CN106593959A - Efficiency-increasing, energy-saving and emission-reducing method for propellers, ruston turbines, fans and turbofans for various uses - Google Patents
Efficiency-increasing, energy-saving and emission-reducing method for propellers, ruston turbines, fans and turbofans for various uses Download PDFInfo
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- CN106593959A CN106593959A CN201710062545.9A CN201710062545A CN106593959A CN 106593959 A CN106593959 A CN 106593959A CN 201710062545 A CN201710062545 A CN 201710062545A CN 106593959 A CN106593959 A CN 106593959A
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- 238000000034 method Methods 0.000 title claims abstract description 18
- 238000004519 manufacturing process Methods 0.000 claims abstract description 13
- 230000002195 synergetic effect Effects 0.000 claims description 25
- 238000007599 discharging Methods 0.000 claims description 18
- 238000005516 engineering process Methods 0.000 claims description 7
- 230000008034 disappearance Effects 0.000 claims description 2
- 238000009434 installation Methods 0.000 abstract description 2
- 238000010348 incorporation Methods 0.000 abstract 1
- 238000005293 physical law Methods 0.000 abstract 1
- 238000004088 simulation Methods 0.000 description 8
- 230000000694 effects Effects 0.000 description 4
- 241001075561 Fioria Species 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 238000001338 self-assembly Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 241000883990 Flabellum Species 0.000 description 1
- 238000005276 aerator Methods 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000009738 saturating Methods 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
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- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/023—Blade-carrying members, e.g. rotors of the screw type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
- F03B3/12—Blades; Blade-carrying rotors
- F03B3/128—Mounting, demounting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D3/00—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor
- F03D3/06—Rotors
- F03D3/062—Rotors characterised by their construction elements
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/20—Hydro energy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/74—Wind turbines with rotation axis perpendicular to the wind direction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Abstract
The invention discloses an efficiency-increasing, energy-saving and emission-reducing method for propellers, ruston turbines, fans and turbofans for various uses for the society. The efficiency-increasing, energy-saving and emission-reducing method is innovated on the basis of the prior art, and blades of the propellers, the ruston turbines, the fans and the turbofans which are used are disassembled and reassembled to enable all the blades on each wheel hud to be arranged for a circle in the mode that one blade is a bit lower than the next one and enable all the blades not to be located on one plane but in a spiral shape on the whole. Original design and production lines of manufactures of the propellers, the ruston turbines, the fans and the turbofans are unchanged, and only in a finished product assembling link, the manufacturers conduct installation according to the efficiency-increasing, energy-saving and emission-reducing method. New incorporations manufacture products of the propellers, the ruston turbines, the fans and the turbofans according to the efficiency-increasing, energy-saving and emission-reducing method. The physical law of the energy-saving and emission-reducing method is that efficiency increasing is in direct proportion with the vertical distance between the blades from zero to an optimal vertical distance value, and efficiency increasing is in inverse proportion and is finally ended after the optimal vertical distance value is exceeded.
Description
Technical field：The present invention be with regard to the variously-shaped propeller of every field various uses all size, vane wheel oar,
Fan, turbofan product, innovate again on the basis of existing technology, make these products realize that Synergistic and energy-saving is reduced discharging.
Background technology：The variously-shaped propeller of known every field various uses all size, vane wheel oar, fan,
Turbofan product, their blade equidistantly waits angle of inclination installation in one plane on wheel hub, between blade and blade
On wheel hub without height point, whole blades are all generally flush with up and down, and during work parallel rotating does work.
