CN1271323C - Dynamic jet type IC engine - Google Patents
Dynamic jet type IC engine Download PDFInfo
- Publication number
- CN1271323C CN1271323C CNB00110585XA CN00110585A CN1271323C CN 1271323 C CN1271323 C CN 1271323C CN B00110585X A CNB00110585X A CN B00110585XA CN 00110585 A CN00110585 A CN 00110585A CN 1271323 C CN1271323 C CN 1271323C
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- Prior art keywords
- engine
- jet type
- dynamic jet
- shaped rotor
- hollow shaft
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- Expired - Lifetime
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- 239000007789 gas Substances 0.000 claims abstract description 35
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 16
- 239000000567 combustion gas Substances 0.000 claims description 8
- 239000000498 cooling water Substances 0.000 claims description 6
- 238000010304 firing Methods 0.000 claims description 6
- 230000007246 mechanism Effects 0.000 claims description 4
- 230000001914 calming effect Effects 0.000 claims description 2
- 230000002093 peripheral effect Effects 0.000 claims 1
- 239000000779 smoke Substances 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 abstract description 6
- 230000000694 effects Effects 0.000 abstract description 5
- 230000008901 benefit Effects 0.000 abstract description 4
- 239000000446 fuel Substances 0.000 abstract description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract description 2
- 239000001301 oxygen Substances 0.000 abstract description 2
- 229910052760 oxygen Inorganic materials 0.000 abstract description 2
- 239000000126 substance Substances 0.000 abstract description 2
- 230000008016 vaporization Effects 0.000 abstract description 2
- 230000005855 radiation Effects 0.000 abstract 1
- 239000007787 solid Substances 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000003912 environmental pollution Methods 0.000 description 2
- 210000004907 gland Anatomy 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 230000029058 respiratory gaseous exchange Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 239000002918 waste heat Substances 0.000 description 2
- 241000406668 Loxodonta cyclotis Species 0.000 description 1
- 210000001015 abdomen Anatomy 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 230000006837 decompression Effects 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 238000002309 gasification Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 230000004899 motility Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000003319 supportive effect Effects 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
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- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The present invention belongs to the field of heat engines. The machine of the present invention has the advantages of an internal combustion engine, a gas turbine, a steam turbine, a jet engine, etc. A heat source is an annular rotor (61) and is arranged on a hollow shaft (29) in a cylinder, and the hollow wheel circumference of the annular rotor (61) is embedded with wing-shaped axial cascades (6). An oxygen supply device, a burning device, a vaporizing device and a work application device of the complete machine are coaxial and integrative, devices incapable of applying work, such as a still furnace, a combustion chamber, a working substance pipeline, etc. of the existing heat engine, are eliminated, and thereby, the ratio of the force to the body, the ratio of the effect to the weight and the ratio of the push to the weight are increased. The machine utilizes atomized water having a certain proportion with fuel as accessory energy sources, the residual heat is trapped to apply work for second time, and the heat efficiency and the exergy parameters are enhanced. The machine has the advantages of simple structure, and less friction and heat radiation, and is energy-saving motive force of large-sized vehicles, ships, aircrafts, etc.
Description
Dynamic jet type IC engine belongs to hot machine field.
Steamer, steam turbine all belong to external-combustion engine has dependence to huge and heavy boiler; Stroke IC engine to-and-fro motion friction ractor is big, vibration and entropy increase all unavoidably, and the thermal efficiency is low; Gas turbine still has devices such as stilling combustion chamber, working medium pipeline, brings to gas compressor can consume in the white elephant greatly; The air breathing engine thermosteresis is serious, and fire is not high with parameter.
It is the energy-conservation motility mechanical of complete new-type, high-power, a small and exquisite clever cage that the shortcoming that the present invention is intended to overcome above-mentioned all hot machines is concentrated its advantage; the special water of the present invention is cooked auxiliary working substance and is held back waste heat twice work doing, reinforcing, postpones the existing using energy source time limit and reduce municipal pollution protection human environment providing feasible shortcut for alleviating energy crisis.
The present invention realizes with following scheme: this machine is formed coaxial integrated by four big portions such as multi stage axial flow compressor, gas turbine, jet nozzle or steam turbine.
