CN105888878A - Turbineless jet engines - Google Patents
Turbineless jet engines Download PDFInfo
- Publication number
- CN105888878A CN105888878A CN201610261774.9A CN201610261774A CN105888878A CN 105888878 A CN105888878 A CN 105888878A CN 201610261774 A CN201610261774 A CN 201610261774A CN 105888878 A CN105888878 A CN 105888878A
- Authority
- CN
- China
- Prior art keywords
- combustor
- jet
- turbofan
- internal combustion
- cylindrical
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention relates to an internal combustion type turbineless jet engine and an electromagnetism type turbineless jet engine. The internal combustion type turbineless jet engine and the electromagnetism type turbineless jet engine do not need a turbine, so that the structure of a prior jet engine is changed completely. The internal combustion type turbineless jet engine and the electromagnetism type turbineless jet engine comprise shell bodies, force bearing frameworks, shafts, bearings, outer channels, adjustable air inlet ports, combustible gas mixture pipes, internal combustion type or electromagnetism type engine bodies, turbofans, gas compressors, cyclones, oxygen and oil supplying pipes, afterburning nozzles, combustion chambers, sparking plugs and adjustable injection pipes. When starting, under the control of a computer, the internal combustion type engine body or the electromagnetism type engine body rotates at high speed to drive the turbofan, the shaft and the gas compressor to run at high speed to convey air to the combustion chamber; the afterburning nozzle injects oil automatically, the sparking plug ignites and bursts automatically, and then the injection pipe would jet great air flow to push an airplane or a guided missile to fly at supersonic speed. The turbineless jet engines are simpler in structure, more scientific, lower in fuel consumption, greater in thrust, faster in speed, lower in noise and cost, easier to maintain, operate and manufacture, and great in commercial development value. The turbineless jet engines provided by the invention are the most advanced turbineless jet engines in the world.
Description
Technical field
The present invention relates to a kind of internal combustion shaped spray without turbine without turbojet and a kind of electromagnetic type
Gas electromotor.
Background technology
The jet engine occurred in the market, the entirely jet engine of band turbine,
They structures are complicated, manufacture difficulty, maintenance difficulty, and thrust is little, and noise is big, and oil consumption is high, and cost is high,
Entirely by utilize the high-pressure gas in combustor to promote turbine rotation, turbine rotation band moving axis and wind
Fan and compressor work, consume the huge energy, also have lost substantial amounts of heat energy, make spray
The power of gas electromotor reduces, and oil consumption is increased, and noise increases, and wants to reduce oil consumption, and reduction is made an uproar
Sound, improves thrust, only removes combustor turbine below, just can remove resistance, structure letter
Single, thrust could be improved, reduce oil consumption, reduce noise, but, current technology is limited, also
Can not remove turbine, present fossil energy is the most exhausted, energy shortage, and oil price is expensive, only
Creating new engine energetically, save the energy, conservation of nature environment is only absolute principle, and today, I invented
A kind of novel jet engine, it need not combustor turbine below and carrys out work, eliminate
Resistance, it is to be mounted with that after air inlet an internal combustion shaped or electromagnetic type electromotor are to drive whirlpool
Fan and axle and compressor work, it changes the structure of existing jet engine completely, its knot
Structure is simpler, and more scientific, oil consumption is lower, and thrust is bigger, and faster, noise is less for speed, becomes
This is lower, and maintenance operation is simpler, it is easier to manufacture.Manufacture a kind of internal combustion shaped without turbine
Jet engine, it is to be combined into one by jet engine part and internal combustion shaped engine section
, jet engine part: include that housing, by-pass air duct, adjustable scoop, internal combustion shaped start
Machine, turbofan, compressor, cyclone, oxygen supply and fuel feed pump, step-up jet, combustor, can
Adjust jet pipe, fire mixture pipe, articulation, bearing, load-bearing frame, internal combustion shaped engine section:
Including cylindrical, flywheel, turbofan, axle, combustion mixture pipe, spring, compression ring, spark plug, spray
Gas device, combustor, brush, electric wire, computer, instrument and meter, electrical switch, novel jet
The invention of electromotor, will bring a revolution, its energy to the industry manufacturing jet engine
Realize low oil consumption, low stain, low emission, low noise, high efficiency, high reliability, runnability
The environmental protection jet engine that energy is good, digital control with computer, can be manual or full-automatic
Starting is started, and it has huge business development to be worth, and will bring huge society's effect for the mankind
Benefit and economic benefit, will save the energy for the mankind, and conservation of nature environment makes huge contribution.