The content of the invention：The various uses propeller vane wheel oar fan turbofan Synergistic and energy-saving discharge-reducing method of the present invention, is existing
Have innovate again on the basis of technology the product for making prior art change system into Synergistic and energy-saving reduce discharging product.1st, user
The variously-shaped propeller of the every field various uses all size that uses, vane wheel oar, fan, the blade dismounting of turbofan product
Get off, the product for being reassembled into Synergistic and energy-saving reduction of discharging is required according to the technology of the present invention.Specific practice is according to the leaf of original product
Piece quantity is constant, and the pitch between blade and blade is constant, and the angle of inclination of whole blades is constant, only changes whole blades in wheel
The distance up and down of hub, makes each blade low a little arrangement of the ratio 1 of number 1 from top to bottom one week, each blade on wheel hub
It is in one plane not overall in the shape of a spiral, have between the first blade and tail position blade than larger height spacing, during work
Spiral rotating acting produces coiled energy makes product increase work efficiency realize effects of energy saving and emission reduction.2nd, every field various uses
The variously-shaped propeller of all size, vane wheel oar, fan, the manufacturer of turbofan product, according to original design constant original production
Streamline is constant, simply finished product assembling link on just with the present invention Synergistic and energy-saving discharge-reducing method, specific practice be according to
Intrinsic blade quantity is constant, and the pitch between intrinsic blade and blade is constant, intrinsic whole blade pitch angles
Degree is constant, only changes up and down distance of whole blades in wheel hub, and from top to bottom the ratio 1 of number 1 is low on wheel hub to make each blade
Little by little arrangement one week, each blade is not in one plane overall in the shape of a spiral, between the first blade and tail position blade
Have than larger height spacing, spiral rotating acting produces coiled energy during work makes product increase work efficiency realize that energy-conservation subtracts
Row's effect.3rd, company's production propeller, vane wheel oar, fan, the turbofan product of new registration, directly using the Synergistic and energy-saving of the present invention
Discharge-reducing method manufactures and designs propeller, vane wheel oar, fan, turbofan product, and specific practice is to make reference design according to prior art
Product formulates production line manufacture parts, and according to the technology of the present invention various finished products are assembled, and makes the blade of product in wheel hub
On low little by little arrangement one week of the ratio 1 of number 1 from top to bottom, each blade is in one plane overall not in the shape of a spiral, first
Have than larger height spacing between position blade and tail position blade, spiral rotating acting produces coiled energy during work increases product
Plus work efficiency realizes effects of energy saving and emission reduction.
The physics law of various uses propeller vane wheel oar fan turbofan Synergistic and energy-saving discharge-reducing method of the present invention is【Blade
Height spacing between blade is stopped Synergistic and energy-saving reduction of discharging and is directly proportional from zero initial to optimal height distance values, more than optimal height
Low distance values initial Synergistic and energy-saving is reduced discharging and is inversely proportional to disappearance】.Increasing is found respectively in production practices in accordance with this physics law
Optimal height distance values are imitated, and finished product assembling is carried out in strict accordance with this height distance values.Due to propeller vane wheel oar fan
The purposes of turbofan is different, makes the width of their blade quantity different leaves different, causes their optimal height distance values
Difference, makes their Synergistic and energy-saving reduce discharging amplitude different, it is therefore desirable to find out respective optimal height respectively in an assembling process
Low distance values, the Synergistic and energy-saving that could obtain amplitude peak reduces discharging benefit.