The firing chamber of this machine, revolving furnace promptly are that dynamic jet type IC engine ring-shaped rotor (61) is seen figure four (), are the rotors of dynamic jet type IC engine, and this rotor is core of the present invention.Under the startup of jiggering motor (15), hollow shaft (29) the drive well behaved spiral slideway formula of power gas compressor (4) is in an opposite direction started working.Air pressure than forming stagnation state in (31) between the inflation that is compressed to gas compressor with certain truth of a matter step by step, can be alleviated upper level gas compressor burden, can be the next stage gas compressor again and establish the air tightness basis.Multistage compressor enters high-pressure air the precombustion chamber (47) of hollow shaft from hollow shaft (29) inlet hole (19) at last, and the mist of oil of sending here with high pressure oil nozzle (32) converges through ignition mechanism (35) mixed gas is become pre-combustion gas.Under the promotion of follow-up air-flow, pre-combustion gas is arrived fiercely burning in the firing chamber (58) fast from pre-gas jet orifice (33) ejection through pre-combustion gas passage (55), and forming combustion gas has stagnation state slightly, and this process is similar to blowtorch.High-pressure gas is sprayed onto holding back on the leaf (7) of inwall in the cylinder through nozzle (5), and at this moment gas can produce thrust and recoil force and solid face efficacy to axial leaf grating stream interface and sees Fig. 9 (C).Axially leaf grating is carried on the back under the stressed irregular situation at abdomen, be added with again lift on the infinitesimal Joukowski efficacy these to try hard to recommend moving axis be the origin that a moment forms to leaf grating by the certain track motion.Rotor is worked in hot environment for a long time to guaranteeing that its safety is under the drive of hollow shaft (29), high-pressure water pump (21) is held back water on the leaf (7) in rotor (61) both sides and stator with atomized spray through spraynozzle (9) by high-pressure water pipe (8), make gas density p and pressure P surge in the cylinder after immediately becoming the mixing of high-quality steam and gas, make thrust increase several times.This intensity and measure very high working medium and directly excrete from jet nozzle (30), will produce axial huge thrust becomes aero-jet engine, sees Fig. 1,2.Small and exquisite, the clever cage of this aeroengine, size are little, in light weight, can be positioned under the wing, also can be positioned on the body afterbody.Promptly can produce radially powerful moment as working medium by multiple tracks stator leaf grating and rotor leaf grating becomes multistage turbine and sees Fig. 3, this be plane its use.In multistage turbine, the steam flow radially moving blades (12) that time ejection vapour Shu Shouxian is sprayed on the tubbiness rotor by the stator leaf grating is gone up work done, enter the tubbiness rotor and fill (13) between vapour, (13) have dead state slightly between inflation, moving blades (36) ejection vertically, at this moment gas can produce thrust and recoil force to the blade stream interface.The vapour bundle is sprayed onto holding back on the leaf (7) of cylinder inner wall, obtains solid face efficacy.Gas passes through stator leaf grating (10) again and enters the next stage rotor, work done so continuously.Gas is discharged from steam-expelling port (30) at last.
Beneficial effect: this gas compressor has the stagnation space, when satisfying level pressurized air, can alleviate the gas compressor burden, saves energy consumption when improving pressure ratio.Ring-shaped rotor (61) itself can have certain air-breathing function in the time of work done, also can alleviate the gas compressor burden, and this structure is better than existing stilling combustion chamber.The revolving furnace cooling water is held back waste heat, becomes working medium, and secondary-working, reinforcing can improve the hot machine thermal efficiency and mechanical efficiency simultaneously, and fire rises with parameter.The fuel-saving power that also strengthened simultaneously, it is free from environmental pollution that cheap water is made supplementary energy, can postpone the time limit that utilizes of the energy.This machine utilizes fuel type tolerance, and natural vegetation can be caught the conversion of solar energy of coming in day of earth energy exhaustion in future be fuel, and the car and boat aircraft that travels is as usual gone up to the sky as usual.Removing and discharge function that this machine high-pressure cooling water and high velocity air are certain to being formed with of dirt can delay mechanical life voluntarily.This machine does not structurally have solid face contact friction, and long working life is less demanding to air cleanliness.The blade of acting mostly is two solid heads, and chatter is little, and noise is little.Because revolving furnace is located in the cylinder, its stove inside and outside differential pressure is not very big, so the furnace wall need not heaviness, this structure makes and pushes away/and anharmonic ratio, effect/anharmonic ratio, effect/body ratio be improved.Mixed gas is better than gas only and water vapor as working medium on workmanship's ability.Lubricant oil is free from environmental pollution away from hot spots, and national defence meaning and social benefit are big, but its usefulness of plane.