Summary of the invention
The present invention seeks to invent a kind of simple in construction, oil consumption without the purpose of turbojet
Low, thrust-weight ratio is big, speed is fast, noise is little, volume is little, low cost, easily manufacture, green
The new engine of environmental protection again.A kind of internal combustion shaped of the manufacturing is without turbojet, and it is by spraying
Gas engine section and internal combustion shaped engine section are combined into one, jet engine part:
Including housing, by-pass air duct, adjustable scoop, internal combustion shaped electromotor, turbofan, compressor, rotation
Stream device, oxygen supply and fuel feed pump, step-up jet, combustor, adjustable jet, combustion mixture pipe,
Articulation, bearing, load-bearing frame, internal combustion shaped engine section: include cylindrical, flywheel, whirlpool
Fan, axle, combustion mixture pipe, spring, compression ring, spark plug, air blast, combustor, brush,
Electric wire, computer, instrument and meter, electrical switch, it is tied than the jet engine of present band turbine
Structure is simpler, more scientific, oil consumption is lower, thrust is bigger, speed faster, noise is less, become
This is the lowest, maintenance operation is simpler, be more easily manufactured, digital control with computer, can manually or
Full-automatic starting is started, and it can realize low oil consumption, low stain, low emission, low noise, height
Efficiency, high reliability, behavior in service good without turbojet.
The technical scheme is that and be achieved in that: a kind of internal combustion shaped without turbojet,
It is combined into one by jet engine part and internal combustion shaped engine section, and jet is started
Machine part: include housing, by-pass air duct, adjustable scoop, internal combustion shaped electromotor, turbofan, pressure
Mechanism of qi, cyclone, oxygen supply mix with fuel feed pump, step-up jet, combustor, adjustable jet, combustion
Close trachea, articulation, bearing, load-bearing frame, internal combustion shaped engine section: include cylindrical,
Flywheel, turbofan, axle, combustion mixture pipe, spring, compression ring, spark plug, air blast, burning
Room, brush, electric wire, computer, instrument and meter, electrical switch, it is characterised in that: in burning
Fumarole is had bottom room, and equipped with step-up jet and spark plug, outside internal combustion shaped electromotor
A circle part is drilled with aperture, and aperture, through by-pass air duct waste air, is also steam vent;Cylindrical one
Point not bore aperture serve as base, closely matches with the compression ring of combustor cylinder body, is
Seal, air in by-pass air duct be dispel the heat with the shell of combustor to cylindrical, cylindrical built-in
Having flywheel, flywheel is built with turbofan, turbofan centre equipped with axle, and axle centre drill is porose, hole
It is used to conveying combustion gaseous mixture, equipped with articulation on combustion mixture pipe, equipped with burning in flywheel
Room, spring, compression ring, spark plug, air blast, fires mixture pipe, brush, electric wire, igniting
Coil, has two circular ports and is used to fill combustor cylinder body, compression ring and spring in flywheel,
It is initially charged with spring, compression ring, reinstalls combustor cylinder body, the elastic force of spring according to actual needs may be used
Adjust, spring compression ring is tightly pushed down and cylindrical base seal, in combustor cylinder body termination built with
Spark plug and air blast, when flywheel and combustor cylinder body are through cylindrical base, during imperforate section, just
Automatic ignition breaks out;When flywheel and combustor cylinder body are through cylindrical base, when having porose area, the most certainly
Dynamic waste air, such reciprocating operation starts, and during light, first starts computer, uses
Computer controls, and restarts internal combustion shaped electromotor, and at this moment air blast will spray combustion gaseous mixture automatically,
Spark plug will break out by automatic ignition, under the promotion of explosive force, and the recoil strength of round bottom seat outside
Under promotion, promote flywheel turns, flywheel turns drive turbofan rotate, turbofan rotational band moving axis with
Compressor run up conveying air will automatically spray to combustor, the step-up jet in combustor
Oil, spark plug will automatic ignition outburst, jet pipe will spray huge air-flow promote aircraft,
Guided missile supersonic flight.
