CN101363387A - Rotating athodyd - Google Patents
Rotating athodyd Download PDFInfo
- Publication number
- CN101363387A CN101363387A CNA2008101609914A CN200810160991A CN101363387A CN 101363387 A CN101363387 A CN 101363387A CN A2008101609914 A CNA2008101609914 A CN A2008101609914A CN 200810160991 A CN200810160991 A CN 200810160991A CN 101363387 A CN101363387 A CN 101363387A
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- hollow rotor
- rotating
- push rod
- ramjet
- fuel
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Abstract
The invention discloses a rotating ramjet engine which is composed of a frame, a hollow rotor shaft, a push rod, a fuel supply system, a fuel static-dynamic pipe joint sealing device and a starting device, etc. The rotating ramjet engine is characterized in that: the push rod vertical to the hollow rotor shaft is provided with a ramjet propeller; the ramjet propeller is drawn by the push rod to do circumferential eccentric motion around the hollow rotor shaft; the complementary work generated by the ramjet propeller during rotary motion can be transferred to the hollow rotor shaft by the push rod and can be output by a power output device which is arranged on the hollow rotor shaft. The rotating ramjet engine has the advantages that: as a ram device is arranged on the jet propeller, an original gas compressor and combustion improver, and the like, in the existing rotating jet engine can be omitted, thus greatly lowering the manufacturing cost and the self weight of the engine, increasing the power of the rotating jet engine and reducing energy consumption. The rotating ramjet engine can be widely applied to various vehicles, generating equipment, etc.
Description
The present invention relates to a kind of air breathing engine, particularly a kind of rotating athodyd.
Motor is as one of most widely used power plant of daily life machinery neck internal area, constantly explored and study as research object by vast motor amateur always, basic goal all is in order to find out better engine structure or the form of performance that a kind of structure is simpler, power consumption more reduces, to tackle the whole world exhausted day by day energy problem and environmental issue.At present, though known jet rotor motor has been obtained more satisfactory effect in form, also exist many problems needs further to be studied and solve at aspects such as energy-conservation, material-saving, losss of weight.The basic problem of current its existence has: the one, and manufacture difficulty is big; The 2nd, also have a lot of technical barriers to need further to be overcome, as heat dissipation problem, sealing problem or the like; The 3rd, except that employing rocket liquor burning-aid method can increase volume and the own wt, the conventional fuel motor also must use at least one gas compressor, so all certainly will bring problems such as manufacture cost increase, weight increase, energy consumption increase and power reduction.
The objective of the invention is: a kind of do not have gas compressor and liquor auxiliary combustion equipment are provided, simple in structure, in light weight, the rotating athodyd that manufacture cost and energy consumption significantly reduce, power enlarges markedly.
The present invention is achieved in that this motor by frame, hollow rotor shafts, and push rod, ignition mechanism, fuel supplying device, the quiet moving pipe of fuel connect seal arrangement and reach (opening) moving device formation.One end of push rod is connected with hollow rotor shafts is vertical, and the other end is connected with the ramjet propulsion device is vertical, allows hollow rotor shafts also vertical with the ramjet propulsion device simultaneously.The ramjet propulsion device should be arranged on the outermost end of push rod for the linear velocity that makes the rotation of ramjet propulsion device the time can obtain maximum.Started (opening) moving device hollow rotor shafts is rotated, driven the ramjet propulsion device by push rod simultaneously and do around hollow rotor shafts that circumference is centrifugal to rotatablely move; When rotatablely moving of ramjet propulsion device reaches required certain speed, begin to add fuel and also light simultaneously, hollow rotor shafts can break away from (opening) motivation and make the ramjet propulsion device begin work done voluntarily and continuation promotion hollow rotor shafts rotation conversely this moment; The complementary work that the ramjet propulsion device is done is by being arranged on outside power take-off on the hollow rotor shafts is output in.Simultaneously one to some push rods and can be set on same hollow rotor shafts as required to several ramjet propulsion devices, the ramjet propulsion device can be arranged in the same plane when a plurality of ramjet propulsion device is set, also can be arranged in the different planes; When a ramjet propulsion device only is set or during the ramjet propulsion device left and right sides gravity unbalance of setting, gravity balance device should be set to eliminate the whirling vibration of motor; Be fuel saving more, should the quiet moving pipe of fuel connect seal arrangement and be set to dual-oil seal liquid sealing device inside and outside the plug-in type.
The present invention compares advantage with known technology: owing to be provided with the ramjet propulsion device, so can save in the at present known jet rotary engine so devices such as gas compressor that has and combustion improvers, can reduce manufacture cost greatly like this and reduce the own wt of engine assembly, make jet rotating forwarding motivation more powerful, energy consumption is lower.This kind motor can be widely used in the various traffic tool and power generating equipment etc.
