can eliminate the defects of a piston reciprocating motor such as complicated structure, large volume, unstable operation, difficulty in acceleration and the like and can effectively overcome the defects of the existing triangular rotary motor such as great vibration, large noise, fast wear of parts, difficult maintenance, severe pollution and the like. In the invention, by virtue of a sealed air chamber composed of an elliptical inner chamber, group blades and a circular rotor, the rotor drives the blades to rotate in the elliptical inner chamber; by means of space difference between an elliptical long shaft and an elliptical short shaft, the operating period of the motor in four strokes is realized so as to finally form the double-blade rotary motor; graphite and a special cooling system are adopted for lubricating and cooling, thus solving the problem that high-temperature friction affects the service life of the parts; and gears and an eccentric shaft structure are not adopted, thus reducing noise and vibration, and achieving simpler and more reliable structure.
Description
Technical field
The invention relates to rotary engine, double runner rotor formula motor particularly, it is mainly used in the power plant of automotive field.
Background technique
Motor is the most key part of automobile, is the most important factor of decision automotive performance, just as human heart.What most people knew that we use always is the piston reciprocating type motor; Be divided into two-cycle engine and four stroke engine (following is example with the four stroke engine) again; A kind of well-known motor is arranged in addition, is exactly that rotary engine (Wankel Engine, Rotary Engine) is called miller cycle motor (Miller Cycle Engine) again.(Felix Wankel, 1902-1988) invention on results of previous studies, has solved key technology problems to this motor, succeeds in developing first rotary engine by German Fei Jiashi wankel.
Initial rotary engine adopts the compression that rotatablely moves control gaseous and the discharging of triangular rotor, and is far different with the straight line motion of traditional piston reciprocating type motor.General reciprocating motion type motor, piston is done linear reciprocating motion during work in cylinder, rotatablely moves in order to be converted into the straight line motion of piston, must use connecting rod.Rotary engine is then different, and it directly is converted into driving torque with the burning expansion power of combustible gas.Compare with Reciprocating engine, rotary engine has been cancelled useless straight line motion, thereby the rotary engine size of same power is less, and weight is lighter, and vibration and noise are lower, have greater advantage.The movement characteristic of rotary engine is the center of three-apexed rotor when revolving round the sun around the output shaft center, and three-apexed rotor itself is again around its center rotation.When three-apexed rotor rotates, be the ring gear at center and be the gear engagement at center with the three-apexed rotor center with the output shaft center, outputting power.
Above-mentioned kinematic relation makes the movement locus (being the shape of cylinder wall) on three-apexed rotor summit like the figure of eight.Three-apexed rotor is divided into three separate space to cylinder; Three spaces are successively accomplished air inlet, compression, acting and exhaust separately, and three-apexed rotor is from circling engine ignition acting three times; Yet compare double leaf chip rotary engine volume of the present invention with rotary polygonal piston engine little, in light weight; Well reduced vehicle's center of gravity and simple in structure, adopted number of parts to reduce, it is structurally more compact than rotary polygonal piston engine.Can export uniform moment of torsion, because the double runner rotor motor has a plurality of active chambers in running order simultaneously, so stressed even; Under the situation of high engine speeds running, move more stablely, the sealing of cavity has flexibility characteristics; So part long service life, air chamber belong to fully and isolate, good airproof performance; So just can solve the gas leakage problem that causes behind the triangular rotor engine scuffing, oil consumption more can not occur and increase and too much pollution.Rotary polygonal piston engine structurally can not occur and adopt eccentric shaft, problem such as the engine luggine that causes is big, and noise is big.
Summary of the invention
Adopt eccentric shaft to cause that number of parts is more, sealing is relatively poor, oil consumption is high, vibration is big in order to overcome the triangular rotor motor; The deficiency that noise is big; The present invention provides a kind of double leaf chip rotary engine that possesses piston reciprocating type motor and triangular rotor motor advantage; This double leaf chip rotary engine is not only simple in structure, compact, and output torque is even more, operation is more stable.
Double leaf chip rotary engine characteristics are: the elliptic stator inner chamber, and round rotor, retractable blades, this motor carries out air inlet, compression, acting, four actions of exhaust when work.
Double leaf chip rotary engine working procedure comprise group blade from airtight, the elliptical-intracavity wall is airtight with cooperating of rotor and group blade, forms the strange shape chamber of a sealing, respectively adds a cover two end cap up and down in the chamber of this sealing, realizes airtight cavity.