A kind of electromagnetic type of the present invention is without turbojet, and it is by jet engine part
It is combined into one with electromagnetic type engine section, jet engine part: include housing, outer
Duct, adjustable scoop, electromagnetic type electromotor, turbofan, compressor, cyclone, oxygen supply with
Fuel feed pump, step-up jet, combustor, adjustable jet, bearing, load-bearing frame, spark plug,
Electromotor, charger, accumulator, brush, electric wire, computer, instrument and meter, electrical switch,
Electromagnetic type engine section: include armature, permanent magnet, axle, turbofan, electromagnetism be by armature and
Permanent magnet composition, be to utilize the shifting magnetic field relying on electric current to produce to promote permanent magnet and turbofan
Rotate, it is characterised in that: at the cylindrical of electromagnetic type electromotor built with armature, outside inner circle
Equipped with permanent magnet, in inner circle built with turbofan, the centre of turbofan, equipped with axle, starts jet
During electromotor, first start computer, use computer control, restart electromotor or by accumulator, open
Dynamic switch, electromagnetic type electromotor high-speed rotation will drive turbofan to run up with compressor with axle
Conveying air to combustor, the step-up jet in combustor will automatic oil spout, spark plug will
Automatic ignition breaks out, and jet pipe will spray huge air-flow and promote aircraft, guided missile supersonic flight.
To breeze up without turbojet above, internal combustion shaped can be increased or electromagnetic type starts
Machine or add fan before turbofan, wind-force is more powerful.
Advantages of the present invention: invention novelty, practical, create without turbojet,
It changes the structure of existing jet engine completely, and its structure is simpler, more scientific, oil consumption
Lower, thrust is bigger, speed faster, noise less, cost is lower, and maintenance operation is simpler,
It is more easily manufactured, uses computer control, can manually or full-automatic start, it has huge business
Development volue, is the most state-of-the-art without turbojet.
Accompanying drawing illustrates:
Fig. 1 is a kind of internal combustion shaped structural representation without turbojet of the present invention;
Fig. 2 is the structural representation that the right side of Fig. 1 regards;
Fig. 3 is a kind of electromagnetic type structural representation without turbojet of the present invention;
Fig. 4 is the structural representation that the right side of Fig. 3 regards
Detailed description of the invention:
As shown in Figure 1, 2, a kind of internal combustion shaped is without turbojet, and it is to be by spraying by it
Gas engine section and internal combustion shaped engine section are combined into one, jet engine part:
Including housing 1, by-pass air duct, adjustable scoop 2, internal combustion shaped electromotor 3, turbofan 4, calm the anger
Machine 5, cyclone 6, oxygen supply and fuel feed pump 7, step-up jet 8, combustor 9, adjustable jet
10, combustion mixture pipe 11, articulation 12, bearing, load-bearing frame, 3, internal combustion shaped electromotor
Point: include cylindrical 13, flywheel 14, turbofan 4, axle 15, combustion mixture pipe 16, spring 17,
Compression ring 18, spark plug 19, air blast 20, combustor 21, brush, electric wire, computer, instrument
Instruments and meters, electrical switch, it is characterised in that: bottom combustor 9, have fumarole, and fill
Having step-up jet 8 and spark plug, cylindrical 13 part at internal combustion shaped electromotor 3 is drilled with aperture,
Aperture, through by-pass air duct waste air, is also steam vent;It is to use that cylindrical 13 part does not bore aperture
