CN2742143Y - Blade rotor engine - Google Patents
Blade rotor engine Download PDFInfo
- Publication number
- CN2742143Y CN2742143Y CN 200420035800 CN200420035800U CN2742143Y CN 2742143 Y CN2742143 Y CN 2742143Y CN 200420035800 CN200420035800 CN 200420035800 CN 200420035800 U CN200420035800 U CN 200420035800U CN 2742143 Y CN2742143 Y CN 2742143Y
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- CN
- China
- Prior art keywords
- rotor
- engine
- stator
- chamber
- blade
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model discloses a blade rotor engine, mainly comprising a stator, a rotor, an engine base, a bearing, an oil supply system and an ignition system. The blade rotor engine is characterized in that the inner surface of the stator comprises 4 cambered surfaces. Wherein, two of the cambered surfaces, the rotor and an output shaft are concentric circles, and the two of the cambered surfaces are divided into two unequal cavity chambers. The circumference of the rotor is provided with 4 deep slots and 4 shallow slots. Each deep slot is provided with 2 blades, and each shallow slot is provided with a radial sealing sheet. The end surface of the rotor is also provided with 2-3 sealing sheets. A spark plug is arranged on a sealing strip formed by the rotor and one cambered surface of the stator, so as to prevent gas mixture and fuel gas from mutually leaking. The oil supply system and the ignition system of the engine are similar with the oil supply system and the ignition system of the traditional reciprocating piston engine. As the capacities of the powering cavity chamber and the exhausting cavity chamber of the engine are larger than the capacities of the air-breathing cavity chamber and the compression cavity chamber, the blade rotor engine can prolong the intumescent period of the operating chamber and improve burning.
Description
[technical field]
The utility model relates to a kind of motor, is specifically a kind ofly to utilize combustion gas to burn the heat energy sent and be the rotary engine that medium becomes heat energy mechanical energy with gas in cylinder combustion.
[background technique]
At present, popular on the market motor generally is a reciprocating-piston engine, this engine structure complexity, volume is big, and Heavy Weight has particularly that vibration is big, the poisonous fume discharging is many, big for environment pollution, inefficient defective makes a lot of research institutions and researcher all in research, discussion, test new work engine, with weight reduction, reduced volume, raise the efficiency, reduce environmental pollution, reduce cost.Yet, up to the present, the motor of selling on the market, still based on reciprocating-piston engine, comparatively desirable new work engine did not also appear on the market.
[summary of the invention]
For overcoming the reciprocating-piston engine heaviness, volume is big, and vibration is big, and efficient is low, defective big for environment pollution, the utility model provide a kind of novel blade rotor engine, to improve the efficient of motor, reduce discharge of harmful gases, reduce vibration, reduce cost.
The technical solution adopted in the utility model is: the utility model comprises rotor, stator, blade, cylinder cap, support, bearing and oil supply system, ignition system, be characterized in: 1. the internal surface of motor stator is made up of 4 sections arc faces, be xx ', yy ', x ' y ', xy4 lonely face, xy wherein, lonely face of x ' y ' and rotor and output shaft are concentric circle, and be separated into the unequal A of volume by rotor, two chambers of B, lonely face of xx ' and rotor cylindrical are formed the A chamber, lonely face of yy ' and rotor cylindrical are formed the B chamber, and the volume of B chamber is greater than the volume of A chamber, the A chamber is used for air-breathing and compression (stroke), and the B chamber is used for work done and exhaust (stroke).2. engine rotor is the cylindrical body of a symmetry, and the rotary inertia of himself can replace flywheel, is provided with 4 road deep trouths on the circumference of rotor, 4 road shallow slots, 2 blades are housed in the per pass deep trouth, in the per pass shallow slot apex seal are housed, and apex seal only works in the x ' of stator y ' cambered surface; Both ends of the surface at rotor respectively are equipped with 2-3 road diaphragm seal, are the sealing strip (radially) between stator, rotor between the x ' of rotor and stator y ' cambered surface, the close plug of spark are housed, in case gas is revealed between two working rooms on this sealing strip.
The utility model beneficial effect is: 1. because the stator surface of this motor is designed to 4 cambered surfaces, and be separated into 2 unequal chambers of volume by rotor, and the volume of the chamber of work done and discharging is greater than air-breathing and volume compression chamber, therefore can prolong the phase of expansion of working room, improve burning, reduce discharge of harmful gases, reduce noise, help improving the efficient of motor.2. since epitrochanterian 4 cover blades and 4 diaphragm seals be installed in the groove of rotor, both ends of the surface at rotor also are provided with 2-3 road diaphragm seal, the close plug of spark is installed on the sealing strip between stator and rotor, therefore, sealing between the working room of motor and two working rooms is tightly reliable, helps improving the reliability of motor.
[description of drawings]
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is an overall structure schematic representation of the present utility model.
Fig. 2 is the sectional view of Fig. 1.
Fig. 3 is that four cambered surfaces and blade C, the D of stator inner surface among Fig. 1 is in the A chamber, and E, F are in the structural representation in B chamber.
Fig. 4 is that blade C, the D of Fig. 1 rotor is in the B chamber, and blade E, F are in the structural representation in A chamber.
Wherein: 1 rotor, 2 stators, 3 blades, 4 supports, 5 front covers, 6 rear end covers, 7 output shafts, 8 sliding pins, 9 sliding pin guide rails, 10 connecting plates, 11 cylinder caps, 12 fore bearings, 13 rear bearing covers, 14 front bearing retainers, 15 rear bearings, 16 apex seals, 17 vaporizers, 18 outlet pipes, 19 fuel tanks, 20 connecting bolts (band locating stud), 21 end sealing strips, 22 runner sealing sheets, the close plug of 23 sparks.