Group blade can slide in guide-track groove along with the variation of elliptical curvature automatically on double leaf chip rotary engine seal chamber when work rotor, realize the volume compression of airtight cavity.
High heat and high wearing and tearing will appear in double leaf chip rotary engine at work, be provided with cooling system and on rotor, will be provided with ventilated port and ventilation slot at the end cap up and down of this motor and rotor and central shaft.
Double leaf chip rotary engine blade in the running should guarantee to contact with the tight of bore of stator, one group of bar V-arrangement shell fragment is housed in the bottom of blade and between guide-track groove and blade, is provided with the oil impregnate crack.
The blade of double leaf chip rotary engine can rub with end cap and elliptic stator up and down in when work, and for guaranteeing the working life of each parts, end cap is equipped with graphite and blade is a high abrasion resisting material about motor.
Friction will take place so inlay the brass metal bar at the guide-track groove sidewall with the guide-track groove sidewall in double leaf chip rotary engine blade when motion, guarantee the working life of blade and rotor.
Description of drawings
Fig. 1 double leaf chip rotary engine overall structure figure:
Fig. 2 double leaf chip rotary engine cut-away view:
23: locking hole 24: blade 25: the shell fragment clip
26: closed cell 27: ventilation slot 28: ventilated port
29:V shape shell fragment 30: fixed bolt hole 31: graphite block
32: central shaft hole
Fig. 3 double leaf chip rotary engine blade guide-track groove structural drawing:
25: shell fragment clip 29:V shape shell fragment 33: brass tinsel
Fig. 4 double leaf chip rotary engine fundamental diagram:
A) engine compresses stroke motor suction stroke b)
C) engine exhaust strokes motor expansion stroke d)
Embodiment
The present invention includes motor body referring to Fig. 1 Fig. 2 and Fig. 4; Housing comprises stator 5 and motor upper end cap 9 motor lower end caps 3 compositions; Spark plug 10 is housed on the motor upper end cap, is positioned at the postive direction of the oval-shaped cavity XY plane projection profile central shaft Y of stator 5.Bearing 15 and bearing 15 is encapsulated on the motor upper end cap 9 by bearing cap 12 is equipped with Carburetor interface 19 bearings 17 and bearings 20 on the motor lower end cap, its middle (center) bearing 20 is encapsulated in it on motor lower end cap by bearing cap.
The upper and lower end of above-mentioned motor covers cooling unit is housed; On motor upper end cap 9 and motor lower end cap 3, be respectively equipped with the import and export 2 and 16 of cooling unit, cooling water will get into from the cooling water intake of lower end cap 3 and got back in the cooling water tank by the water-cooled mouth 16 on the motor upper end cap 9 at last along flow through motor stator 5 and motor upper end cap 9 of system pipeline during engine operation.
Above-mentioned rotor 7 is connected to the water-cooling circulating system of double leaf chip rotary engine through the particular bore on central shaft hole 32 inwalls, and rotor 7 both ends of the surface have ventilation slot 27, are uniformly distributed with ventilated port 28 in rotor center axis hole periphery, accelerates rotor 7 heat radiations.
Be distributed with six groups of blade guide-track grooves on above-mentioned engine rotor 7 circumference; 12 blades 24 are housed in the guide-track groove; Offset distance between the guide-track groove axis of symmetry and rotor center axis is 10-15mm, and there is certain angular relationship in the blade 24 when making rotor 7 rotations in the guide-track groove at specific position and engine center axis.Central shaft 14 drive rotors 7 rotate in the oval-shaped cavity of stator 5 during engine running, and central shaft is supported by bearing 15,17,20.
The blade 24 that above-mentioned rotor is equipped with on the rotor 7 when rotating is being pressed under the effect of centrifugal force, fluid pressure and V-arrangement shell fragment 29 on the elliptical-intracavity wall of motor stator 5; The difference of the length semiaxis of elliptical-intracavity should be not excessive, guarantees that velocity jump numerical value is in allowed band.Along with the variation of oval inwall curvature, the blade 24 of rotor 7 can be free to slide along guide-track groove.
The completion of above-mentioned action will realize forming by the seal chamber of oval inwall, round rotor, group blade, motor covers.
