CN203702261U - Novel rotor engine - Google Patents
Novel rotor engine Download PDFInfo
- Publication number
- CN203702261U CN203702261U CN201320868968.7U CN201320868968U CN203702261U CN 203702261 U CN203702261 U CN 203702261U CN 201320868968 U CN201320868968 U CN 201320868968U CN 203702261 U CN203702261 U CN 203702261U
- Authority
- CN
- China
- Prior art keywords
- rotor
- rotating vane
- seal
- engine
- shaped
- 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
Landscapes
- Rotary Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The utility model discloses a novel rotor engine which comprises an engine shell, rotary vane shafts, rotary vanes, a main shaft and a rotor, where an air inlet and an air outlet are formed in the engine shell; a sparking plug is arranged on the engine shell; the two ends of the cylindrical engine shell are sealed with end covers; a rail is arranged at the inner wall of each end cover; the rotor and the main shaft are coaxially arranged in the shell; multiple rotary vane grooves are uniformly distributed in the radial direction on the rotor; a rotary vane shaft and a rotary vane are arranged in each rotary vane groove in a sliding manner; two sides of each rotary vane shaft are embedded in the rail on each end cover and matched with the rail in a sliding manner. According to the novel rotor engine, the technical problem that the seal sheet of a traditional rotor engine is quickly abraded and poor in sealing performance is overcome; by supporting each rotary vane shaft in the rail on each end cover, the rotor slides along a track and the over abrasion of a seal sheet is avoided; and meanwhile, by embedding a seal ring in a ring-shaped seal groove, the sealing performance of the engine cavity is improved; the novel rotor engine has the characteristic of small size, good sealing performance, high compressing ratio, low production cost and good practicality.
Description
Technical field
The utility model relates to technical field of engines, is specifically related to a kind of New rotor engine.
Background technique
At present, rotary polygonal piston engine has entered the practical stage.Although rotary polygonal piston engine has some feature of reciprocating engine and gas turbine concurrently, but, between the adjacent cavity volume due to three-apexed rotor engine, only has an apex seal, apex seal is that line contacts with cylinder body all the time, and the position contacting with cylinder body on apex seal is changing all the time, therefore three non-isolation completely in firing chamber, apex seal quick abrasion.Engine easily causes gas leakage problem because of oil sealing fret wear after using a period of time, significantly increases oil consumption and pollution.Its unique mechanical structure also causes the more difficult maintenance of this class engine.
Summary of the invention
The purpose of this utility model is to overcome the deficiencies in the prior art part, and a kind of durable, good sealing effect firm in structure, a kind of New rotor engine that compression ratio is high are provided.
The purpose of this utility model is achieved through the following technical solutions:
A kind of New rotor engine, comprise motor body, rotating vane axle and rotating vane, main shaft and rotor, motor body is provided with suction port, relief opening and spark plug, the two ends of described motor body cylindraceous are sealed with end cap, this end cap inwall is provided with track, the inner chamber of described motor body is column equidistant curve body, in housing, be coaxially arranged with rotor and main shaft, on described rotor, radial equipartition is shaped with multiple rotating vane grooves, is slidably fitted with rotating vane axle and rotating vane in rotating vane groove, and the both sides of this rotating vane axle are flush-mounted in the track on end cap and are slidably matched with it.
And, described rotating vane is made up of blade axis hole, blade, seal groove and diaphragm seal, multiple rotating vanes are installed in rotating vane groove, and with in rotating vane groove, multiple rotating vanes being installed, with being connected by blade triangle chock between adjacent two rotating vanes in rotating vane groove, rotating vane and housing joint are shaped with multiple seal grooves, and seal groove is connected with diaphragm seal by stage clip, and diaphragm seal forms and seals moving cooperation with housing inner chamber, described blade bottom is provided with blade axis hole.
And, described rotor end-face periphery is coaxially shaped with annular seal groove, in this annular seal groove, be embedded with multiple seal rings, between adjacent two rotating vanes, multiple seal rings are installed, and adjacent two seal rings adopt concavo-convex embedding structure to connect, wherein a side sealing ring is shaped with projection, and opposite side seal ring is shaped with blind slot, and sealing stage clip is installed in blind slot.
