CN110469367A - Generous body leaf starches active force structure engine - Google Patents
Generous body leaf starches active force structure engine Download PDFInfo
- Publication number
- CN110469367A CN110469367A CN201811272113.1A CN201811272113A CN110469367A CN 110469367 A CN110469367 A CN 110469367A CN 201811272113 A CN201811272113 A CN 201811272113A CN 110469367 A CN110469367 A CN 110469367A
- Authority
- CN
- China
- Prior art keywords
- leaf
- slurry
- technical characteristic
- lodicule
- leaf slurry
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/148—Blades with variable camber, e.g. by ejection of fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
Abstract
The research and development of punching engine and practical application basis are that quite richness, leaf slurry technology are even more richer in place of having.The basic structure flattening appearance of punching engine is formed in leaf lodicule, makes have fuel combustion propulsion functions in its leaf lodicule inner cavity.For punching engine it is that flattening holds system in leaf lodicule, and is that generous body becomes active force leaf and starches for leaf slurry.The two is to have the feasibility combined conscientiously in conjunction with from the point of view of from surface.How the two effectively combination novel aero-engine is prepared in practice highly further to explore.
Description
Technical field；1, the present invention relates to aero-engine and combustor technical fields.
Background technique；2, the research and development of punching engine and practical application basis are that quite richness, leaf slurry technology even more had
Place is richer.The basic structure flattening appearance of punching engine is formed in leaf lodicule, makes to have in its leaf lodicule inner cavity
Fuel combustion propulsion functions.It is flattening appearance system for punching engine in leaf lodicule, and is generous for leaf slurry
Body becomes active force leaf and starches.The two is to have the feasibility combined conscientiously in conjunction with from the point of view of from surface.How by the two in practice
Effectively combination prepares novel aero-engine and highly further explores.
Summary of the invention；3, the basic structure flattening appearance of punching engine is formed in leaf slurry, is made in its leaf lodicule inner cavity
Have fuel combustion propulsion functions.Punching engine basis cross-sectional view is understood that just and is tended to have and is conducive to prepare generous body actively
Power leaf slurry, set in punching engine punching press cone be interpreted as in set leaf lodicule, which left and right sides tube wall is exactly two and sets in
The attached leaf lodicule of leaf lodicule two sides sets leaf lodicule by and the attached leaf lodicule in two sides is added to form whole active force leaf slurry, prepares integral
Impeller and on the hollow spindle be exactly brand new engine.In set leaf slurry front side end non-rear end material spray flame windward, two
The attached leaf lodicule inner wall front end portion in side is air contracting function, and rear tail portion is combustion chamber and promotes spout, and outer wall is exactly moving
It is middle to be radiated by active air cooling.The basic function principle of punching engine so does not change, only its flattening in leaf slurry
Form completely new leaf slurry.Then impeller is made and on the hollow spindle in engine tube sandwich type element.Make this impeller ten
It is whole that ten pedestal of main shaft, ten spindle carrier, ten motor body forms engine.Since impeller slurry thrust backward can claim this impeller
For postposition active force impeller or postposition impeller, pushes ahead good but main shaft can be placed in forward among raging fire appearance refining certainly.Phase
It closes engine start and can be used in main shaft frame completely and ten high-speed transmission of motor, ten leaf slurry main shaft is set to realize, starting is just
Normal Rear Derailleur separated with leaf paddle wheel main shaft both can, preparation blade wheel group and this will be referred to as preposition blade wheel in motor front end,
After speed changer is separated with leaf slurry main shaft, motor is converted into generator, preposition blade wheel group provides wind-force this moment for generator
Kinetic energy, while having the function of the protection cover of protection engine at extreme rear active force impeller again.
Technical solution；
Active force leaf described in one, slurry structure technical characteristic be；The basic structure flattening appearance of punching engine is formed on
In leaf slurry, make have fuel combustion propulsion functions technical characteristic in its leaf lodicule inner cavity.Punching engine basis cross-sectional view this
Sample, which understands just and tends to have, is conducive to prepare generous body active force leaf slurry, set in punching engine punching press cone be interpreted as in set leaf slurry
Piece, which left and right sides tube wall is exactly two attached leaf lodicules that leaf lodicule two sides are set in, leaf lodicule is set by, two sides is added to pay leaf
Lodicule forms whole leaf slurry, produces the active force technical characteristic leaf slurry of brand new.In set on front side of leaf lodicule rear side flame windward,
The attached leaf slurry in two sides is pressurized the technical pattern feature of combustion-supporting boosting during exercise.(auspicious to see diagram)
Leaf slurry technical characteristic is set in described in two, is；In to set leaf slurry ectosome be to set punching in v bathtub construction and punching engine
Pressure cone attribute is consistent, and inner body slot type structure feature, which can be v channel-shaped, can also be u channel-shaped, and v or u mouthfuls are just combustion spout, has outside v
Function of increasing pressure windward, inside groove be fuel eruption at technical characteristic, can this will be referred to as in set leaf slurry stern notch spout.(auspicious to see diagram)
Leaf slurry v nozzle back segment flame stabilizer technical characteristic is set in described in three, is；The hole of v spout two sides is set
Formula batten, it can be understood as turbojet engine burns indoor porous tubular device battenization preparation in spout two sides.