Make base, closely match with the compression ring 18 of combustor 21 cylinder body, be to seal, outward
Air in duct be to the shell heat radiation of cylindrical 13 and combustor 9, cylindrical 13 built with
Flywheel 14, flywheel 14 built with turbofan 4, turbofan 4 centre equipped with axle 15, in axle 15
The heart is drilled with hole, and hole is used to conveying combustion gaseous mixture, equipped with articulation 12 on combustion mixture pipe 11,
Equipped with combustor 21 in flywheel 14, spring 17, compression ring 18, spark plug 19, air blast 20,
Combustion mixture pipe 16, brush, electric wire, ignition coil, having two circular ports in flywheel 14 is
It is used for filling combustor 21 cylinder body, compression ring 18 and spring 17, is initially charged with spring 17, compression ring
18, reinstall combustor 21 cylinder body, spring 17 elastic force the most adjustable, spring
Compression ring 18 is tightly pushed down and the sealing of cylindrical 13 base by 17, built-in in combustor 21 cylinder body termination
There are spark plug 19 and air blast 20, when flywheel 14 and combustor 21 cylinder body are through cylindrical 13 end
Seat, during imperforate section, breaks out with regard to automatic ignition;When flywheel 14 and combustor 21 cylinder body are through outward
Circle 13 bases, when having porose area, with regard to automatic waste discharge gas, such reciprocating operation starts, and starts jet
During electromotor, first start computer, use computer control, restart internal combustion shaped electromotor, at this moment spray
Gas device 20 will spray combustion gaseous mixture automatically, and spark plug 19 will break out by automatic ignition, in outburst
Under the promotion of power, under the recoil strength of cylindrical 13 base promotes, promote flywheel 14 to rotate, fly
Wheel 14 rotation drives turbofan 4 to rotate, turbofan 4 rotational band moving axis 15 and compressor 5 fortune at a high speed
Transfer send air to combustor 9, the step-up jet 8 in combustor 9 will automatic oil spout, spark
Plug will break out by automatic ignition, and jet pipe 10 will spray huge air-flow and promote aircraft, guided missile to surpass
Sonic flight.
As shown in Figure 3,4, a kind of electromagnetic type is without turbojet, and it is to be started by jet
Machine part and electromagnetic type engine section are combined into one, jet engine part: include shell
Body 1, by-pass air duct, adjustable scoop 2, electromagnetic type electromotor 22, turbofan 23, compressor 5,
Cyclone 6, oxygen supply and fuel feed pump 7, step-up jet 8, combustor 9, adjustable jet 10, axle
Hold, load-bearing frame, spark plug, electromotor, charger, accumulator, brush, electric wire, electricity
Brain, instrument and meter, electrical switch, electromagnetic type electromotor 22 part: include armature 24, permanent magnetism
Ferrum 25, turbofan 23, axle 26, electromagnetism are made up of armature and permanent magnet, are to utilize to rely on electricity
The shifting magnetic field of miscarriage life promotes permanent magnet 25 and turbofan 23 to rotate, it is characterised in that:
It is at the cylindrical of electromagnetic type electromotor 22 built with armature 24, outer equipped with permanent magnet 25 in inner circle,
In inner circle built with turbofan 23, the centre of turbofan 23, equipped with axle 26, starts jet and starts
During machine, first starting computer, use computer control, restart electromotor or by accumulator, startup is opened
Closing, electromagnetic type electromotor 22 high-speed rotation will drive turbofan 23 and axle 26 high with compressor 5
Speed operating conveying air to combustor 9, the step-up jet 8 in combustor 9 will automatic oil spout,
Spark plug will break out by automatic ignition, and jet pipe 10 will spray huge air-flow to promote aircraft, lead
Play supersonic flight.