Above-mentioned seal chamber realizes that rear engine rotor banding moving vane when work rotates; Because the motor inner chamber is oval; So when rotor clockwise rotates; (blade 1 place is an initial position with diagram) increase in 0 ° of-90 ° of space, 90 ° of-180 ° of spaces reduce, 180 ° of-270 ° of spaces increase, 270 ° of-360 ° of spaces reduce, and the formation of space difference has realized the working procedure shown in figure below:
Aspirating stroke: Fig. 4-a black part is divided into the air chamber that contains oil gas mixing inflammable matter; 1 blade and mixed gas clockwise rotate with rotor; Volume increases gradually between blade 1 and the blade 2 when blade 1 turns over suction port, and the fluid inflammable gas gets into confined space, and air inlet is accomplished.
Compression stroke: Fig. 4-b black part is divided into oily mixing inflammable matter in the air chamber, blade 1 and reduce the gradually reduce indoor mixed gas of blade 2 when blade 1 clockwise direction of a last action rotates owing to the air chamber space, i.e. and compression is accomplished.
Expansion stroke: when gas is compressed to appropriate value, mixed gas arrives spark plug sparking place just, and spark plug is struck sparks simultaneously; Gas is lighted, and Fig. 4-c black part is divided into the air chamber that contains combustion gas, and combustion gas is known from experience promotion blade 2; The rotation of accelerating rotor; Because the space of air chamber increases, combustion gas also can become noenergy waste gas thereupon, and acting is accomplished.
Exhaust stroke: Fig. 4-d black part is divided into an air chamber and includes waste gas after burning, and a last action back promotes blade owing to the flywheel inertia rotors can be rotated further advances, and gets rid of the gas chamber waste gas, and exhaust is accomplished.
Rotor rotation one all plug ignitions six times, each Seal cage are accomplished the one action circulation.
Above-mentioned principle is that example is explained with two groups of blades only, and every group of blade is all in work in the reality.
Service behaviour is (laboratory data) relatively
Annotate: with discharge capacity four-stroke piston reciprocating type motor and double leaf chip rotary engine
Claims (9)
1. double leaf chip rotary engine; Comprise stator with oval-shaped cavity and the round rotor that is arranged in bore of stator; At the even six groups of blade guide-track grooves that distribute of rotor circumference; There are offset distance in guide-track groove symmetry axis and rotor centerline, in the two ends of rotor face has oil guide slot, seal groove, ventilated port, axis hole and rotor respectively, are provided with water-cooled circulation lumen pore, in the two side of blade guide-track groove the brass metal bar are housed; In the bottom of guide-track groove the V-arrangement shell fragment is housed, 12 blades of packing in the guide-track groove and can be free to slide along rotor radial.
2. double leaf chip rotary engine according to claim 1; It is characterized in that: the blade guide-track groove axis of symmetry that distributes on the rotor circumference and the offset distance between the rotor center axis are 10~15mm, and there is certain angular relationship in the blade when making the rotor rotation in the guide-track groove at specific position and double leaf chip rotary engine central axis.
3. double leaf chip rotary engine according to claim 1; It is characterized in that: be provided with cavity in the rotor; It is connected to the water-cooling circulating system of double leaf chip rotary engine through the particular bore on the rotor center shaft hole inner wall; The two ends of rotor face has ventilation slot, is uniformly distributed with ventilated port in rotor center axis hole periphery, accelerates the rotor heat radiation.
4. double leaf chip rotary engine according to claim 1; It is characterized in that: two brass metal bars are housed on the guide-track groove sidewall of rotor; Reduce the wearing and tearing of blade; Improve the working life of blade, be positioned at the guide-track groove bottom and the V-arrangement shell fragment be housed, the part radial force that provides blade and bore of stator closely to contact.
5. double leaf chip rotary engine according to claim 1; It is characterized in that: rotor blade adopts in groups and installs; Every group of two blades; Two blades closely contact with stator inner wall simultaneously, between two blades and bore of stator, form sealed gas chamber, pressure when having guaranteed double leaf chip engine compresses gas and the tightness between air chamber.
6. double leaf chip rotary engine according to claim 1 is characterized in that: the stator cavity adopts oval, and the difference of the length semiaxis of elliptical-intracavity should be not excessive, guarantees that velocity jump numerical value in allowed band, is provided with the water-cooled circulation port on stator.
