CN104100367A - Novel engine - Google Patents
Novel engine Download PDFInfo
- Publication number
- CN104100367A CN104100367A CN201410378152.5A CN201410378152A CN104100367A CN 104100367 A CN104100367 A CN 104100367A CN 201410378152 A CN201410378152 A CN 201410378152A CN 104100367 A CN104100367 A CN 104100367A
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- rotor
- intermediary
- cylinder body
- power
- cylinder
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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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- Supercharger (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
The invention discloses a novel engine. Active rotor cylinder bodies in petal-shaped distribution and active rotors are arranged in a cylinder body of the engine, an intermediary rotor is mounted in an intermediary rotor cylinder body, an annular compression chamber is reserved between each active rotor and the corresponding active rotor cylinder body, each active rotor is provided with strip racks, strip grooves are formed in the annular sidewall of the intermediary rotor, a fuel gas inlet and a waste gas outlet of each compression chamber are formed in the end wall of a front cylinder cover, an intake and exhaust adapter is mounted on the front cylinder cover, rotor shafts of the active rotors penetrate out of bearing holes on the periphery of a central shaft hole backwards, gears are mounted at penetrating-out ends of the rotor shafts of the intermediary rotor and the active rotors and are in star-shaped engagement, an inner gear ring is arranged on the peripheries of the gears, a flywheel is mounted behind the inner gear ring, and a power output shaft is mounted at the center of the rear wall of the flywheel. The novel engine has the advantages of compact structure, high output power and capability of utilizing various powers such as fuel and compressed gas by adopting the multi-cylinder design.
Description
Technical field:
The present invention relates to a kind of new work engine.
Background technique
Existing motor still exists many deficiencies, is first that used fuel is single, also to be compressed than restriction.The structure of existing motor is all very loaded down with trivial details in addition, and volume is very large, but the power of output is very limited.
Summary of the invention:
The technical problem to be solved in the present invention is to provide a kind of new work engine, and this motor has advantages of that compact structure, output power are large.
New work engine of the present invention by the following technical solutions.
The assembly of this new work engine comprises high-pressure pump, gas tank, throughput modulating valve, firing chamber, and intake and exhaust meet dish, front end housing, cylinder body, back cylinder cover and Hou great Gai.
In cylinder body, be provided with petal four symmetrical power rotor cylinder bodies, in each power rotor cylinder body, power rotor be housed respectively.Be intermediary's rotor cylinder in the center of power rotor cylinder body, intermediary's rotor cylinder is Open architecture, at intermediary's rotor cylinder, intermediary's rotor is housed.Between the outer wall of power rotor and the inwall of power rotor cylinder body, leave between annular compression, on power rotor outer wall, be axially arranged with two ribbon tooth bars, banded tooth bar outer surface is surrounded by diaphragm seal, banded tooth bar closely cooperates by diaphragm seal and power rotor cylinder body, the post side of intermediary's rotor and power rotor is tangent, on the annular sidewall of intermediary's rotor, be arranged with the strip groove matching with banded tooth bar, the periphery of intermediary's rotor and intermediary's rotor cylinder closely cooperate.Cylinder body front end is front end housing, and front end housing is by the sealing of cylinder body front end, and front end housing is provided with bearing support, and the rotor shaft front end of all power rotors and intermediary's rotor is arranged on bearing support.On the end wall of front end housing, be provided with fuel gas inlet and waste gas outlet between every section of compression; Every group of fuel gas inlet and waste gas outlet one end communicate with the two ends between compression in corresponding power rotor cylinder body respectively, the other end of all fuel gas inlet and waste gas outlet converges respectively, intake and exhaust are housed on front end housing and connect dish, fuel tube and outlet pipe connect dish from intake and exhaust and outwards pass; Fuel tube is connected with firing chamber, throughput modulating valve, gas tank, high-pressure pump, and multistage worm gear compressor is connected with gas tank.
The rear portion of cylinder body is back cylinder cover, and rear end of the cylinder block is sealed by back cylinder cover; Back cylinder cover is provided with multiple bearing holes, and the bearing hole from central shaft hole periphery of the rotor shaft of power rotor passes backward, at the traversing through end of intermediary's rotor and power rotor rotor shaft, gear is housed, all gear star engagements.Periphery at gear is provided with ring gear, and the gear that is positioned at periphery engages with ring gear.At ring gear rear side, flywheel is housed, flywheel is connected with ring gear bolt by periphery bolt hole, and pto＝power take-off is equipped with in the rear wall center of flywheel; After back cylinder cover, Hou great Gai is housed, above-mentioned flywheel and ring gear cover in rear large lid, and pto＝power take-off is protruding from the center hole of Hou great Gai.
The working principle of new work engine of the present invention is that the pressurized gas that motor is provided by high-pressure pump start, burning by fuel in firing chamber drives engine revolution, and waste gas is discharged and formed pressurized gas by worm gear multi-stage booster and enter gas tank and realize air re-circulation.Power is provided by four power rotors, is delivered to gear-box below by rotor shaft, and the synchronous multiple gears of size ensure synchronous operation transmission, then in increasing by imperial palace circulation tooth, torque drives output shaft output.Drive four rotors by the pressurized gas in firing chamber, inverse expansion power is born by transition rotor.By discharging work done waste gas, waste gas forms recirculation by worm wheel pressure booster.
