CN109139242A - Tangential force engine and its core component - Google Patents
Tangential force engine and its core component Download PDFInfo
- Publication number
- CN109139242A CN109139242A CN201811094266.1A CN201811094266A CN109139242A CN 109139242 A CN109139242 A CN 109139242A CN 201811094266 A CN201811094266 A CN 201811094266A CN 109139242 A CN109139242 A CN 109139242A
- Authority
- CN
- China
- Prior art keywords
- rotating wheel
- shell
- anger
- combustion chamber
- tangential force
- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/02—Pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/16—Admission or exhaust passages in pistons or outer members
-
- 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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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
The present invention provides a kind of tangential force engine and its core component, comprising: shell has air inlet and exhaust outlet；Rotating wheel is located in shell, and rotating wheel can be rotated axially, and rotating wheel includes: rotating wheel ontology, and the cross section of rotating wheel ontology is circle；At least one combustion chamber, combustion chamber are set on the excircle of rotating wheel ontology；It calms the anger part, part of calming the anger is arranged corresponding to combustion chamber, and part of calming the anger can be rotated axially, closes or opens combustion chamber and changes the opening direction of combustion chamber；And put forth effort part, it is set on shell；Wherein, air inlet, shell, to put forth effort cavity that part and rotating wheel ontology surround be inlet chamber, exhaust outlet, shell, to put forth effort the cavity that part and rotating wheel ontology surround be discharge chamber, and the volume of inlet chamber is less than the volume of discharge chamber.Tangential force engine structure is simple, and mechanical friction is small, the little energy consumed during acting, meanwhile, expansion ratio is greater than compression ratio, and fuel efficiency is high.
Description
Technical field
The present invention relates to engine art more particularly to a kind of tangential force engines and its core component.
Background technique
There are piston type reciprocating movement engine, the prevailing engines such as turbine turbofan engine on the market at present.Piston reciprocating
Campaign-styled engine is to convert rotary power by crankshaft for the straight reciprocating motion of piston to export, turbine turbofan engine
It is high temperature and high pressure gas to be stamped on the blade of rotary shaft and be converted into rotary power output.
Piston type reciprocating movement engine includes piston, the crank link mechanism connected on piston, crankshaft, timing mechanism,
The moving components such as valve actuating mechanism.Moving component is more, and mechanical friction is big, and the energy consumed during acting is more.In addition, conventional
The compression ratio of piston-mode motor is equal with expansion ratio, and fuel efficiency is not high.There is a kind of Atkinson motor on the market at present,
Output it uses more complicated connecting rod as power from piston to crankshaft is cooperated with different rod mechanisms, is made
It is different to obtain each stroke amplitude, so that expansion ratio is greater than compression ratio, fuel efficiency is than conventional piston type reciprocating movement engine
Want high.But complicated connecting rod is in volume and fault condition is all not so good as conventional piston type reciprocating movement engine, so failing
It is universal.It is very high to engine material and processing request although turbine turbofan engine structure is simple, at present mainly in aviation
It is used in field.
Summary of the invention
Complicated to solve engine structure, the thermal efficiency is low, the not high problem of fuel efficiency, and the present invention provides a kind of tangential
Force engine and its core component.
The present invention provides a kind of core component of tangential force engine, comprising: shell has air inlet and exhaust outlet；Rotation
Runner is located in shell, and rotating wheel can be rotated axially, and rotating wheel includes: rotating wheel ontology, and the cross section of rotating wheel ontology is circle
Shape；At least one combustion chamber, combustion chamber are set on the excircle of rotating wheel ontology；It calms the anger part, part of calming the anger is set corresponding to combustion chamber
It sets, part of calming the anger can be rotated axially, closed or opened combustion chamber and changed the opening direction of combustion chamber；And put forth effort part, it is set to outer
On shell；Wherein, air inlet, shell, to put forth effort cavity that part and rotating wheel ontology surround be inlet chamber, exhaust outlet, puts forth effort part at shell
And the cavity that rotating wheel ontology surrounds is discharge chamber, the volume of inlet chamber is less than the volume of discharge chamber.