Fig. 1 dynamic jet type IC engine unitary construction schematic representation (being applied on the baby plane)
Fig. 2 dynamic jet type IC engine unitary construction schematic representation (being applied on the large aircraft)
Fig. 3 dynamic jet type IC engine high pulling torque complete machine schematic representation (it uses plane)
Fig. 4 dynamic jet type IC engine aircraft rotor schematic representation
(1) rotor A is to view
(2) schematic representation cuts open in three-dimensional office
Fig. 5 dynamic jet type IC engine rotor cut-away view
Schematic representation cuts open in Fig. 6 dynamic jet type IC engine turbine rotor office
Fig. 7 dynamic jet type IC engine B is to cut-away view
C is to cut-away view
Fig. 8 (one) dynamic jet type IC engine gas compressor A is to diagrammatic sketch
(2) the afterburning nozzle D of jet nozzle is to schematic representation
The axial leaf grating working principle of Fig. 9 dynamic jet type IC engine schematic representation (one)
The axial leaf grating working principle of Figure 10 dynamic jet type IC engine schematic representation (two)
1. the afterburning nozzle 2. compressor rotors 3. casing 4. spiral slideway formula gas compressors 5. nozzles 6. axial hollow leaf gratings 7. of calming the anger are held back radially 14. cylinders, 15. jiggering motors, 16. high-pressure oil pipes between moving blades 13. rotors inflations of leaf 8. high-pressure cooling water pipes 9. cooling water nozzles 10. stator leaf gratings 11. turbine rotor sealed mouths 12.
17. circuit 18. high-pressure oil pipe inner bearings
19. hollow shaft inlet hole 20. bearings 21. water pumps 22. oil pumps 23. water tanks
24. high-pressure oil pipe 25. gas turbine shells 26. fuel tanks 27. water-cooling tubes
28. steam turbine stator 29. hollow shafts, 30. jet nozzles (steam-expelling port)
31. 32. high pressure oil nozzles, 33. pre-gas jet orifices between the gas compressor inflation
34. equalizing orifice 35. ignition mechanisms 36. turbine shafts are to leaf grating 37. turbine rotors
38. moving blades 39. steam turbine tubular rotor supports radially
40. rotor chuck 41. advances oxygen road 42. air breathing engine supports, 43. bearings
44. the axial leaf grating 46. tail cone spring bearings of steam discharge rectification tail cone 45. steam discharges
47. precombustion chamber 48. bearings 49. bafflers
51. pre-gas jet orifice decompression shaft sealing gland in leaf grating 52. exhaust ports 53. high-pressure oil pipes
54. pre-57. turbine rotor spaces, warm water sleeve 55. pre-combustion gas passage 56. suction holes
58. firing chamber 59. turbine rotor involute burrs, 60. steam turbine fill inner casing between vapour
61. dynamic jet type IC engine ring-shaped rotor 62. outer cards
The well behaved gas compressor classification of the power of will clashing is installed in the compressor casing (3), is communicated with between casket, has before the impeller (31) between inflation, plays a part to form a connecting link.High-pressure oil pipe (24) and circuit (17) are arranged in the hollow shaft (29), high-pressure oil pipe plays a supportive role by high-pressure oil pipe inner bearing (18), keeps static, and sealing gland (53) is arranged, circuit (17) is installed in the high-pressure oil pipe (24), is provided with ignition mechanism (35) in the precombustion chamber of circuit (17).The axle center air inlet has at revolving furnace rotates the effect that air inlet alleviates the gas compressor burden easily under the centrifugal action.Spiral slideway formula gas compressor (4) is coaxial integrated all affixed with hollow shaft (29) with dynamic jet type IC engine rotor (61).The bearing fulcrum is arranged between gas compressor and the revolving furnace and outside output torque shaft part is arranged, can drive water pump, oil pump work.Pre-warm water sleeve (54) can cool off to gas compressor, and institute recepts the caloric self to lay in and is sent to spraynozzle (9) by water pump and removes to cool off revolving furnace, and the vaporization heat basis is arranged.Coming to be mixed in the warm water of pre-warm water sleeve (54) and gasification back combustion gas that working medium discharges from jet nozzle is the several times of former single-fuel institute exoergic working efficiency, and cooling had the anti-surge effect before this combustion back cooling was better than firing, and fuselage reduces.