[embodiment]
With reference to accompanying drawing: on support (4), be fixed with stator (2), be provided with front cover (5) and rear end cover (6) in the front-end and back-end of stator, on the rear end of passing through front bearing retainer (14) and fore bearing (12) stator thereof on the front cover of stator, pass through rear bearing cover (13) and rear bearing (15) thereof, be fixed with a shaft (7), output shaft (7) is connected with rotor (1) and fixed plate (10) by spline, fixed plate (10) is provided with sliding pin (8), sliding pin (8) is used for the blade timing under the cooperation of sliding pin guide rail (9).On the circumference of rotor (1), be provided with 4 road deep trouths and 4 road shallow slots, two blades (3) are installed in the per pass deep trouth, apex seal (16) is installed in the per pass shallow slot, on stator inner surface, be provided with four sections cambered surfaces, be xx ', yy ', x ' y ', xy4 section cambered surface, xy wherein, x ' y ' cambered surface and rotor and output shaft belong to concentric circle, and be separated into unequal two chambers (being cylinder) A and B by rotor, and the volume of B chamber is greater than the volume of A chamber, cylinder cap (11) is arranged in stator and between the rotor, rotor and fixed plate fixedly are connected as a single entity by bolt (20) (band locating stud), be provided with vaporizer (17) at the suction port place of cylinder, exhaust ports at cylinder is provided with outlet pipe (18), be provided with oil tank (19) at the top of support, on the end face of rotor, be provided with 2-3 road end sealing strip (21), be provided with runner sealing sheet (22) between a plurality of blades on changeing and the deep trouth, the close plug of spark (23) is housed between the sealing strip of stator.
The working principle of this motor is: the oil supply system of motor, ignition system are similar to existing Reciprocating engine, by the work of Otto cycle principle.In its working procedure: the C in 4 blades, when the F blade enters working surface, as shown in Figure 2, D, the F blade face of deactivating, the C vacuum side of blade in A chamber is air-breathing, positive compression, meanwhile, the F face of blade exhaust in B chamber, back side work done, when the F blade moves to xy cambered surface section, when the C blade moves to x ' y ' cambered surface section, the rotor operation half cycle, respectively finish half cycles (totally four strokes), blade C, the F face of deactivating, blade D, E enter working surface, as shown in Figure 3, repeat said process, the blade timing; When blade C, F enter working surface xx ' respectively, during yy ' cambered surface section, the sliding pin of two ends of rotor (8) is with its release, and blade D, E are pinned, otherwise, when blade D, E enter working surface respectively, the sliding pin at two ends pins blade C, F, blade D, E is discharged, to adapt to the circulation requirement.Sealing, mainly be meant the sealing between the movement parts in the cylinder, each end face of rotor all adopts 2-3 road diaphragm seal (21) sealing between rotor and stator, reverse side adopts the light spring sheet to press to cylinder cap (11) end face, radial seal is adopted two kinds, a kind of is the interior table of blade and cylinder body, two blades in each deep trouth can slide mutually, to guarantee that two blades run to any section and can both be close to working surface by centrifugal force, another kind is that the apex seal of all blades all evenly distributes by circumference, when x ' y ' the cambered surface section of process stator, all seal, do not reveal mutually to guarantee mixed gas and combustion gas; In addition, between all blades and the chute by the sealing of separately diaphragm seal (22).
Claims (2)
1, a kind of blade rotor engine, mainly form by stator, rotor, blade, support, bearing and oil supply system, ignition system, it is characterized in that: the internal surface of motor stator is made up of 4 sections arc surfaces, be xx ', yy ', x ' y ', an xy4 cambered surface, wherein xy, x ' y ' cambered surface and rotor and output shaft are concentric circle, and be separated into two chambers of the unequal A of volume, B by rotor, xx ' cambered surface and rotor cylindrical are formed the A chamber, yy ' cambered surface and rotor cylindrical are formed the B chamber, and the volume of B chamber is greater than the volume of A chamber.
2, blade rotor engine according to claim 1, it is characterized in that: engine rotor is the cylindrical body of a symmetry, on the circumference of rotor, be provided with 4 road deep trouths, 4 road shallow slots, 2 blades are housed in the per pass deep trouth, in the per pass shallow slot apex seal is housed, and apex seal only works in the x ' of stator y ' cambered surface, 2-3 road diaphragm seal respectively is housed on the both ends of the surface of rotor, on the sealing strip between the x ' of rotor and stator y ' cambered surface, be provided with the close plug of spark, in case gas leaks between two chambers.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200420035800 CN2742143Y (en) | 2004-05-02 | 2004-05-02 | Blade rotor engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200420035800 CN2742143Y (en) | 2004-05-02 | 2004-05-02 | Blade rotor engine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN2742143Y true CN2742143Y (en) | 2005-11-23 |
Family
ID=35477614
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 200420035800 Expired - Fee Related CN2742143Y (en) | 2004-05-02 | 2004-05-02 | Blade rotor engine |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN2742143Y (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102116196A (en) * | 2011-02-25 | 2011-07-06 | 绍兴文理学院 | Vane type diesel engine |
CN111456846A (en) * | 2020-03-10 | 2020-07-28 | 魏善兆 | Fluid engine |
-
2004
- 2004-05-02 CN CN 200420035800 patent/CN2742143Y/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102116196A (en) * | 2011-02-25 | 2011-07-06 | 绍兴文理学院 | Vane type diesel engine |
CN111456846A (en) * | 2020-03-10 | 2020-07-28 | 魏善兆 | Fluid engine |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20051123 |