7. double leaf chip rotary engine according to claim 1; It is characterized in that: the upper and lower end at double leaf chip motor is covered with the ventilated port that matches with rotor; At the interior edge face of end cap up and down graphite is housed, improves the life-span of rotor and end cap, reduce both frictions.
8. double leaf chip rotary engine according to claim 1 is characterized in that: the loam cake of double leaf chip motor is provided with the pairing hole that can connect with the water-cooled hole on the double leaf chip motor stator with covering down, connects the external refrigeration system.
9. double leaf chip rotary engine according to claim 1, it is characterized in that: spark plug is installed in the upper end cap of double leaf chip motor, is positioned at the postive direction of oval XY plane projection profile central shaft Y.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN2009100701142A CN101994566B (en) | 2009-08-11 | 2009-08-11 | Double-blade rotary motor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN2009100701142A CN101994566B (en) | 2009-08-11 | 2009-08-11 | Double-blade rotary motor |
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CN101994566A CN101994566A (en) | 2011-03-30 |
CN101994566B true CN101994566B (en) | 2012-12-05 |
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CN2009100701142A Expired - Fee Related CN101994566B (en) | 2009-08-11 | 2009-08-11 | Double-blade rotary motor |
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Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
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CN102213138B (en) * | 2011-04-06 | 2012-11-14 | 郎槟 | Elliptical sliding vane type engine |
CN104047711B (en) * | 2014-06-17 | 2016-08-24 | 曹瑞 | Gear type rotor engine |
CN104819052A (en) * | 2014-06-28 | 2015-08-05 | 蒋旭东 | Engine shell with good cooling performance |
CN104967237A (en) * | 2015-06-29 | 2015-10-07 | 蔡勇 | Rotor and rotor engine cooling system |
CN111946611B (en) * | 2020-08-09 | 2022-04-15 | 肇庆高新区伙伴汽车技术有限公司 | Baffle type slide machine |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1160811A (en) * | 1996-03-29 | 1997-10-01 | 唐禾天 | Vane rotor engine |
US6237560B1 (en) * | 1998-01-06 | 2001-05-29 | Saitoh & Co., Ltd. | Overexpansion rotary engine |
US6401687B1 (en) * | 1998-12-11 | 2002-06-11 | Arktur-Trading Gmbh | Axial rotary engine |
CN1414214A (en) * | 2001-10-26 | 2003-04-30 | 张长春 | Self-balanced rotor engine |
JP2006517273A (en) * | 2003-02-10 | 2006-07-20 | チラール,ジル サン | (Not mentioned in the translation) |
CN201092883Y (en) * | 2007-08-25 | 2008-07-30 | 陈昌全 | Rotary plate-type internal combustion engine |
CN201202526Y (en) * | 2008-05-30 | 2009-03-04 | 翟树球 | Vane rotor engine |
CN201560841U (en) * | 2009-08-11 | 2010-08-25 | 天津工程师范学院 | Double-vane type rotor engine |
-
2009
- 2009-08-11 CN CN2009100701142A patent/CN101994566B/en not_active Expired - Fee Related
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1160811A (en) * | 1996-03-29 | 1997-10-01 | 唐禾天 | Vane rotor engine |
US6237560B1 (en) * | 1998-01-06 | 2001-05-29 | Saitoh & Co., Ltd. | Overexpansion rotary engine |
US6401687B1 (en) * | 1998-12-11 | 2002-06-11 | Arktur-Trading Gmbh | Axial rotary engine |
CN1414214A (en) * | 2001-10-26 | 2003-04-30 | 张长春 | Self-balanced rotor engine |
JP2006517273A (en) * | 2003-02-10 | 2006-07-20 | チラール,ジル サン | (Not mentioned in the translation) |
CN201092883Y (en) * | 2007-08-25 | 2008-07-30 | 陈昌全 | Rotary plate-type internal combustion engine |
CN201202526Y (en) * | 2008-05-30 | 2009-03-04 | 翟树球 | Vane rotor engine |
CN201560841U (en) * | 2009-08-11 | 2010-08-25 | 天津工程师范学院 | Double-vane type rotor engine |
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Address after: 300222 Dagu South Road, Tianjin, No. 1310, No. Applicant after: Tianjin University of Technology and Education Address before: 300222 Dagu South Road, Tianjin, No. 1310, No. Applicant before: Tianjin Engineering Normal College |
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