Embodiment：The various uses propeller vane wheel oar fan turbofan Synergistic and energy-saving discharge-reducing method of the present invention, is existing
Have on the basis of technology and innovate again, first is applied the spiral shell being currently in use variously-shaped in every field various uses all size
On rotation oar, vane wheel oar, fan, turbofan product, second is applied in the producer for producing propeller, vane wheel oar, fan, turbofan product
On, apply for the 3rd and produced on propeller, vane wheel oar, fan, turbofan product in new registration company.Come as a example by first below
Illustrate specific embodiment：1st, the steam turbine turbine rotor turbofan of thermal power plant, wheel hub and turbofan blade are disassembled according to leaf
Sheet gauge trellis shape is copied into small-sized emulation turbine rotor turbofan, and using this emulation turbine rotor turbofan simulation Synergistic and energy-saving is explored
Optimal height distance values are reduced discharging, according to this optimal height distance values steam turbine turbine rotor turbofan is re-assemblied, made by
Not in one plane, the turbofan blade low little by little arrangement of the ratio 1 of number 1 from front to back a week is whole for the blade of turbine rotor turbofan
In the shape of a spiral, spiral rotating acting during work produces coiled energy to body, and thermal power plant's generating efficiency energy-saving and emission-reduction each hundred are increased on year-on-year basis
/ bis- ten or so.2nd, the steam turbine turbine rotor turbofan of nuclear power station, wheel hub and turbofan blade are disassembled according to blade rule
Trellis shape is copied into small-sized emulation turbine rotor turbofan, explores Synergistic and energy-saving using this emulation turbine rotor turbofan simulation and reduces discharging
Optimal height distance values, according to this optimal height distance values steam turbine turbine rotor turbofan is re-assemblied, made by turbine
Not in one plane, from front to back the low one week entirety of little by little arrangement of the ratio 1 of number 1 is in turbofan blade the blade of rotor turbofan
Helical form, spiral rotating acting during work produces coiled energy, and nuclear power station generating efficiency energy-saving and emission-reduction each percent are increased on year-on-year basis
20 or so.3rd, the big machinery such as naval vessel steam turbine electromotor, gas turbine engine, gas turbine powered generator turbine rotor whirlpool
Fan, their wheel hub is disassembled with turbofan blade, and according to blade specification shape small-sized emulation turbine rotor turbofan is copied into,
Respective Synergistic and energy-saving is explored using this emulation turbine rotor turbofan simulation and reduce discharging optimal height distance values, according to this optimal height
Low distance values re-assembly respective turbine rotor turbofan, made by turbine rotor turbofan blade not in one plane, whirlpool
In the shape of a spiral, spiral rotating acting during work produces spiral shell to the low one week entirety of little by little arrangement of the flat ratio 1 of number 1 from front to back of flabellum
Rotation energy, increases on year-on-year basis respective work efficiency energy-saving and emission-reduction each 20 or so percent.4th, the hydraulic turbine vane wheel oar in power station,
Its wheel hub and blade are disassembled and is copied into small hydraulic turbine vane wheel oar according to blade specification shape, using this emulation turbine
The optimal height distance values of Synergistic and energy-saving are explored in oar simulation, and according to this optimal height distance values hydraulic turbine turbine is re-assemblied
Oar, made by hydraulic turbine vane wheel oar blade not in one plane, from top to bottom the ratio 1 of number 1 is low little by little for turbine impellers
In the shape of a spiral, spiral rotating acting during work produces coiled energy to one week entirety of arrangement, and the generating efficiency in power station is increased on year-on-year basis
Save water resource each more than 20 percent.5th, wind energy turbine set wind wind wheel oar explores the optimal height distance values of potentiation, according to this
Optimal height distance values remake wind wheel propeller hub and assembling blade, made by wind wheel oar blade not in a plane
On, integrally in the shape of a spiral spiral rotating does work during work within one week for the Wind wheel paddle low little by little arrangement of the ratio 1 of number 1 from front to back
Coiled energy is produced, the generating efficiency 20 or so percent of wind-driven generator is increased on year-on-year basis.6th, turbocharger, by the saturating of it
The sub- turbofan blade of flat turn is disassembled, and according to 30 percent digital average of 1 width of blade turbine rotor turbofan is distributed to
Each blade do height distance values, re-assembly turbine rotor turbofan according to this height distance values, made by turbine increase
The blade of depressor turbine rotor turbofan not in one plane, the low little by little arrangement one of the ratio 1 of number 1 from front to back of turbofan blade
In the shape of a spiral, spiral rotating acting during work produces coiled energy to all entirety.The high-pressure fan blade of turbocharger is dismantled
Get off, each blade for distributing to high-pressure fan according to 1 15 digital average of 1 width of blade does height spacing number
Value, re-assembly high pressure turbofan according to this height distance values, made by high pressure turbofan blade not in one plane, turbofan leaf
The piece low little by little arrangement of the ratio 1 of number 1 from front to back one week is overall in the shape of a spiral, spiral rotating acting generation spiral energy during work
Amount, increases on year-on-year basis the work efficiency energy-saving and emission-reduction each 20 or so percent of turbocharger.7th, turbofan air compressor machine is centrifuged, by it
High pressure turbofan blade disassemble, distribute to the every of high pressure turbofan according to 1 15 digital average of 1 width of blade
Individual blade does height distance values, and according to this height distance values high pressure turbofan is re-assemblied, made by high pressure turbofan blade not
In one plane, the turbofan blade low little by little arrangement of the ratio 1 of number 1 from front to back a week integrally in the shape of a spiral, spiral shell during work
Rotation rotation acting produces coiled energy, and the work efficiency energy-saving and emission-reduction each 1 15 or so of centrifugal air compressor are increased on year-on-year basis.