Further, part of calming the anger includes calm the anger part main body and rotary shaft, and part main body of calming the anger and rotary shaft are integrally formed, rotation
Axis is mounted on rotating wheel ontology.
Further, part of calming the anger further includes rotating member, and rotating member includes: curved bar, and it is separate that one end of curved bar is set to rotary shaft
The one end for part main body of calming the anger；Curved bar directive wheel, one end set on curved bar far from rotary shaft；And spring, it is placed in rotary shaft, bullet
One end of spring is fixed on rotating wheel ontology, and the other end of spring is fixed on curved bar.
Further, shell is equipped with guide rail close to the circumference of inlet chamber, and curved bar directive wheel slides on guide rail.
Further, shell further includes partition, and partition is for separating air inlet and exhaust outlet.
Further, partition is opposite with the position of part on the shell is puted forth effort.
Further, the quantity of combustion chamber is two, position phase of two combustion chambers on the excircle of rotating wheel ontology
It is right.
Further, putting forth effort part close to the side in the shell center of circle is arc, put forth effort part installation thickness inside the shell be by
It is gradually increased.
The present invention also provides a kind of tangential force engine, the core component including tangential force engine described above,
Tangential force engine further include: igniter, igniter include spark plug, high-tension ignition electrode and by electrode, high pressure
Ignitor is set on shell, and spark plug is set in combustion chamber, is set on rotating wheel ontology by electrode, and electrical with spark plug
Connection；And atomizer, set on shell on the circumference of inlet chamber.
The beneficial effects of the present invention are:
More compared to the moving component of piston-mode motor, mechanical friction is big, and the energy consumed during acting is more, cuts
There was only rotating wheel ontology to force engine and two moving components of part of calming the anger, so structure is simple, mechanical friction is being done work with regard to small
The little energy consumed in the process, the thermal efficiency are high.In addition, the volume due to inlet chamber is less than the volume of discharge chamber, compression stroke is small
It is less than expansion ratio in the compression ratio of expansion stroke, tangential force engine, more kinetic energy can be exported.Relative to expansion ratio and pressure
Than equal engine, the fuel efficiency of tangential force engine is higher for contracting.
Detailed description of the invention:
Fig. 1 is the present invention when the first combustion chamber rotates near partition, the cross-sectional view of tangential force engine；
Fig. 2 is the present invention when the rotation of the first combustion chamber passes through partition, the diagrammatic cross-sectional view of tangential force engine；
Fig. 3 is the present invention after rotation of the first combustion chamber is by partition, the cross-sectional view of tangential force engine；
Fig. 4 is the structural schematic diagram of of the invention calm the anger part and rotating member.
Specific embodiment:
It is described below and is served only for disclosing the present invention so that those skilled in the art can implement the present invention.In being described below
Embodiment be only used as illustrating, it may occur to persons skilled in the art that other obvious are deformed.It defines in the following description
Basic principle of the invention can be applied to other embodiments, deformation scheme, improvement project, equivalent program and other do not carry on the back
Other schemes from spirit and scope of the invention.
As shown in Figure 1, Figure 2 and Figure 3, a kind of core component of tangential force engine, including shell 1, there are two the tools of shell 1
Opening, air inlet 111 and exhaust outlet 112.Shell 1 includes partition 2, and partition 2 is for separating air inlet 111 and exhaust outlet 112
It opens, partition 2, which is mounted on shell 1, to be integrally formed with shell 1.