Claims (2)
1. internal combustion shaped is without a turbojet, and it is by jet engine part and internal combustion
H type engine h part is combined into one, jet engine part: include housing (1), outer culvert
Road, adjustable scoop (2), internal combustion shaped electromotor (3), turbofan (4), compressor (5),
Cyclone (6), oxygen supply and fuel feed pump (7), step-up jet (8), combustor (9), adjustable
Jet pipe (10), combustion mixture pipe (11), articulation (12), bearing, load-bearing frame, internal combustion
H type engine h (3) part: include cylindrical (13), flywheel (14), turbofan (4), axle (15),
Combustion mixture pipe (16), spring (17), compression ring (18), spark plug (19), air blast (20),
Combustor (21), brush, electric wire, computer, instrument and meter, electrical switch, it is characterised in that:
A fumarole is had in combustor (9) bottom, and equipped with step-up jet (8) and spark plug,
Cylindrical (13) part for internal combustion shaped electromotor (3) is drilled with aperture, and aperture is through by-pass air duct waste discharge
Gas, be also steam vent;Cylindrical (13) part is not bored aperture and is served as base,
Closely match with the compression ring (18) of combustor (21) cylinder body, be to seal, in by-pass air duct
Air be dispel the heat with the shell of combustor (9) to cylindrical (13), cylindrical (13) built-in
Having flywheel (14), flywheel (14) fills built with the centre of turbofan (4), turbofan (4)
Having axle (15), axle (15) centre drill is porose, and hole is used to conveying combustion gaseous mixture, combustion mixing
Equipped with articulation (12) on trachea (11), flywheel (14) is inner equipped with combustor (21), bullet
Spring (17), compression ring (18), spark plug (19), air blast (20), combustion mixture pipe (16),
Brush, electric wire, ignition coil, have two circular ports and be used to dress burning in flywheel (14)
Room (21) cylinder body, compression ring (18) and spring (17), it is initially charged with spring (17), compression ring
(18), reinstall combustor (21) cylinder body, the elastic force of spring (17) according to actual needs may be used
Adjusting, compression ring (18) is tightly pushed down and is sealed with cylindrical (13) base, in combustion by spring (17)
Burning room (21) cylinder body termination is built with spark plug (19) and air blast (20), when flywheel (14)
With combustor (21) cylinder body through cylindrical (13) base, during imperforate section, quick-fried with regard to automatic ignition
Send out;When flywheel (14) and combustor (21) cylinder body are through cylindrical (13) base, there is porose area
Time, with regard to automatic waste discharge gas, such reciprocating operation starts, and during light, first starts
Computer, uses computer control, restarts internal combustion shaped electromotor, and at this moment air blast (20) will be certainly
Dynamic spray combustion gaseous mixture, spark plug (19) will break out by automatic ignition, under the promotion of explosive force,
Under the recoil strength of cylindrical (13) base promotes, flywheel (14) is promoted to rotate, flywheel (14)
Rotate and drive turbofan (4) to rotate, turbofan (4) rotational band moving axis (15) and compressor (5)
Run up conveying air to combustor (9), the step-up jet (8) in combustor (9) is just
Meeting automatic oil spout, spark plug will break out by automatic ignition, and jet pipe (10) will spray huge
Air-flow promotes aircraft, guided missile supersonic flight.
2. electromagnetic type is without a turbojet, and it is by jet engine part and electromagnetism
H type engine h part is combined into one, jet engine part: include housing (1), outer culvert
Road, adjustable scoop (2), electromagnetic type electromotor (22), turbofan (23), compressor (5),
Cyclone (6), oxygen supply and fuel feed pump (7), step-up jet (8), combustor (9), adjustable
