CN105134364A - Vortex air inlet engine - Google Patents
Vortex air inlet engine Download PDFInfo
- Publication number
- CN105134364A CN105134364A CN201510504525.3A CN201510504525A CN105134364A CN 105134364 A CN105134364 A CN 105134364A CN 201510504525 A CN201510504525 A CN 201510504525A CN 105134364 A CN105134364 A CN 105134364A
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- CN
- China
- Prior art keywords
- air inlet
- engine
- vortex
- air
- inlet disk
- 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.)
- Pending
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Classifications
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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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- Hybrid Electric Vehicles (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Abstract
A vortex air inlet engine is obtained by improving an air inlet system of an ordinary engine and utilizing the principle that the air pressure of a vortex area is lower than the air pressure in the normal state. In the air suction process of the engine, vortex generators can generate vortexes rotating at a high speed so that the pressure intensity in a cylinder can be much lower than the pressure obtained when air enters the ordinary engine, and more air can be sucked into the engine from an air inlet hole. The air inlet amount of the engine can be greatly increased, and accordingly the performance of the engine can be greatly improved. The larger the air inlet amount is, the less the fuel in use is, and the utilization rate of fuel can be greatly increased as well. By means of the vortex air inlet engine, the maximum output power of the engine can be greatly improved, and the engine can provide more powerful power.
Description
Technical field: a kind of novel motor, mainly contains the burning that advantage can optimize fuel oil, improves the performance of motor.Save a large amount of fuel oils.Effectively raise the utilization ratio of fuel oil, be conducive to protection of the environment.
Background technique: have larger improvement to the air inflow of motor in the past and intake method, air inflow increases, and intake method is slightly complicated.
Summary of the invention: vortex air intake motor is the gas handling system improving common engine, the eddy current that vortex generator can produce High Rotation Speed in engine suction process makes the pressure in cylinder more much lower than pressure during common engine air inlet, and motor can from the more air of inlet hole inspiration.The air inflow increase of motor can make the performance of motor be very significantly improved.The utilization ratio of fuel oil also can improve a lot.
During engine operation in Fig. 1, piston 2 reciprocates through 4 crank-rocker and drives pto＝power take-offs 3 to rotate, kinematic link 5 be connected with pto＝power take-off 3 and together with move.The lower end of kinematic link 5 is connected with 6 gears 1, drives 6 gears 1 to rotate.6 gear 1 and 7 gears 2 are mediated.7 gears 2 are connected with an axle, axle is fixing on the engine by two 8 struts, and ensure that axle can only rotate, axle is fixed two 10 cams, a cam is for controlling 9 outlet valves, and a cam is for controlling air inlet disk in 20.
The relation of 6 gear 1 and 7 gears 2 in Fig. 1 is that 6 gears 1 revolve 7 gears 2 that take two turns and rotate 1 circle.
The spring force that 9 outlet valves in Fig. 1 overcome self under the extruding of rotating cam realizes cut-offfing of outlet valve
In Fig. 1, the air inlet of motor to have in the sharp 13 eddy current dish 15 inlet hole 16 internal thread devices 17 of 10 cams 11 air inlet disk axle in air inlet disk axle 20 jointly complete.In 17, air inlet disk axle there is the screw thread in outside thread and 16 internal thread devices to match.16 internal thread devices are static all the time.10 cams air inlet disk axle in rotary push 17 under the drive of axle, in 17, air inlet disk axle moves together with air inlet disk in 20, and rotates a certain angle under the effect of 16 internal thread devices.At this moment 14 vortex generators and 15 inlet holes are left in 18 air inlet disk blocked areas of interior air inlet disk.Motor starts air inlet, piston upwards.After air inlet terminates, in air inlet disk axle and 20, air inlet disk gets back to operating position under the effect of own spring force in 17, and at this moment the blocked area of 18 air inlet disks shelters from 14 vortex generators and 15 inlet holes.Ensuing compressed action exhaust process is completed with rear engine.
Inlet hole and vortex generator can take scheme 15 inlet hole in Fig. 1 more bigger than 14 vortex generators, 14 vortex generators are placed on the inside of 15 inlet holes.Also the scheme in Fig. 2 can be taked 16 inlet holes and the side being placed on 15 vortex generators.
In Fig. 2, the air inlet of motor is identical with the air inlet principle of motor in Fig. 1, but in Fig. 1, the vortex air intake mode of motor can be formed in the cylinder evenly vortex air inlet effect meeting compared with the motor in Fig. 2 is efficiently better.