Below in conjunction with accompanying drawing, the present invention program is further described.
Fig. 1 is a positive side view of the present invention
Fig. 2 is a front view of the present invention
Fig. 3 connects seal arrangement one form sectional view for the quiet moving pipe of fuel of the present invention
Fig. 4 connects its two forms sectional view of seal arrangement for the quiet moving pipe of fuel of the present invention
Among the figure: 1 frame, 2 hollow rotor shafts, 3 push rods, 4 ramjet propulsion devices, the quiet moving pipe of 5 fuel connects seal arrangement, the quiet pipe of 6 fuel supplies, 7 power take-off, 8 inner oil seals, 9 bearings, 10 outer oil seals, 11 sealing fluids, 12 seal arrangement shells, 13 fuel inject the dead axle pipe, 14 fuel supply arms, 15 sealing fluid auto-feeding devices.
Among Fig. 1, on entablature 1, be provided with hollow rotor shafts 2, make the push rod 3 that is located on the hollow rotor shafts 2 vertical with hollow rotor shafts 2, and make the jet direction that is located at the ramjet propulsion device 4 on push rod 3 the other ends vertical with push rod 3, also make the jet direction of ramjet propulsion device 4 vertical simultaneously with hollow rotor shafts 2; Play (opening) motivation hollow rotor shafts 2, push rod 3 and the ramjet propulsion device 4 of motor are all rotated simultaneously, when the linear velocity of ramjet propulsion device 4 reaches the speed of calming the anger required, begin to add fuel and also light simultaneously; When ramjet propulsion device 4 begins work done voluntarily, cut off the driving of (opening) motivation, make ramjet propulsion device 4 continue to promote hollow rotor shafts 2 by push rod 3 conversely and rotate; The needed combustion-supporting body of calming the anger of motor comes from the stamping process of motor self fully, thereby saves huge gas compressor and liquid auxiliary combustion equipment; When a plurality of ramjet propulsion device 4 was set, the direction of propulsion of each ramjet propulsion device 4 should be in full accord, and each ramjet propulsion device 4 can according to circumstances be arranged in the same plane with needs, also can be arranged in a plurality of planes and (not represent among the figure); When a ramjet propulsion device 4 is set, gravity balance device (not representing among the figure) should be set to reduce vibration; The fuel of ramjet propulsion device 4 is provided by fuel supply arm 14.
Among Fig. 2, be provided with hollow rotor shafts 2 on entablature 1, an end of hollow rotor shafts 2 blocks, and the other end connects seal arrangement 5 by the quiet moving pipe of fuel and is communicated with the quiet pipe 6 of fuel supply, and hollow rotor shafts 2 is communicated with fuel supply arm 14 simultaneously; On hollow rotor shafts 2, be provided with power take-off 7; Make the push rod 3 that is located on the hollow rotor shafts 2 vertical, make the jet direction of the ramjet propulsion device 4 that is located on the push rod 3 vertical and vertical with hollow rotor shafts 2 with push rod 3 with hollow rotor shafts 2; For reducing the wearing and tearing of contactless ignition, after ignition mechanism is finished igniting, contactless ignition is hightailed touch part (not representing among the figure).The complementary work that ramjet propulsion device 4 is done is by push rod 3 and be arranged on outside power take-off 7 on the hollow rotor shafts 2 is output in.
Among Fig. 3, the quiet moving pipe of fuel connects seal arrangement 5 and is made of hollow rotor shafts 2 and inner oil seal 8, bearing 9, outer oil seal 10, sealing fluid 11, seal arrangement shell 12 and fuel injection dead axle pipe 13.Assembly method is: the opening end in hollow rotor shafts 2 inserts the interior core assembly of being made up of inner oil seal 8, bearing 9, outer oil seal 10, sealing fluid 11 and fuel injection dead axle pipe 13, the end of the quiet pipe 6 of fuel supply is communicated with the outer end that fuel injects dead axle pipe 13, and 2 interior the connections with hollow rotor shafts 2 of the inner insertion hollow rotor shafts that fuel injects dead axle pipe 13 constitute the fuel supply house steward; For replenishing the sealing fluid 11 of loss gradually, sealing fluid auto-feeding device 15 should be set above seal arrangement shell 12, seal arrangement shell 12 is fixed together with frame 1, can not deviate to guarantee the interior core assembly that the quiet moving pipe of fuel connects seal arrangement 5.