The advantage of new work engine of the present invention is owing to adopting multi-cylinder design, can adopt the multiple power such as fuel, pressurized gas, has advantages of that compact structure, output power are large.
Brief description of the drawings
Below in conjunction with the drawings and specific embodiments, the present invention is described in detail.
Fig. 1 is the exploded view at left of the present invention visual angle.
Fig. 2 is the structural representation at cylinder body front-end face place in Fig. 1.
Fig. 3 is the structural representation at rear end of the cylinder block face place in Fig. 1.
Number in the figure:
1, high-pressure pump 2, gas tank 3, throughput modulating valve 4, firing chamber 5, intake and exhaust connect dish
6, front end housing 7, cylinder body 8, back cylinder cover 9, rear large lid 10, power rotor cylinder body
11, between power rotor 12, intermediary's rotor cylinder 13, intermediary's rotor 14, compression 15, banded tooth bar
16, strip groove 17, bearing support 18, fuel gas inlet 19, waste gas outlet 20, fuel tube
21, outlet pipe 22, multistage worm gear compressor 23, gear 24, ring gear 25, flywheel
26, pto＝power take-off 27, rotor shaft.
Embodiment
Example
As shown in Figure 1, Figure 2, Figure 3 shows, the assembly of this new work engine comprises high-pressure pump 1, gas tank 2, throughput modulating valve 3, firing chamber 4, and intake and exhaust connect dish 5, front end housing 6, cylinder body 7, back cylinder cover 8 and rear large lid 9.
In cylinder body 7, be provided with petal four symmetrical power rotor cylinder bodies 10, in each power rotor cylinder body 10, power rotor 11 be housed respectively.Be intermediary's rotor cylinder 12 in the center of power rotor cylinder body 10, intermediary's rotor cylinder 12 is Open architecture, at intermediary's rotor cylinder 12, intermediary's rotor 13 is housed.Between the outer wall of power rotor 11 and the inwall of power rotor cylinder body 10, leave between annular compression 14, on power rotor 11 outer walls, be axially arranged with two ribbon tooth bars 15, banded tooth bar 15 outer surfaces are surrounded by diaphragm seal, banded tooth bar 15 closely cooperates by diaphragm seal and power rotor cylinder body 10, intermediary's rotor 13 is tangent with the post side of power rotor 11, on the annular sidewall of intermediary's rotor 13, be arranged with the strip groove 16 matching with banded tooth bar 15, the periphery of intermediary's rotor 13 and intermediary's rotor cylinder 12 closely cooperate.Cylinder body 7 front ends are front end housing 6, and front end housing 6 is by cylinder body 7 front end sealings, and front end housing 6 is provided with bearing support 17, and rotor shaft 27 front ends of all power rotors 11 and intermediary's rotor 13 are arranged on bearing support 17.On the end wall of front end housing 6, be provided with between every section of compression 14 fuel gas inlet 18 and waste gas outlet 19; Every group of fuel gas inlet 18 and waste gas outlet 19 one end respectively with the interior compression of corresponding power rotor cylinder body 10 between 14 two ends communicate, the other end of all fuel gas inlet 18 and waste gas outlet 19 converges respectively, intake and exhaust are housed on front end housing 6 and connect dish 1, fuel tube 20 and outlet pipe 21 connect dish 1 from intake and exhaust and outwards pass; Fuel tube 20 is connected with firing chamber 3, throughput modulating valve 4, gas tank 2, high-pressure pump 1, and multistage worm gear compressor 22 is connected with gas tank 2.
The rear portion of cylinder body 7 is back cylinder cover 8, and cylinder body 7 rear ends are sealed by back cylinder cover 8; Back cylinder cover 8 is provided with multiple bearing holes, and the bearing hole from central shaft hole periphery of the rotor shaft 27 of power rotor 11 passes backward, at the traversing through end of the rotor shaft 27 of intermediary's rotor 13 and power rotor, gear 23 is housed, all gear 23 stars engagements.Be provided with ring gear 24 in the periphery of gear 23, the gear 23 that is positioned at periphery engages with ring gear 24.At ring gear 24 rear sides, flywheel 25 is housed, flywheel 25 is connected with ring gear 24 bolts by periphery bolt hole, and pto＝power take-off 26 is equipped with in the rear wall center of flywheel 25; Large lid 9 after being equipped with after back cylinder cover 8, above-mentioned flywheel 25 and ring gear 24 cover in rear large lid 8, and pto＝power take-off 26 is protruding from the center hole of Hou great Gai 8.