Jet pipe (10), bearing, load-bearing frame, spark plug, electromotor, charger, accumulator, electricity
Brush, electric wire, computer, instrument and meter, electrical switch, electromagnetic type electromotor (22) part:
It is by armature including turbofan (23), armature (24), permanent magnet (25), axle (26), electromagnetism
With permanent magnet composition, it is to utilize the shifting magnetic field relying on electric current to produce to promote permanent magnet (25)
Rotate with turbofan (23), it is characterised in that: in the cylindrical of electromagnetic type electromotor (22)
Equipped with armature (24), outer equipped with permanent magnet (25) in inner circle, in inner circle built with turbofan (23),
The centre of turbofan (23) is equipped with axle (26), during light, first starts computer,
Use computer control, restart electromotor or with accumulator, activate switch, electromagnetic type electromotor (22)
High-speed rotation turbofan (23) and axle (26) and compressor (5) will be driven to run up conveying
Air to combustor (9), the step-up jet (8) in combustor (9) will automatic oil spout,
Spark plug will automatic ignition outburst, jet pipe (10) will spray huge air-flow promote aircraft,
Guided missile supersonic flight.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610261774.9A CN105888878A (en) | 2016-04-18 | 2016-04-18 | Turbineless jet engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610261774.9A CN105888878A (en) | 2016-04-18 | 2016-04-18 | Turbineless jet engines |
Publications (1)
Publication Number | Publication Date |
---|---|
CN105888878A true CN105888878A (en) | 2016-08-24 |
Family
ID=56705310
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610261774.9A Pending CN105888878A (en) | 2016-04-18 | 2016-04-18 | Turbineless jet engines |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN105888878A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106005402A (en) * | 2016-06-18 | 2016-10-12 | 夏建国 | Flying saucer type hypersonic stealth jet aircraft capable of realizing vertical take-off and landing |
CN106121861A (en) * | 2016-06-21 | 2016-11-16 | 王启振 | Jet engine without efficient turbine |
CN106224126A (en) * | 2016-08-29 | 2016-12-14 | 曾令霞 | Intermediate layer and the jet engine of following height |
CN106837531A (en) * | 2017-02-19 | 2017-06-13 | 夏建国 | Gas type saves at a high speed force engine |
CN107701313A (en) * | 2017-11-10 | 2018-02-16 | 中国空气动力研究与发展中心计算空气动力研究所 | A kind of electric mixed aviation engine of oil |
CN108518289A (en) * | 2018-05-17 | 2018-09-11 | 南京航空航天大学 | A kind of blade tip jet is from driving wheel-type Duct-Burning Turbofan |
CN109098841A (en) * | 2018-08-11 | 2018-12-28 | 芜湖市新海域智能科技有限公司 | A kind of automobile engine using new energy resources energy-saving emission-reducing apparatus |
CN109236494A (en) * | 2018-11-01 | 2019-01-18 | 夏丰 | Ultrahigh speed thrust vectoring jet engine |
CN112228245A (en) * | 2020-09-08 | 2021-01-15 | 邵阳学院 | Non-turbine type ultrahigh-speed thrust vector jet engine |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2631107Y (en) * | 2003-07-02 | 2004-08-04 | 曹玉刚 | Integrated electric generator |
CN2645326Y (en) * | 2003-08-04 | 2004-09-29 | 梁荣富 | Permanent-magnetic DC brushless motor for electric vehicle |
CN1747290A (en) * | 2004-09-08 | 2006-03-15 | 有限会社金星研究所 | Motor and devive using this |
CN101338702A (en) * | 2008-07-23 | 2009-01-07 | 周林 | Pulse knock rotor spindle engine |
CN101649781A (en) * | 2008-08-11 | 2010-02-17 | 刘佳骏 | Jet engine |
CN101725431A (en) * | 2008-10-31 | 2010-06-09 | 南昌航空大学 | Electric fuel oil jet propeller |
CN102452401A (en) * | 2010-11-01 | 2012-05-16 | 吴德滨 | Ultrahigh-speed train with electromagnetic-induction turbine engine |
CN102493868A (en) * | 2011-12-28 | 2012-06-13 | 韩小余 | Intelligent efficient engine and control method |
CN103629011A (en) * | 2013-11-21 | 2014-03-12 | 孙朝宽 | Engine |
-
2016
- 2016-04-18 CN CN201610261774.9A patent/CN105888878A/en active Pending