Four, the position of the fuel nozzle ports and technical characteristic: on the outer wall of the main shaft impeller center penetrating with bead core
Set in leaf slurry stern notch spout line correspondences prepare, impeller center spout spray fuel along in set leaf slurry stern notch in burning and from
In set leaf slurry stern notch spout spray generate thrust technical characteristic.
Five, it is described in set leaf slurry independent utility technical characteristic be；It subtracts attached leaf slurry and widens in V formula and set leaf slurry, can make to fire
Material sets the technical characteristic for generating power in leaf slurry after just combustion from V mouthfuls of eruptions in V formula.And linear dotted arrangement is equipped at the bottom V
Aperture is pressurized combustion-supporting technical characteristic to increase gas.
Beneficial effect；It has been weighed much than punching engine, has increased the components such as motor power main shaft and two groups of impellers, just open
Dynamic to starch resultant force with active force leaf by motor, the success rate and reliability of starting can be more powerful.Fuel-air heat is superimposed combustion twice
It burns, once starches inner cavity in leaf, once then generate thrust backward in shell tail pipe inner cavity, Theoretical combustion rate can be higher more energy efficient.
Surface see it is lighter than turbojet engine by 50 percent, due to have heat must there is cold wind to cool down to material structural design theory on manufacture
Material technology can reduce by 50 percent, manufacturing cost expense meeting bottom 50 percent, if can reach the same of turbojet engine
Power, theoretically probably, the beneficial effect after realization can not be imagined.Can not achieve it is also that highly desirable combustor has
The no small market space.The gas night fluid fuel that can complete eruption burning as combustor much theoretically can all be applied.
Detailed description of the invention
Fig. 1；The technical characteristic figure of active force leaf slurry structure.It is as follows to represent component for each label in attached drawing；Leaf is set in 1.V formula
Slurry.2. attached leaf lodicule.3. leaf slurry V formula fuel combustion spout is set in.4. leaf starches nozzle.5. slatted securing bracket.6. burning
Room.
Fig. 2；Complete machine schematic diagram.It is as follows to represent component for each label in attached drawing；1. active force leaf starches .2. main tapping and impeller is pacified
At dress.Accelerate clutch installation place 3. becoming.4. the slatted bracket of main shaft frame, fuel exists through this bracket to main shaft inner cavity by the way that shell is outer
Burning generates thrust in active force leaf slurry.5. the preposition impeller installation place of motor.6. preposition blade.7. tubular type casing shell.8.
Inside and outside shell tube-sheet type connecting bracket.9. tubular type casing inner casing.10. tail mouth thrust direction.
Specific embodiment
All components ten refer to denumerable.Common machine pincers worker two working days in the conditionally complete situation of workmanship easily make non-
Standard specimen machine.Commercialization can be entered within 3 to 6 months in conditionally complete situation as combustor.If engine is quick-fried with gas-liquid height
A possibility that 2 to 3 months heavens of fuel, is very big.Conventional fuel needs the long period by each item number tool reserve requirements in basis.
Claims (5)
1. the technical characteristic of the active force leaf slurry structure is；The basic structure flattening appearance of punching engine is formed on leaf slurry
In, make have fuel combustion propulsion functions technical characteristic in its leaf lodicule inner cavity.Punching engine basis cross-sectional view is managed in this way
Solution just and tends to have and is conducive to prepare generous body active force leaf slurry, set in punching engine punching press cone be interpreted as in set leaf lodicule, which
Left and right sides tube wall is exactly two attached leaf lodicules that leaf lodicule two sides are set in, leaf lodicule is set by, two sides is added to pay leaf lodicule shape
Integral leaf slurry produces the active force technical characteristic leaf slurry of brand new.In set on front side of leaf lodicule that rear side flame, two sides are attached windward
Leaf starches the technical pattern feature for being pressurized combustion-supporting boosting during exercise.(auspicious to see diagram).