Among Fig. 4, the quiet moving pipe of fuel connects seal arrangement 5 and is made of hollow rotor shafts 2 and inner oil seal 8, bearing 9, outer oil seal 10, sealing fluid 11 and seal arrangement shell 12.Assembly method is: the opening end of hollow rotor shafts 2 is run business into particular one to be inserted it into the quiet moving pipe of fuel that is made of outer oil seal 10, bearing 9, inner oil seal 8 and sealing fluid 11 and seal arrangement shell 12 and connects in the seal arrangement 5, and the quiet pipe 6 of fuel supply is communicated with seal arrangement shell 12 and is communicated with hollow rotor shafts 2 and constitutes the fuel supply house steward.For replenishing the constantly sealing fluid 11 of loss, sealing fluid auto-feeding device 15 should be set above seal arrangement shell 12; For preventing that the quiet moving pipe of fuel from connecing seal arrangement 5 and coming off, seal arrangement shell 12 and frame should be fixed together.
Claims (4)
1. rotating athodyd, by frame (1), hollow rotor shafts (2), push rod (3), ignition mechanism, fuel supplying device, the quiet moving pipe of fuel connect seal arrangement and starting arrangement and constitute, and it is characterized in that: with the vertically disposed push rod of hollow rotor shafts (2) (3) on be provided with jet direction and hollow rotor shafts (2), the orthogonal ramjet propulsion device of push rod (3) (4).
2. a kind of rotating athodyd according to claim 1 is characterized in that: the complementary work that ramjet propulsion device (4) is produced is by push rod (3) and be arranged on outside power take-off (7) on the hollow rotor shafts (2) is output in.
3. a kind of rotating athodyd according to claim 1 is characterized in that: when a plurality of ramjet propulsion devices (4) were set, jet propeller (4) can be arranged in the different planes.
4. a kind of rotating athodyd according to claim 1 is characterized in that: the quiet moving pipe of fuel connects seal arrangement (5) and injects dead axle pipe (13) formation by hollow rotor shafts (2) and inner oil seal (8), bearing (9), outer oil seal (10), sealing fluid (11), seal arrangement shell (12) and fuel; In the top of seal arrangement shell (12) sealing fluid auto-feeding device (15) is set.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2008101609914A CN101363387A (en) | 2008-09-17 | 2008-09-17 | Rotating athodyd |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2008101609914A CN101363387A (en) | 2008-09-17 | 2008-09-17 | Rotating athodyd |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101363387A true CN101363387A (en) | 2009-02-11 |
Family
ID=40389943
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2008101609914A Pending CN101363387A (en) | 2008-09-17 | 2008-09-17 | Rotating athodyd |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101363387A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102192045A (en) * | 2010-03-05 | 2011-09-21 | 余志刚 | Stamping type rotor fan engine |
| CN103573470A (en) * | 2012-10-05 | 2014-02-12 | 摩尔动力(北京)技术股份有限公司 | Rotor sprayer-nozzle phase-cycling engine |
| CN104061066A (en) * | 2013-08-07 | 2014-09-24 | 摩尔动力(北京)技术股份有限公司 | Rotor motor for gas liquefied materials |
| CN105736148A (en) * | 2016-02-18 | 2016-07-06 | 江西洪都航空工业集团有限责任公司 | Gunpowder starting device of aircraft engine |
| CN106438107A (en) * | 2016-09-22 | 2017-02-22 | 姚永新 | Blade propeller side jet type aeroengine |
| CN107191290A (en) * | 2017-04-19 | 2017-09-22 | 西北工业大学 | A kind of dynamic power machine of the spiral pulse-knocking engine of application |
| CN110273784A (en) * | 2018-03-13 | 2019-09-24 | 姚永新 | Screw eruption type engine |
| CN110469367A (en) * | 2018-10-25 | 2019-11-19 | 姚永新 | Generous body leaf starches active force structure engine |
-
2008
- 2008-09-17 CN CNA2008101609914A patent/CN101363387A/en active Pending
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102192045A (en) * | 2010-03-05 | 2011-09-21 | 余志刚 | Stamping type rotor fan engine |
| CN103573470A (en) * | 2012-10-05 | 2014-02-12 | 摩尔动力(北京)技术股份有限公司 | Rotor sprayer-nozzle phase-cycling engine |
| CN104061066A (en) * | 2013-08-07 | 2014-09-24 | 摩尔动力(北京)技术股份有限公司 | Rotor motor for gas liquefied materials |
| CN105736148A (en) * | 2016-02-18 | 2016-07-06 | 江西洪都航空工业集团有限责任公司 | Gunpowder starting device of aircraft engine |
| CN106438107A (en) * | 2016-09-22 | 2017-02-22 | 姚永新 | Blade propeller side jet type aeroengine |
| CN107191290A (en) * | 2017-04-19 | 2017-09-22 | 西北工业大学 | A kind of dynamic power machine of the spiral pulse-knocking engine of application |
| CN110273784A (en) * | 2018-03-13 | 2019-09-24 | 姚永新 | Screw eruption type engine |
| CN110469367A (en) * | 2018-10-25 | 2019-11-19 | 姚永新 | Generous body leaf starches active force structure engine |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20090211 |