Accompanying drawing illustrates:
Fig. 1 is vortex air intake engine map
1 cylinder body
2 pistons
3 pto＝power take-offs
4 crank-rocker
5 kinematic links
6 gears 1
7 gears 2
8 struts
9 outlet valves
10 cams
11 eddy current dishes
12 jets
13 eddy current dishes
14 vortex generators
15 inlet holes
16 internal thread devices
Air inlet disk axle in 17
18 air inlet disk blocked areas
19 air inlet disk air inlet area
Air inlet disk in 20
Fig. 2 is vortex air intake valve figure
1 cylinder body
2 pistons
3 air inlets
4 exhausts
Air inlet disk axle in 5
6 internal thread devices
7 eddy current dishes
Air inlet disk in 8
9 exhaust valve pillars
10 internal thread walls
11 internal threads
Air inlet disk in 12
13 air inlet disk air inlet area
14 air inlet disk blocked areas
15 vortex generators
16 inlet holes
17 vortex generator rotating plate
18 vortex generator air outlet holes
Embodiment
The present invention designs the utilization ratio that can improve fuel oil in concrete enforcement, saves a large amount of fuel oils.The stronger motor in the faster vortex of rotating speed of motor only can the more air of inspiration.That is the fuel oil required for power that the higher generation of the rotating speed of motor is same is fewer.Interior air inlet disk can protect vortex generator, not by the impact of the High Temperature High Pressure produced during oil inflame, guarantees stable operation.
The present invention's design can make the maximum output of motor improve a lot.Motor can provide more powerful power.
Claims (6)
1. air inlet disk in 11 eddy current generation dishes 20 in Fig. 1,16 internal thread devices constitute the vortex intake system of vortex air intake motor jointly.
2. in Fig. 1, air inlet disk has 18 air inlet disk blocked areas in 20,19 air inlet disk air inlet area compositions.
3. 5 kinematic links in Fig. 1,6 gear 1,7 gear 2,8 struts, the air intake-exhaust of 10 cam composition vortex air intake motors controls.
4. 13 eddy current dishes in Fig. 1,14 are made up of vortex generator and 15 inlet holes.In 20, air inlet disk is arranged on inner side and can protects 14 vortex generators.
5. in Fig. 1,14 vortex generators are arranged on the inside of 15 inlet holes, and in figure bis-, 15 vortex generators are arranged on the adjacency of 15 inlet holes.
6. air inlet disk axle there are outside thread and 6 internal thread devices to match in 5 in Fig. 2, in moving up and down, guarantee that in 12, air inlet disk rotates a certain angle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510504525.3A CN105134364A (en) | 2015-08-18 | 2015-08-18 | Vortex air inlet engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510504525.3A CN105134364A (en) | 2015-08-18 | 2015-08-18 | Vortex air inlet engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105134364A true CN105134364A (en) | 2015-12-09 |
Family
ID=54719893
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510504525.3A Pending CN105134364A (en) | 2015-08-18 | 2015-08-18 | Vortex air inlet engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105134364A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2125517A1 (en) * | 1971-05-22 | 1973-02-22 | Maschf Augsburg Nuernberg Ag | PISTON ENGINE WITH FUEL INJECTION |
| JPS61108828A (en) * | 1984-10-29 | 1986-05-27 | ゼネラル モーターズ コーポレーシヨン | Adjustable vortex-flow generating means for internal combustion engine |
| US6065692A (en) * | 1999-06-09 | 2000-05-23 | Siemens Automotive Corporation | Valve seat subassembly for fuel injector |
| JP2002285845A (en) * | 2001-03-27 | 2002-10-03 | Kubota Corp | Swirl-chamber type combustion chamber for diesel engine |
-
2015
- 2015-08-18 CN CN201510504525.3A patent/CN105134364A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2125517A1 (en) * | 1971-05-22 | 1973-02-22 | Maschf Augsburg Nuernberg Ag | PISTON ENGINE WITH FUEL INJECTION |
| JPS61108828A (en) * | 1984-10-29 | 1986-05-27 | ゼネラル モーターズ コーポレーシヨン | Adjustable vortex-flow generating means for internal combustion engine |
| US6065692A (en) * | 1999-06-09 | 2000-05-23 | Siemens Automotive Corporation | Valve seat subassembly for fuel injector |
| JP2002285845A (en) * | 2001-03-27 | 2002-10-03 | Kubota Corp | Swirl-chamber type combustion chamber for diesel engine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20151209 |
|
| WD01 | Invention patent application deemed withdrawn after publication |