Claims (1)
1. a new work engine, it is characterized in that: the assembly of this new work engine comprises high-pressure pump (1), gas tank (2), throughput modulating valve (3), firing chamber (4), intake and exhaust connect dish (5), front end housing (6), cylinder body (7), back cylinder cover (8) and rear large lid (9); In cylinder body (7), be provided with petal symmetrical four power rotor cylinder bodies (10), power rotor (11) is housed respectively in each power rotor cylinder body (10), be intermediary's rotor cylinder (12) in the center of power rotor cylinder body (10), intermediary's rotor cylinder (12) is Open architecture, at intermediary's rotor cylinder (12), intermediary's rotor (13) is housed; Between the outer wall of power rotor (11) and the inwall of power rotor cylinder body (10), leave (14) between annular compression, on power rotor (11) outer wall, be axially arranged with two ribbon tooth bars (15), banded tooth bar (15) outer surface is surrounded by diaphragm seal, and banded tooth bar 15 closely cooperates by diaphragm seal and power rotor cylinder body (10); Intermediary's rotor (13) is tangent with the post side of power rotor (11), on intermediary's rotor (13) sidewall, be arranged with banded tooth bar (15) and mate the strip groove (16) engaging, the periphery of intermediary's rotor (13) and intermediary's rotor cylinder (12) closely cooperate; Cylinder body (7) front end is front end housing (6), front end housing (6) seals cylinder body (7) front end, front end housing (6) is provided with bearing support (17), and rotor shaft (27) front end of all power rotors (11) and intermediary's rotor (13) is arranged on bearing support (17); On the end wall of front end housing (6), be provided with fuel gas inlet (18) and the waste gas outlet (19) of (14) between every section of compression; Every group of fuel gas inlet (18) and waste gas outlet (19) one end respectively with in corresponding power rotor cylinder body (10) between compression the two ends of (14) communicate, the other end of all fuel gas inlet (18) and waste gas outlet (19) converges respectively, intake and exhaust are housed on front end housing (6) and connect dish (1), fuel tube (20) outlet pipe (21) connects dish (1) from intake and exhaust and outwards passes; Fuel tube (20) is connected with firing chamber (3), throughput modulating valve (4), gas tank (2), high-pressure pump (1), and multistage worm gear compressor (22) is connected with gas tank (2); The rear portion of cylinder body (7) is back cylinder cover (8), and cylinder body (7) rear end is sealed by back cylinder cover (8); Back cylinder cover (8) is provided with multiple bearing holes, the bearing hole from central shaft hole periphery of the rotor shaft (27) of power rotor (11) passes backward, at intermediary's rotor (13) and power rotor rotor shaft (27) traversing through end, gear (23) is housed, the engagement of all gears (23) star; Be provided with ring gear (24) in the periphery of gear (23), the gear (23) that is positioned at periphery engages with ring gear (24); At ring gear (24) rear side, flywheel (25) is housed, flywheel (25) is connected with ring gear (24) bolt by periphery bolt hole, and pto＝power take-off (26) is equipped with in the rear wall center of flywheel (25); Hou great Gai (9) is housed after back cylinder cover (8), above-mentioned flywheel (25) and ring gear (24) cover in Hou great Gai (8), and pto＝power take-off (26) is protruding from the center hole of Hou great Gai (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410378152.5A CN104100367B (en) | 2014-08-04 | 2014-08-04 | A kind of new work engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410378152.5A CN104100367B (en) | 2014-08-04 | 2014-08-04 | A kind of new work engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104100367A true CN104100367A (en) | 2014-10-15 |
| CN104100367B CN104100367B (en) | 2016-08-24 |
Family
ID=51668850
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410378152.5A Active CN104100367B (en) | 2014-08-04 | 2014-08-04 | A kind of new work engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104100367B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09264152A (en) * | 1996-03-28 | 1997-10-07 | Shiro Onishi | Rotary piston type internal combustion engine |
| CN1281527A (en) * | 1998-12-02 | 2001-01-24 | 金昌钧 | Reciprocating rotary piston system and pressure pump and IC engine using same |
| US20040088981A1 (en) * | 2000-10-16 | 2004-05-13 | Ollis William Henry | Rotary drive mechanism |
| CN101360899A (en) * | 2005-11-23 | 2009-02-04 | 文吉恩斯动力公司 | Internal combustion engine |
| CN101900028A (en) * | 2009-05-27 | 2010-12-01 | 杨焕利 | Multipurpose energy converter |
| CN204163852U (en) * | 2014-08-04 | 2015-02-18 | 杨焕利 | A kind of new work engine |
-
2014
- 2014-08-04 CN CN201410378152.5A patent/CN104100367B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09264152A (en) * | 1996-03-28 | 1997-10-07 | Shiro Onishi | Rotary piston type internal combustion engine |
| CN1281527A (en) * | 1998-12-02 | 2001-01-24 | 金昌钧 | Reciprocating rotary piston system and pressure pump and IC engine using same |
| US20040088981A1 (en) * | 2000-10-16 | 2004-05-13 | Ollis William Henry | Rotary drive mechanism |
| CN101360899A (en) * | 2005-11-23 | 2009-02-04 | 文吉恩斯动力公司 | Internal combustion engine |
| CN101900028A (en) * | 2009-05-27 | 2010-12-01 | 杨焕利 | Multipurpose energy converter |
| CN204163852U (en) * | 2014-08-04 | 2015-02-18 | 杨焕利 | A kind of new work engine |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104100367B (en) | 2016-08-24 |
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