2. setting leaf slurry technical characteristic in described is；In to set leaf slurry ectosome be that punching press cone is set in v bathtub construction and punching engine
Attribute is consistent, and inner body slot type structure feature, which can be v channel-shaped, can also be u channel-shaped, and v or u mouthfuls are just combustion spout, has windward outside v
Function of increasing pressure, inside groove be fuel eruption at technical characteristic, can this will be referred to as in set leaf slurry stern notch spout.(auspicious to see diagram).
3. setting leaf slurry v nozzle back segment flame stabilizer technical characteristic in described is；The cellular type item of v spout two sides is set
Plate, it can be understood as turbojet engine burns indoor porous tubular device battenization preparation in spout two sides.
4. position and the technical characteristic of the fuel nozzle ports: being set on the outer wall of the main shaft impeller center penetrating with bead core
Leaf is starched stern notch spout line correspondences and is prepared, and the fuel that impeller center spout sprays is set along in burn in leaf slurry stern notch and therefrom set leaf
It starches stern notch spout and sprays the technical characteristic for generating thrust.
5. the technical characteristic for setting leaf slurry independent utility in described is；It subtracts attached leaf slurry and widens in V formula and set leaf slurry, fuel can be made in V
The technical characteristic for generating power in leaf slurry after just combustion from V mouthfuls of eruptions is set in formula.And it is used in the aperture that the bottom V is equipped with linear dotted arrangement
Combustion-supporting technical characteristic is pressurized to increase gas.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811272113.1A CN110469367A (en) | 2018-10-25 | 2018-10-25 | Generous body leaf starches active force structure engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811272113.1A CN110469367A (en) | 2018-10-25 | 2018-10-25 | Generous body leaf starches active force structure engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110469367A true CN110469367A (en) | 2019-11-19 |
Family
ID=68504662
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811272113.1A Pending CN110469367A (en) | 2018-10-25 | 2018-10-25 | Generous body leaf starches active force structure engine |
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1173144A (en) * | 1965-10-14 | 1969-12-03 | Rolls Royce | Power Plants including a Ducted Fan |
| CN2526515Y (en) * | 2002-03-21 | 2002-12-18 | 高恒伟 | High-supersonic vortex pressurizing propelling engine |
| US20050016157A1 (en) * | 2003-07-22 | 2005-01-27 | National Aerospace Laboratory Of Japan | Combined engine for single-stage spacecraft |
| US20070056290A1 (en) * | 2005-09-09 | 2007-03-15 | The Regents Of The University Of Michigan | Rotary ramjet turbo-generator |
| CN101363387A (en) * | 2008-09-17 | 2009-02-11 | 王学章 | Rotating athodyd |
| US20110173985A1 (en) * | 2008-07-11 | 2011-07-21 | Daniel Peyrisse | Thruster comprising a plurality of rocket motors |
| US20140047816A1 (en) * | 2011-03-01 | 2014-02-20 | Grollo Aerospace | Engine for use in an aerial vehicle |
| CN104234868A (en) * | 2013-06-13 | 2014-12-24 | 陶财德 | Vane-shaped scramjet engine |
-
2018
- 2018-10-25 CN CN201811272113.1A patent/CN110469367A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1173144A (en) * | 1965-10-14 | 1969-12-03 | Rolls Royce | Power Plants including a Ducted Fan |
| CN2526515Y (en) * | 2002-03-21 | 2002-12-18 | 高恒伟 | High-supersonic vortex pressurizing propelling engine |
| US20050016157A1 (en) * | 2003-07-22 | 2005-01-27 | National Aerospace Laboratory Of Japan | Combined engine for single-stage spacecraft |
| US20070056290A1 (en) * | 2005-09-09 | 2007-03-15 | The Regents Of The University Of Michigan | Rotary ramjet turbo-generator |
| US20110173985A1 (en) * | 2008-07-11 | 2011-07-21 | Daniel Peyrisse | Thruster comprising a plurality of rocket motors |
| CN101363387A (en) * | 2008-09-17 | 2009-02-11 | 王学章 | Rotating athodyd |
| US20140047816A1 (en) * | 2011-03-01 | 2014-02-20 | Grollo Aerospace | Engine for use in an aerial vehicle |
| CN104234868A (en) * | 2013-06-13 | 2014-12-24 | 陶财德 | Vane-shaped scramjet engine |
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Application publication date: 20191119 |