As shown in Figure 1, Figure 2 and Figure 3, the core component of tangential force engine further includes rotating wheel, and rotating wheel is mounted on outer
In shell 1, the center of circle of rotating wheel is overlapped with the center location of shell 1, and rotating wheel can axial-rotation.Rotating wheel includes rotating wheel ontology
5, the cross section of rotating wheel ontology 5 is circle, and the circumference of rotating wheel ontology 5 is just struck against partition 2 close to the one end in the center of circle.Rotation
Wheel further includes at least one combustion chamber, air-fuel mixture gas burning expansion in the combustion chamber.In this present embodiment, rotating wheel includes
Two combustion chambers, the first combustion chamber 61 and the second combustion chamber 62, the first combustion chamber 61 and the second combustion chamber 62 are in rotating wheel ontology 5
Circumference on position it is opposite, i.e. angle between the first combustion chamber 61 and the second combustion chamber 62 is 180 °, and combustion chamber is cylinder
Shape.Two combustion chambers are set on shell 1, and two combustion chambers can successively do work, and increase the power output of engine.First burning
The position of room 61 and the second combustion chamber 62 is opposite so that two combustion chambers respectively complete air inlet, compression and acting, exhaust when
Between can link up.In other embodiments, the quantity of combustion chamber can be other numerical value, such as one, and the present invention is to burning
The quantity of room is with no restriction.Rotating wheel further includes part of calming the anger, and part of calming the anger is arranged corresponding to combustion chamber, and part of calming the anger can be rotated axially,
It is used to open or closes combustion chamber and change the opening direction of the combustion chamber.In this present embodiment, rotating wheel includes two pressures
Gas part, the first part 71 and second of calming the anger are calmed the anger part 72.The axle center that part of calming the anger axially rotates is Chong Die with the center of circle of combustion chamber.In other
In embodiment, the quantity for part of calming the anger can be other numerical value, and the quantity for part of calming the anger and the quantity of combustion chamber are consistent.
As shown in figure 3, shell 1, which is equipped with, puts forth effort part 3, putting forth effort part 3 and partition 2 will be between rotating wheel ontology 5 and shell 1
Cavity is divided into volume not equal two parts.Put forth effort part 3 with both ends, first end 31 and second end 32, the circumference of rotating wheel ontology 5
It is just struck against the first end 31 for putting forth effort part 3.In this present embodiment, put forth effort part 3 to be embedded in shell 1, put forth effort the first end 31 of part 3 with
Position of the partition 2 on shell 1 is opposite, that is, putting forth effort the angle between the first end 31 of part 3 and partition 2 is 180 °, puts forth effort part 3
Second end 32 is on the circumference of shell 1.Partition 2 is opposite with position of the part 3 on shell 1 is puted forth effort, partition 2 and put forth effort part 3 will be outer
The circumference of shell 1 is divided into two symmetrical circular arcs, and two combustion chambers are being connected by the time of two circular arcs respectively
Get up.Putting forth effort part 3 close to the side in 1 center of circle of shell is arc, put forth effort thickness that part 3 is mounted in shell 1 from second end 32 to
First end 31 gradually increases, so that when combustion chamber, which rotates through, puts forth effort part 3, part of calming the anger is with putting forth effort 3 side of part
Radian variation, in the combustion chamber gradually rotation to close combustion chamber.Put forth effort part 3 to be mounted on shell 1, it can also be with
Shell 1 is integrally formed.In other embodiments, putting forth effort the position of part 3 and partition 2 on shell 1 can be other situations, put forth effort part
3 can be used other shapes, and the present invention is to putting forth effort the location and shape of part with no restriction.
Wherein, the cavity that 111 partition 2 of air inlet, shell 1, the first end 31 for putting forth effort part 3 and rotating wheel ontology 5 surround is
Inlet chamber 8, the cavity that exhaust outlet 112, partition 2, shell 1, the first end 31 for putting forth effort part 3 and rotating wheel ontology 5 surround are exhaust
Chamber 9.The volume of inlet chamber 8 is less than the volume of discharge chamber 9.
As shown in figure 4, part of calming the anger includes calm the anger part main body 711 and rotary shaft 712, part main body 711 of calming the anger and rotary shaft 712
It is integrally formed.In this present embodiment, part of calming the anger includes calming the anger part main body 711 and two rotary shafts 712, rotary shaft 712 are mounted on
On rotating wheel ontology 5.Part of calming the anger is rotated with the rotation of rotating wheel ontology 5 on one side, on one side around the axial rotation of rotary shaft 712
Turn.
As shown in figure 4, in this present embodiment, part of calming the anger further includes rotating member, rotating member includes curved bar 101, curved bar guiding
Wheel 102 and spring 103.One end of curved bar 101 is set to the one end of rotary shaft 712 far from part main body 711 of calming the anger.Curved bar directive wheel
102 are set to the one end of curved bar 101 far from rotary shaft 712.Spring 103 is placed in rotary shaft 712, and one end of spring 103 is fixed on
On rotating wheel ontology 5, the other end of spring 103 is fixed on curved bar 101.
As shown in figure 3, shell 1 is equipped with guide rail 11 close to the circumference of inlet chamber 8.Guide rail 11 is from shell 1 close to air inlet
111 one end extends to the first end 31 for putting forth effort part 3.However, the present invention is not limited in any way this.In other embodiments,
Can not have guide rail 11, part of calming the anger can be arranged in correspondence with sliding block by the way that sliding slot is arranged on shell 1 to realize cunning on part of calming the anger
Row cooperation.
It calms the anger the rotary principle of part: when combustion chamber as rotating wheel ontology 5 goes to shell 1 on the circumference of inlet chamber 9
When, curved bar directive wheel 102 slides on guide rail 11, and the rotation of curved bar 101 is determined by guide rail 11, passes through curved bar 101 and rotary shaft
712, part of calming the anger axially rotates, to open or close combustion chamber and change the opening direction of combustion chamber.When combustion chamber rotates to
Near partition 2, the curved bar directive wheel 102 calmed the anger on part is moved by the track of guide rail 11, realizes that combustion chamber is closed in part rotation of calming the anger,
And accessible pass through partition 2.When the first end 31 for putting forth effort part 3 is passed through in combustion chamber, part of calming the anger at this time is revolved by the track of guide rail 11
Turn to close combustion chamber, and accessible by putting forth effort part 3.Then combustion chamber rotates to the part of no guide rail 11, spring 103 not by
It constrains, is restored to the original state of spring 103, while curved bar 101 being driven to rotate, to axially be rotated with action pneumatic part.
As shown in figure 3, the present invention also provides a kind of tangential force engine, including tangential force engine described above
Core component.Tangential force engine further includes igniter, and igniter includes spark plug 121, high-tension ignition electrode 122 and
By electrode 123.High-tension ignition electrode 122 is set on shell 1.Spark plug 121 is set in combustion chamber.It is set to by electrode 123
On rotating wheel ontology 5, and it is electrically connected by conducting wire and spark plug 121.When combustion chamber is just completely by putting forth effort the first of part 3
When holding 31, high-tension ignition electrode 122 is connected with by electrode 123.
The working principle of igniter: with the rotation of rotating wheel ontology 5, when combustion chamber is just completely by putting forth effort part 3
First end 31 when, gone to the position of high-tension ignition electrode 122 by electrode 123, high-tension ignition electrode 122 with by electric electrode
123 connect, and power supply is connected, and spark plug 121 is lighted a fire.
Tangential force engine further includes atomizer 4, and atomizer 4 is set to shell 1 on the circumference of air inlet 111.
The working principle of tangential force engine:
Fresh air in inlet chamber 8 to enter from air inlet 111.Rotating wheel ontology 5 rotates clockwise, when the first burning
Room 61 and the first part 71 of calming the anger rotate near partition 2, the first curved bar directive wheel 102 calmed the anger on part 71 by guide rail 11 track
Movement realizes that the first combustion chamber 61 is closed in the first 71 rotation of part of calming the anger, and accessible passes through partition 2.Inlet chamber 8 is calmed the anger by first
Part 71 is divided, and the first side for calming the anger part 71 is suction zone, and first other side for calming the anger part 71 is compressional zone.Atomizer 4 sprays
Fuel oil, first calm the anger part 71 in inlet chamber 8 fresh air and the fuel oil that sprays of atomizer 4 be compressed to the first combustion chamber 61
It is interior.
When the first combustion chamber 61 and first calm the anger part 71 go to the position for putting forth effort part 3 when, first calms the anger part 71 by guide rail 11
Track rotation close the first combustion chamber 61, air-fuel mixture gas is maintained in the first combustion chamber 61, and it is accessible by
Power part 3.First combustion chamber 61 is completely by putting forth effort the first end 31 of part 3, at this point, by electrode 123 and high-tension ignition electrode 122
Contact, spark plug 121 are lighted a fire, the explosion of high-pressure oil gas gaseous mixture and the expansion being compressed in the first combustion chamber 61, in the first pressure
71 two sides of gas part generate pressure difference, and rotating wheel ontology 5 is pushed to rotate clockwise.Meanwhile the reverse reset clockwise of spring 103, it beats
Open the first combustion chamber 61.Discharge chamber 9 is divided by the first part 71 of calming the anger, and the first side for calming the anger part 71 is the detonation of air-fuel mixture gas
Area, first other side for calming the anger part 71 is exhaust gas discharge region, and exhaust gas is discharged by exhaust outlet 112.
At this point, in the other side of rotating wheel ontology 5, the second combustion chamber 62 and the second part 72 of calming the anger pass through partition 2, the second pressure
Gas part 72 in inlet chamber 8 air and the fuel oil that sprays of atomizer 4 be compressed in the second combustion chamber 62.Second calms the anger part 72
Curved bar directive wheel 102 is moved along guide rail 11, when rotating to the position for putting forth effort part 3, second calm the anger part 72 by guide rail 11 rail
The second combustion chamber 62 is closed in mark rotation, and air-fuel mixture gas is maintained in the second combustion chamber 62, and by putting forth effort part 3.
First combustion chamber 61 and the first part 71 of calming the anger rotate near partition 2, and the expansion of exploding gas is close to terminating, and first
The curved bar directive wheel 102 calmed the anger on part 71 by guide rail 11 track move, realize first calm the anger 24 rotation of part close first burning
Room 61, and pass through the position of partition 2.So rotation is reciprocal.
Rotating wheel rotation does work and other attachmentes on engine is driven to work.
The above description is only a preferred embodiment of the present invention, not thereby limits scope of patent protection of the invention, all
It is directly or indirectly to be used in other relevant technologies with equivalent structure transformation made by description of the invention and accompanying drawing content
Field similarly includes within the scope of the present invention.
Claims (9)
1. a kind of core component of tangential force engine characterized by comprising
Shell, the shell have air inlet and exhaust outlet；
Rotating wheel, the rotating wheel are located in the shell, and the rotating wheel can be rotated axially, and the rotating wheel includes:
Rotating wheel ontology, the cross section of the rotating wheel ontology are circle；
At least one combustion chamber, the combustion chamber are set on the excircle of the rotating wheel ontology；And
It calms the anger part, the part of calming the anger is arranged corresponding to the combustion chamber, and the part of calming the anger can be rotated axially, closes or opens described
Combustion chamber and the opening direction for changing the combustion chamber；And
Put forth effort part, the part of putting forth effort is on the shell；
Wherein, the air inlet, the shell, described to put forth effort cavity that part and the rotating wheel ontology surround be inlet chamber, institute
State that exhaust outlet, the shell, described to put forth effort cavity that part and the rotating wheel ontology surround be discharge chamber, the body of the inlet chamber
Product is less than the volume of the discharge chamber.
2. the core component of tangential force engine as described in claim 1, which is characterized in that the part of calming the anger includes the part master that calms the anger
Body and rotary shaft, the part main body of calming the anger are integrally formed with the rotary shaft, and the rotary shaft is mounted on the rotating wheel ontology
On.
3. the core component of tangential force engine as claimed in claim 2, which is characterized in that the part of calming the anger further includes rotation
Part, the rotating member include:
Curved bar, one end of the curved bar are set to the one end of the rotary shaft far from the part main body of calming the anger；
Curved bar directive wheel, one end set on the curved bar far from the rotary shaft；And
Spring is placed in the rotary shaft, and one end of the spring is fixed on the rotating wheel ontology, the spring it is another
End is fixed on the curved bar.
4. the core component of tangential force engine as claimed in claim 3, which is characterized in that the shell is close to the inlet chamber
Circumference be equipped with guide rail, the curved bar directive wheel slides on the guide rail.
5. the core component of tangential force engine as described in claim 1, which is characterized in that the shell includes partition, described
Partition is for separating the air inlet and the exhaust outlet.
6. the core component of tangential force engine as claimed in claim 5, which is characterized in that the partition and the part of putting forth effort exist
Position on the shell is opposite.
7. the core component of tangential force engine as described in claim 1, which is characterized in that the quantity of the combustion chamber is two
A, position of described two combustion chambers on the excircle of the rotating wheel ontology is opposite.
8. the core component of tangential force engine as described in claim 1, which is characterized in that the part of putting forth effort is close to the shell
The side in the center of circle is arc, described to put forth effort the thickness that part is mounted in the shell and gradually increase.
9. a kind of tangential force engine, the core component including tangential force engine a method as claimed in any one of claims 1-8 is special
Sign is, further includes
Igniter, the igniter include spark plug, high-tension ignition electrode and by electrode, the high-tension ignition electrode
On the shell, the spark plug is set in the combustion chamber, described to be set on the rotating wheel ontology by electrode, and
It is electrically connected with the spark plug；And
Atomizer, the atomizer are set to the shell on the circumference of the inlet chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811094266.1A CN109139242A (en) | 2018-09-19 | 2018-09-19 | Tangential force engine and its core component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811094266.1A CN109139242A (en) | 2018-09-19 | 2018-09-19 | Tangential force engine and its core component |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109139242A true CN109139242A (en) | 2019-01-04 |
Family
ID=64815158
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811094266.1A Withdrawn CN109139242A (en) | 2018-09-19 | 2018-09-19 | Tangential force engine and its core component |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109139242A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2136066A (en) * | 1935-05-13 | 1938-11-08 | C J Bartlett | Rotary engine |
| US4075981A (en) * | 1976-04-15 | 1978-02-28 | Duane Burton | Rotary internal combustion engine |
| US4373484A (en) * | 1980-10-06 | 1983-02-15 | Boehling Daniel E | Rotary piston mechanism |
| CN1276037A (en) * | 1997-10-15 | 2000-12-06 | 埃米利安·布安 | Four stroke orbital internal combustion engine |
| CN101014758B (en) * | 2004-07-14 | 2012-01-04 | Clr有限公司 | Concentric internal combustion rotary engine |
| CN103375248A (en) * | 2012-04-13 | 2013-10-30 | 刘千省 | Rotary engine |
| CN103233782B (en) * | 2012-09-07 | 2015-09-09 | 胡武琼 | Cock-type rotary compression expansion mechanism |
| CN204738871U (en) * | 2015-07-15 | 2015-11-04 | 胡尹烟 | Slide formula rotating engine |
-
2018
- 2018-09-19 CN CN201811094266.1A patent/CN109139242A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2136066A (en) * | 1935-05-13 | 1938-11-08 | C J Bartlett | Rotary engine |
| US4075981A (en) * | 1976-04-15 | 1978-02-28 | Duane Burton | Rotary internal combustion engine |
| US4373484A (en) * | 1980-10-06 | 1983-02-15 | Boehling Daniel E | Rotary piston mechanism |
| CN1276037A (en) * | 1997-10-15 | 2000-12-06 | 埃米利安·布安 | Four stroke orbital internal combustion engine |
| CN101014758B (en) * | 2004-07-14 | 2012-01-04 | Clr有限公司 | Concentric internal combustion rotary engine |
| CN103375248A (en) * | 2012-04-13 | 2013-10-30 | 刘千省 | Rotary engine |
| CN103233782B (en) * | 2012-09-07 | 2015-09-09 | 胡武琼 | Cock-type rotary compression expansion mechanism |
| CN204738871U (en) * | 2015-07-15 | 2015-11-04 | 胡尹烟 | Slide formula rotating engine |
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| PB01 | Publication | ||
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Application publication date: 20190104 |