And described rotor end-face is uniform is shaped with multiple Cooling Holes.
And described track end face is shaped with oil leab.
Advantage of the present utility model and economic effect are:
1, the utility model has overcome the technical barrier of conventional rotors motor diaphragm seal quick abrasion, poor sealing, by rotating vane axle is supported in the track on end cap, rotor is slided along track, has avoided the inordinate wear of diaphragm seal; Meanwhile, by the seal ring of setting-in in annular seal groove, improved the sealing in engine cavity; The utlity model has that volume is little, good airproof performance, high, the cheap feature of compression ratio, there is good practicability.
2, the utility model is by the blade triangle chock being slidably installed between adjacent two diaphragm seals in same rotating vane groove, in the time that rotor banding motive sealing sheet rotates, triangle chock can be adjusted diaphragm seal height in time, diaphragm seal and housing inner chamber and both sides end cap is formed and seal moving cooperation.
3, the annular seal groove that the utility model is coaxially shaped with by rotor end-face periphery matches with seal ring, can effectively improve the sealing between rotor and both sides end cap.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 be the utility model rotor stereogram;
Fig. 3 is the structural scheme of mechanism of the utility model housing;
Fig. 4 is the structural representation of the utility model end cap;
Fig. 5 is the structural representation of the utility model rotating vane;
Fig. 6 is the left view of the utility model rotating vane;
Fig. 7 is the structural representation of the utility model seal ring.
Embodiment
For further understanding content of the present utility model, Characteristic, hereby exemplify following examples, and coordinate accompanying drawing to be described in detail as follows.It should be noted that, the present embodiment is descriptive, is not determinate, can not limit thus protection domain of the present utility model.
Shown in Fig. 1-7, a kind of New rotor engine, comprise motor body 1, rotating vane axle 4 and rotating vane 5, main shaft 7 and rotor 3, motor body is provided with suction port 10, relief opening 9 and spark plug 8, the two ends of described motor body cylindraceous are sealed with end cap 12, this end cap inwall is provided with track 13, the inner chamber of described motor body is column equidistant curve body, in housing, be coaxially arranged with rotor and main shaft, on described rotor, radial equipartition is shaped with multiple rotating vane grooves 14, in rotating vane groove, be slidably fitted with rotating vane axle and rotating vane, the both sides of this rotating vane axle are flush-mounted in the track on end cap and are slidably matched with it.
And, described rotating vane is made up of blade axis hole 19, blade 20, seal groove 17 and diaphragm seal 15, multiple rotating vanes are installed in rotating vane groove, and with in rotating vane groove, multiple rotating vanes being installed, between adjacent two rotating vanes, be connected by blade triangle chock 21, rotating vane and housing joint are shaped with multiple seal grooves, and seal groove is connected with diaphragm seal by stage clip 16, described blade bottom is provided with blade axis hole, and diaphragm seal forms with housing inner chamber, and sealing is moving to be coordinated.Described rotor end-face periphery is coaxially shaped with annular seal groove 2, in this annular seal groove, be embedded with multiple seal rings 22, between adjacent two rotating vanes, multiple seal rings are installed, and adjacent two seal rings adopt concavo-convex embedding structure to connect, wherein a side sealing ring is shaped with projection 23, opposite side seal ring is shaped with blind slot 18, and sealing stage clip 24 is installed in blind slot.Described rotor end-face is uniform is shaped with multiple Cooling Holes 6.Described track end face is shaped with oil leab 11.
Action principle of the present utility model is: in the time that rotating vane forwards suction port position to rotor, air inlet finishes, and between last rotating vane, form a seal space, along with the rotor rotary seal space air that diminishes is gradually compressed, starting point kerosene gas explosion combustion acting in the time that last blade turns over spark plug.Combustion gas simultaneously.Circulation successively, next working procedure starts.