8th, aerator, heat emission fan, air conditioner, range hood, air staticizer, wait fan, and their wind wheel fan leaf is disassembled
Each according to 10 to 15 numerical value of 1 width of blade, each blade for being averagely allocated to respective wind wheel fan does height
Low distance values, according to this height distance values respective wind wheel fan is re-assemblied, made by wind wheel fan leaf it is not flat at one
On face, the wind wheel fan leaf low little by little arrangement of the ratio 1 of number 1 from front to back a week is overall in the shape of a spiral, during each of which work
Spiral rotating acting produces coiled energy, and respective work efficiency energy-saving and emission-reduction each more than 10 are increased on year-on-year basis.9th, water pump
Chemical liquid pump, by their turbine 10 numerical value according to 1 turbine leaf width degree are disassembled, and are averagely allocated to each
Each turbine leaf of turbine does height distance values, and according to this height distance values respective turbine leaf is re-assemblied, made by
Not in one plane, the turbo blade low little by little arrangement of the ratio 1 of number 1 from front to back a week is integrally helically for turbo blade
Shape, spiral rotating acting during work produces coiled energy, and water pump chemical pump work efficiency energy-saving and emission-reduction each percent are increased on year-on-year basis
More than ten.10th, the mechanically-propelled propeller vane wheel oar waterborne such as naval vessel, the blade of their propeller vane wheel oar is disassembled,
The propeller vane wheel oar of 3-4 blade, according to 10 to 15 numerical value of respective 1 width of blade, is averagely allocated to each
Height distance values are done from each blade of propeller vane wheel oar, according to this height distance values respective propeller is re-assemblied
Vane wheel oar, made by propeller turbine paddle blade not in one plane, propeller turbine paddle blade 1 ratio 1 of number from front to back
In the shape of a spiral, spiral rotating acting when propeller vane wheel oar works produces coiled energy to individual low one week entirety of little by little arrangement, together
It is more each by 10 to more than 15 than increasing speed of a ship or plane energy-saving and emission-reduction.The propeller vane wheel oar of 5-6 blade, according to respective 1 leaf
1 15 to 20 numerical value of piece width, each blade for being averagely allocated to respective propeller vane wheel oar does height spacing number
Value, according to this height distance values again each self assembly screw vortex wheel oar, made by propeller vane wheel oar blade not one
In individual plane, the propeller turbine paddle blade low little by little arrangement of the ratio 1 of number 1 from front to back a week integrally in the shape of a spiral, spiral
Spiral rotating acting when oar vane wheel oar works produces coiled energy, and speed of a ship or plane energy-saving and emission-reduction each 1 15 to 20 are increased on year-on-year basis
More than.Propeller vane wheel oar more than 7 blades, according to 25 percent numerical value of respective 1 width of blade, mean allocation
Height distance values are done to each blade of respective propeller vane wheel oar, according to this height distance values again each self assembly spiral
Oar vane wheel oar, made by propeller vane wheel oar blade not in one plane, propeller turbine paddle blade number 1 from front to back
One week overall curl of little by little arrangement lower than 1, spiral rotating acting when propeller vane wheel oar works produces coiled energy,
Increase speed of a ship or plane energy-saving and emission-reduction each 20 to more than 25 percent on year-on-year basis.11st, the low pressure fan of aircraft engine sets according to original
Meter is copied into artificial small low pressure fan, explores Synergistic and energy-saving using this emulation low pressure fan simulation and reduces discharging optimal height spacing