Claims (2)
1. a dynamic jet type IC engine is characterized in that: contain multi stage axial flow compressor, dynamic jet type IC engine ring-shaped rotor (61), hollow shaft (29); One end of described hollow shaft (29) embed in the dynamic jet type IC engine ring-shaped rotor (61) and with outer card (62) sealing-in of dynamic jet type IC engine ring-shaped rotor (61); Be precombustion chamber (47) and pre-gas jet orifice (33) is arranged in described hollow shaft (29) embedding section; Described hollow shaft (29) communicates with the firing chamber (58) of dynamic jet type IC engine ring-shaped rotor (61) through pre-combustion gas passage (55) by the pre-gas jet orifice (33) above it; Be axially arranged with high-pressure oil pipe (16) in described hollow shaft (29), there is high pressure oil nozzle (32) end; In described high-pressure oil pipe (16), circuit (17) is arranged; In precombustion chamber (47) section of described circuit (17), ignition mechanism (35) is arranged; Between described dynamic jet type IC engine ring-shaped rotor (61) two cards, axially be provided with equalizing orifice (34); Described equalizing orifice (34) is separated mutually with pre-combustion gas passage (55); The peripheral part of described dynamic jet type IC engine ring-shaped rotor (61) is embedded with axial hollow leaf grating (6); The nozzle (5) that communicates with the firing chamber (58) of dynamic jet type IC engine ring-shaped rotor (61) is arranged between described axial hollow leaf grating (6).
2. contain multi stage axial flow compressor in the dynamic jet type IC engine according to claim 1, casing (3) outside of calming the anger has pre-warm water sleeve (54) to communicate with high-pressure cooling water nozzle (9) through aqueduct (8), and cooling water smoke is to be sprayed on dynamic jet type IC engine rotor (61) outside.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB00110585XA CN1271323C (en) | 2000-06-29 | 2000-06-29 | Dynamic jet type IC engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB00110585XA CN1271323C (en) | 2000-06-29 | 2000-06-29 | Dynamic jet type IC engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1331383A CN1331383A (en) | 2002-01-16 |
| CN1271323C true CN1271323C (en) | 2006-08-23 |
Family
ID=4580569
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB00110585XA Expired - Lifetime CN1271323C (en) | 2000-06-29 | 2000-06-29 | Dynamic jet type IC engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1271323C (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101915132B (en) * | 2010-07-29 | 2013-07-24 | 刘春� | Oxygen-enriched combustion engine |
| CN103498803A (en) * | 2013-10-28 | 2014-01-08 | 岑溪市东正新泵业贸易有限公司 | Multistage mute energy-saving air compressor |
| CN103603693A (en) * | 2013-12-05 | 2014-02-26 | 罗亚军 | Hollow-shaft new power engine |
| CN104847418B (en) * | 2015-05-14 | 2018-02-09 | 北京良明宇航节能动力装备技术开发中心 | Micro- combustion cogenerator |
-
2000
- 2000-06-29 CN CNB00110585XA patent/CN1271323C/en not_active Expired - Lifetime
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| Publication number | Publication date |
|---|---|
| CN1331383A (en) | 2002-01-16 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| C49 | Reinstatement of patent right or utility model | ||
| RR01 | Reinstatement of patent right | ||
| C56 | Change in the name or address of the patentee | ||
| CP02 | Change in the address of a patent holder |
Address after: 550081 Guizhou Province, Guiyang City Lake District Yun Tan Road No. 602 Patentee after: Liu Jing Address before: 1799 mailbox, east campus, Xi'an Jiao Tong University Patentee before: Liu Jing |
|
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20060823 |