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2631107Y (en) * | 2003-07-02 | 2004-08-04 | 曹玉刚 | Integrated electric generator |
CN2645326Y (en) * | 2003-08-04 | 2004-09-29 | 梁荣富 | Permanent-magnetic DC brushless motor for electric vehicle |
CN1747290A (en) * | 2004-09-08 | 2006-03-15 | 有限会社金星研究所 | Motor and devive using this |
CN101338702A (en) * | 2008-07-23 | 2009-01-07 | 周林 | Pulse knock rotor spindle engine |
CN101649781A (en) * | 2008-08-11 | 2010-02-17 | 刘佳骏 | Jet engine |
CN101725431A (en) * | 2008-10-31 | 2010-06-09 | 南昌航空大学 | Electric fuel oil jet propeller |
CN102452401A (en) * | 2010-11-01 | 2012-05-16 | 吴德滨 | Ultrahigh-speed train with electromagnetic-induction turbine engine |
CN102493868A (en) * | 2011-12-28 | 2012-06-13 | 韩小余 | Intelligent efficient engine and control method |
CN103629011A (en) * | 2013-11-21 | 2014-03-12 | 孙朝宽 | Engine |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106005402A (en) * | 2016-06-18 | 2016-10-12 | 夏建国 | Flying saucer type hypersonic stealth jet aircraft capable of realizing vertical take-off and landing |
CN106005402B (en) * | 2016-06-18 | 2018-09-04 | 夏建国 | Flying disk type VTOL hypersonic speed jet stealth aircraft |
CN106121861A (en) * | 2016-06-21 | 2016-11-16 | 王启振 | Jet engine without efficient turbine |
CN106224126A (en) * | 2016-08-29 | 2016-12-14 | 曾令霞 | Intermediate layer and the jet engine of following height |
CN106837531A (en) * | 2017-02-19 | 2017-06-13 | 夏建国 | Gas type saves at a high speed force engine |
CN107701313A (en) * | 2017-11-10 | 2018-02-16 | 中国空气动力研究与发展中心计算空气动力研究所 | A kind of electric mixed aviation engine of oil |
CN108518289A (en) * | 2018-05-17 | 2018-09-11 | 南京航空航天大学 | A kind of blade tip jet is from driving wheel-type Duct-Burning Turbofan |
CN109098841A (en) * | 2018-08-11 | 2018-12-28 | 芜湖市新海域智能科技有限公司 | A kind of automobile engine using new energy resources energy-saving emission-reducing apparatus |
CN109236494A (en) * | 2018-11-01 | 2019-01-18 | 夏丰 | Ultrahigh speed thrust vectoring jet engine |
CN109236494B (en) * | 2018-11-01 | 2022-09-23 | 夏丰 | Ultrahigh-speed thrust vector jet engine |
CN112228245A (en) * | 2020-09-08 | 2021-01-15 | 邵阳学院 | Non-turbine type ultrahigh-speed thrust vector jet engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105888878A (en) | Turbineless jet engines | |
CN106065830B (en) | A kind of pulse detonation combustor device combined based on rotary valve with pneumatic operated valve | |
CN201025157Y (en) | Micro turbine jet engine | |
RU2387851C2 (en) | Prechamber rotary ice | |
CN109236494B (en) | Ultrahigh-speed thrust vector jet engine | |
CN102889132B (en) | The launcher of gas-turbine unit | |
CN103233814A (en) | Labor-saving engine | |
CN103195565B9 (en) | Save force engine | |
CN110145396A (en) | Concentric circumferences rotor-type internal combustion engine | |
CN102168610B (en) | Non-turbine rotor internal combustion engine with partition blade chamber | |
CN103629011B (en) | Motor | |
US8850791B2 (en) | Flywheel engine | |
CN102588143B (en) | Minitype turbofan engine | |
CN110714838A (en) | Turbojet engine started by gas | |
CN104234867A (en) | Scramjet engine | |
CN101255801B (en) | High back pressure internal combustion steam turbine | |
CN106930825A (en) | Without compression engine | |
CN202851156U (en) | Starting equipment of gas turbine engine | |
CN202348475U (en) | Micro-turbofan engine | |
CN107218155B (en) | A kind of pulse ignite in advance can steady operation detonation engine | |
CN106089445B (en) | The bullet engine that a kind of high-altitude ignition starts | |
CN108590864A (en) | A kind of small-sized missile turbojet engine cartridge start method and device | |
CN101929406A (en) | Vortex cold vacuum aircraft engine | |
CN101629517A (en) | Jet propulsion method and jet engine | |
CN203717126U (en) | Turbine engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination |