CN1912351A - Rotation jet engine - Google Patents
Rotation jet engine Download PDFInfo
- Publication number
- CN1912351A CN1912351A CN 200510085779 CN200510085779A CN1912351A CN 1912351 A CN1912351 A CN 1912351A CN 200510085779 CN200510085779 CN 200510085779 CN 200510085779 A CN200510085779 A CN 200510085779A CN 1912351 A CN1912351 A CN 1912351A
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- piston
- cylinder
- jet engine
- runner
- rotary jet
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Abstract
A rotary jet engine is prepared as connecting air cylinders to be rotary body on the same axle; setting air channel one-way valve, compression chamber, combustion chamber, jet nozzle on rotary wheel; setting air inlet one-way valve on air inlet and setting piston in air cylinder; connecting piston with square bar being set with round boss, setting guide groove at right-end internal wall of air cylinder and placing round boss in said groove and enabling round boss to slide in the groove.
Description
Affiliated technical field:
The present invention relates to a kind of motor, especially the incendivity thing after the compression can be entered pressing chamber on the runner by air flue, and then enter the firing chamber on the runner, the rotation of knocking fuel recoil pull runner, the rotary jet engine that compression, burning separate.
Background technique:
At present, known piston engine mainly is made up of cylinder, piston, connecting rod, bent axle, intake valve, exhaust valve, spark plug, air-breathing, the compression of this motor, work done, exhaust all are to finish in same cylinder, and by piston, connecting rod, the external outputting power of bent axle, because the to-and-fro motion of piston, connecting rod, bent axle, distribution device, limited it rotating speed and exert oneself, efficient is lower.
Advanced is triangular piston rotary engine, this motor is innovation to some extent structurally, connecting rod, bent axle have been saved, piston is a triangle, but its biggest problem is sealing, three linear sealing gases of triangle piston, also have two end faces, therefore be one discontinuous and the sealing curve of flex point arranged, and triangle piston discontinuity in cylinder, make cylinder operation occur chatter mark (being commonly called as the washing board phenomenon) after a period of time, its also has a series of problems such as heat radiation, lubricated, manufacturing technology, makes this motor fail so far to be extensive use of.
Air breathing engine is because technical requirements height, the manufacture difficulty of its turbine are big, high the only limiting to of cost used on the aircraft.
Summary of the invention:
Air-breathing in order to overcome piston engine, compression, work done, exhaust is all finished and connecting rod in same cylinder, bent axle, the unfavorable inertia of distribution device, the potted line that overcomes triangle piston circulating engine is discontinuous, the piston discontinuity, overcome problems such as the air breathing engine manufacture difficulty is big, the invention provides a kind of air-breathingly in cylinder, finish, compression, work done, exhaust is finished at another place, save connecting rod, bent axle, the distribution device reciprocator, piston no longer is the parts of external outputting power, directly by the runner outputting power, so the present invention has overcome the congenital shortcoming of aforementioned motor, concentrated the piston engine tightness good, triangle piston circulating engine does not have connecting rod, bent axle, distribution device reciprocator and simple in structure, and several big advantage of air breathing engine high-temperature high-pressure fuel gas recoil.
The technical solution adopted for the present invention to solve the technical problems is:
Suction port, runner, cylinder sequence are connected as a single entity, and form the solid of rotation of a same axis; Three air flues at 120 degree angles are each other arranged on runner, communicate with three pressing chambers respectively, three pressing chambers communicate with three firing chambers respectively again, and there is a spout each firing chamber; The air flue one-way cock is installed on each air flue, and the gas after preventing to compress is fed back in the cylinder.Be fixed with suction port on the runner left side, the breather check valve door is installed on suction port; Be fixed with a cylinder on runner the right, the other end inwall of cylinder is fixed with the direction recess that makes the piston move left and right; Piston and square bar in the cylinder are rigidly connected, and are fixed with a garden boss on the square bar certain position, and the convex portion of garden boss places in the groove of direction recess, and can slide.When cylinder block is rotated, the convex portion of garden boss is move left and right under the drive of direction recess, thereby make the piston move left and right, (being similar to an advance and retreat mode of some garden pearl pen) the gas in the cylinder by airway pressure to pressing chamber, the other end of square bar, place in the square hole seat of location, and can slide.
Working principle of the present invention is such: (starting this motor) piston is gone from left to right, the breather check valve door is opened, pass through suction port, the mixture of suck air and oil, piston is gone from right to left, the breather cheek valve door is closed, mixture is compressed and opens the air flue one-way cock and enters pressing chamber, when the mixture of pressing chamber is compressed to a certain degree by compression ignite, (or light, do not draw ignition mechanism among the figure) enters the firing chamber again and fiercely burns, and the combustion gas of High Temperature High Pressure sprays from spout, form recoil thrust, make the runner rotation.Because suction port, runner, cylinder are rotary integrals, direction recess on the cylinder inner wall, the move left and right that garden boss, square bar, piston in the groove are not stopped, mixture just constantly is pressed towards pressing chamber like this, and enter the firing chamber and carry out knocking fuel, combustion gas sprays from spout, forms recoil thrust promotion runner and ceaselessly rotates external outputting power.
In fact the present invention has formed a rotary integral by suction port, runner (being included in pressing chamber, firing chamber above it) cylinder, by the outer outputting power of the gear mesh on this rotary integral, and piston only plays a part to calm the anger, and it is translation, not external outputting power.But the present invention's multi-cylinder serial or parallel connection, by many piston gas-pressings, single runner rotation outputting power can obtain bigger output power.Big small gear on the solid of rotation can play transmission action, further reduces volume.
It is the continuous works done of 360 degree that the present invention whenever circles, and torque is in maximum value all the time, the two all works done of piston engine revolution once, therefore, the present invention compares with the piston engine of discharge capacity on an equal basis, and is more powerful; Owing to do not have connecting bar and crankshaft and distribution device, rotating speed is higher; Compression to fuel oil mixture can be pressed onto until compression ignite, improves compression ratio and efficient greatly; Also having overcome piston engine makes cylinder become ellipse garden to the cross component force of piston because of connecting rod for a long time, reduce the problem of sealability, also overcome three the angle discontinuity of triangular piston rotary engine, made cylinder chatter mark and sealing problem occur at power stroke intermediate cam piston.Piston of the present invention no longer is a power output part, and is in the translation state all the time, and the turbine that the present invention need not air breathing engine makes simplified manufacturing process, and cost reduces.
The invention has the beneficial effects as follows, simple in structure, volume is little, in light weight, power is big, rotating speed is high, vibration is little, efficient is high, good airproof performance, easy to manufacture, fuel-economizing, makes lubricatedly simultaneously, heat radiation also becomes simple.
Description of drawings:
The present invention is further illustrated below in conjunction with drawings and Examples:
Fig. 1 is a first embodiment of the present invention structural principle schematic representation.
Fig. 2 is a second embodiment of the present invention structural principle schematic representation.
Fig. 3 is a rotaring wheel structure floor map of the present invention.
Fig. 4 is that direction recess of the present invention launches schematic representation.
Among the figure, 1 runner, 2 cylinders, 3 pistons, 4 square bars, 5 suction ports, 6 breather check valve doors, 7 pressing chambers, 8 air flue one-way cocks, 9 firing chambers, 10 spouts, 11 direction recess, 12 garden boss, 13 location square hole seats, 14 output gears, 15 bearings.
Embodiment:
In Fig. 1, suction port 5, runner 1, cylinder 2 order coaxial lines are linked to be the solid of rotation of an integral body.Be fixed with suction port 5 on the left side of runner 1, be fixed with cylinder 2 on the right of runner 1, a piston 3 is arranged in cylinder 2, the right-hand member of piston 3 and square bar 4 are rigidly connected, be fixed with garden boss 12 on the certain position of square bar 4, the other end of square bar 4 can slide in location square hole seat 13.Bearing 15 and output gear 14 that fixing whole solid of rotation is arranged in the outside of solid of rotation.
In Fig. 2, as suction port 5, cylinder 2 can seal the rotation of sliding on suction port 5, breather check valve door 6 is housed on piston 3 an end of cylinder 2.
In Fig. 3, three (or many) air flue at 120 degree angles is each other arranged on the runner 1, air flue communicates with three pressing chambers 7 (or a plurality of) respectively, and three pressing chambers 7 communicate with three firing chambers 9 (or a plurality of) respectively again, and a spout 10 is arranged on each firing chamber.On three air flues of pressing chamber 7, being separately installed with air flue one-way cock 8, flow so that the mixed gas that prevents pressing chamber 7 is counter.If the total measurement (volume) of (fuel oil is for lighting) three pressing chambers is preferably about the 1/10----1/16 of cylinder total volume; If the total measurement (volume) of (fuel oil is a compression ignite) three pressing chambers is preferably about the 1/16----1/22 of cylinder total volume, make compression ratio reach optimum value
In Fig. 4, direction recess 11 is fixed on the cylinder 2 right-hand member inwalls, and the convex portion of garden boss 12 places in the groove of direction recess 11, and can slide in groove.