Claims (5)
1. a New rotor engine, comprise motor body, rotating vane axle and rotating vane, main shaft and rotor, motor body is provided with suction port, relief opening and spark plug, it is characterized in that: described motor body is cylindric and two ends end cap seals, this end cap inwall is provided with track, the inner chamber of described motor body is column equidistant curve body, in housing, be coaxially arranged with rotor and main shaft, on described rotor, radial equipartition is shaped with multiple rotating vane grooves, in rotating vane groove, be slidably fitted with rotating vane axle and rotating vane, the both sides of this rotating vane axle are flush-mounted in the track on end cap and are slidably matched with it.
2. a kind of New rotor engine according to claim 1, it is characterized in that: described rotating vane is made up of blade axis hole, blade, seal groove and diaphragm seal, multiple rotating vanes are installed in rotating vane groove, and with in rotating vane groove, multiple rotating vanes being installed, between adjacent two rotating vanes, be connected by blade triangle chock, rotating vane and housing joint are shaped with multiple seal grooves, seal groove is connected with diaphragm seal by stage clip, described blade bottom is provided with blade axis hole, and diaphragm seal forms with housing inner chamber, and sealing is moving to be coordinated.
3. a kind of New rotor engine according to claim 1, it is characterized in that: described rotor end-face periphery is coaxially shaped with annular seal groove, in this annular seal groove, be embedded with multiple seal rings, between adjacent two rotating vanes, multiple seal rings are installed, and adjacent two seal rings adopt concavo-convex embedding structure to connect, wherein a side sealing ring is shaped with projection, and opposite side seal ring is shaped with blind slot, and sealing stage clip is installed in blind slot.
4. a kind of New rotor engine according to claim 1, is characterized in that: described rotor end-face is uniform is shaped with multiple Cooling Holes.
5. a kind of New rotor engine according to claim 1, is characterized in that: described track end face is shaped with oil leab.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201320868968.7U CN203702261U (en) | 2013-12-26 | 2013-12-26 | Novel rotor engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201320868968.7U CN203702261U (en) | 2013-12-26 | 2013-12-26 | Novel rotor engine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN203702261U true CN203702261U (en) | 2014-07-09 |
Family
ID=51052716
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201320868968.7U Expired - Fee Related CN203702261U (en) | 2013-12-26 | 2013-12-26 | Novel rotor engine |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN203702261U (en) |
-
2013
- 2013-12-26 CN CN201320868968.7U patent/CN203702261U/en not_active Expired - Fee Related
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2478803C2 (en) | Rotary piston internal combustion engine | |
WO2013077776A3 (en) | Six-stroke rotary engine and operating method thereof | |
RU2009115121A (en) | ROTOR-PISTON INTERNAL COMBUSTION ENGINE | |
CN202091036U (en) | Turbine rotor engine | |
CN110195645B (en) | Multi-cylinder rotor engine | |
CN203702261U (en) | Novel rotor engine | |
CN103233782B (en) | Cock-type rotary compression expansion mechanism | |
CN103670520A (en) | Novel rotary engine | |
CN107448281A (en) | Oval engine | |
CN203515794U (en) | Vane engine | |
CN106121810A (en) | A kind of Wankel engine of Ratios | |
CN101852123A (en) | Cycloid rotor engine | |
CN204783255U (en) | Drum formula combined engine | |
CN204511648U (en) | The air-cooled petrol engine of blade type based on elliptic stator | |
CN202789516U (en) | Oil-gas recovery pump | |
CN103821610A (en) | Rotary piston engine | |
CN104295395A (en) | Piston mechanism assembly | |
KR101161685B1 (en) | rotary engine | |
RU188307U1 (en) | ENGINE | |
RU2330973C1 (en) | Rotary-piston internal combustion engine | |
CN203796403U (en) | Novel piston engine | |
CN104963766A (en) | Cylinder type combination engine | |
RU2659639C1 (en) | Rotary piston internal combustion engine | |
CN203584571U (en) | Rotary engine | |
CN105179076A (en) | Curved surface track cylinder body 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 | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140709 Termination date: 20181226 |