Claims (8)
1. a rotary jet engine is connected by suction port, runner, cylinder sequence coaxial line, and it is characterized in that: suction port is connected with runner, and the another side of runner is connected to become a rotary integral with cylinder again.
2. rotary jet engine according to claim 1, it is characterized in that: three air flues that are mutually 120 degree angles are arranged on the runner, the air flue one-way cock is installed on the air flue, three air flues communicate with three pressing chambers respectively, three pressing chambers communicate with three firing chambers respectively again, and a spout is installed on each firing chamber.
3. rotary jet engine according to claim 1 is characterized in that: the breather check valve door is installed on the suction port.
4. rotary jet engine according to claim 1 is characterized in that: on the inwall of cylinder one end direction recess has been installed.
5. rotary jet engine according to claim 1 is characterized in that: piston one end and square bar are rigidly connected, and the other end of square bar is slidingly connected with location square hole seat.
6. according to claim 1,5 described rotary jet engines, it is characterized in that: be fixed with the garden boss on the square bar.
7. according to claim 1,4,6 described rotary jet engines, it is characterized in that: the convex portion of garden boss is slidingly matched and places in the groove of direction recess.
8. rotary jet engine according to claim 1 is characterized in that: the breather check valve door is installed on the piston.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200510085779 CN1912351A (en) | 2005-08-09 | 2005-08-09 | Rotation jet engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200510085779 CN1912351A (en) | 2005-08-09 | 2005-08-09 | Rotation jet engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1912351A true CN1912351A (en) | 2007-02-14 |
Family
ID=37721387
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200510085779 Pending CN1912351A (en) | 2005-08-09 | 2005-08-09 | Rotation jet engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1912351A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102392689A (en) * | 2011-08-16 | 2012-03-28 | 王瀚诚 | Injection type rotating motor |
| CN102434352A (en) * | 2011-12-10 | 2012-05-02 | 天台亘盛能源科技有限公司 | Hydraulic energy generating set driven by backshock kinetic energy engine |
| CN102434216A (en) * | 2011-12-09 | 2012-05-02 | 天台亘盛能源科技有限公司 | Recoil kinetic energy engine |
| CN103306736A (en) * | 2012-04-30 | 2013-09-18 | 王政玉 | Power turbine and power machine of the power turbine |
| CN102356214B (en) * | 2009-03-18 | 2016-05-04 | Hk轮机有限公司 | Reaction turbine |
| CN104141512B (en) * | 2009-03-18 | 2016-11-30 | Hk轮机有限公司 | Reaction turbine |
| CN108361109A (en) * | 2018-01-29 | 2018-08-03 | 余四艳 | General molded breadth energy rotary jet engine |
-
2005
- 2005-08-09 CN CN 200510085779 patent/CN1912351A/en active Pending
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102356214B (en) * | 2009-03-18 | 2016-05-04 | Hk轮机有限公司 | Reaction turbine |
| CN104141512B (en) * | 2009-03-18 | 2016-11-30 | Hk轮机有限公司 | Reaction turbine |
| CN102392689A (en) * | 2011-08-16 | 2012-03-28 | 王瀚诚 | Injection type rotating motor |
| WO2013023607A1 (en) * | 2011-08-16 | 2013-02-21 | Wang Hancheng | Jet rotary motor |
| CN102434216A (en) * | 2011-12-09 | 2012-05-02 | 天台亘盛能源科技有限公司 | Recoil kinetic energy engine |
| CN102434352A (en) * | 2011-12-10 | 2012-05-02 | 天台亘盛能源科技有限公司 | Hydraulic energy generating set driven by backshock kinetic energy engine |
| CN103306736A (en) * | 2012-04-30 | 2013-09-18 | 王政玉 | Power turbine and power machine of the power turbine |
| CN103306736B (en) * | 2012-04-30 | 2015-10-14 | 王政玉 | A kind of power turbine and power engine thereof |
| CN108361109A (en) * | 2018-01-29 | 2018-08-03 | 余四艳 | General molded breadth energy rotary jet engine |
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Open date: 20070214 |