Numerical value, according to this optimal height distance values the low pressure fan of aircraft engine is manufactured, made by aircraft engine low pressure fan
Blade not in one plane, the low pressure fan blade low little by little arrangement of the ratio 1 of number 1 from front to back a week is integrally helically
Shape, spiral rotating acting when low pressure fan works produces coiled energy, and the low pressure fan work effect of aircraft engine is increased on year-on-year basis
Rate more than 10.The high pressure turbofan of aircraft engine is copied into artificial small high pressure turbofan according to original design, imitative using this
True high pressure turbofan simulation explores Synergistic and energy-saving and reduces discharging optimal height distance values, flies according to this optimal height distance values manufacture
The high pressure turbofan of machine electromotor, made by aircraft engine high pressure turbofan blade not in one plane, the leaf of high pressure turbofan
The piece low little by little arrangement of the ratio 1 of number 1 from front to back one week is overall in the shape of a spiral, spiral rotating acting product when high pressure turbofan works
Raw coiled energy, increases on year-on-year basis the work efficiency more than 10 of aircraft engine high pressure turbofan.Aircraft engine high-low pressure
Turbine turbofan, according to original design artificial small high pressure and low pressure turbine turbofan is copied into, using this emulation high pressure and low pressure turbine turbofan simulation
Explore Synergistic and energy-saving and reduce discharging optimal height distance values, according to this optimal height distance values aircraft engine high-low pressure is manufactured
Turbine turbofan, made by aircraft engine high pressure and low pressure turbine turbofan blade not in one plane, high pressure and low pressure turbine turbofan
The blade low little by little arrangement of the ratio 1 of number 1 from front to back one week is overall in the shape of a spiral, and spiral revolves when high pressure and low pressure turbine turbofan works
Turn acting and produce coiled energy, high pressure and low pressure turbine turbofan work efficiency energy-saving and emission-reduction each more than 10 are increased on year-on-year basis.12nd, spiral shell
Propeller more than rotation oar three paddle blades of aircraft, according to original design duplication artificial small propeller, using this emulation propeller
Simulation explores Synergistic and energy-saving and reduces discharging optimal height distance values, and according to this optimal height distance values properller is manufactured,
Made by properller blade not in one plane, the propeller blade low little by little arrangement one of the ratio 1 of number 1 from front to back
In the shape of a spiral, spiral rotating acting during propeller works produces coiled energy to all entirety, and propeller aeroplane speed of a ship or plane section is increased on year-on-year basis
Each more than 10 can be reduced discharging.
Claims (4)
1. every field, various uses, all size, variously-shaped propeller, vane wheel oar, fan, the potentiation of turbofan product
Energy-saving and emission-reduction method, is innovated on the basis of prior art products, propeller that user is currently in use, vane wheel oar,
Fan, the blade of turbofan product are disassembled, and the product reduced discharging with Synergistic and energy-saving are reassembled into according to synergisting method, specifically
Way be according to original product blade quantity is constant, the spacing of blade and blade is constant, blade angle of inclination is constant, only changes leaf
The upper-lower position of piece, makes 1 ratio 1 low a little arrangement one week on wheel hub of each blade, and each blade is not flat at one
On face it is overall in the shape of a spiral.
2. every field, various uses, all size, variously-shaped propeller, vane wheel oar, fan, the production of turbofan product
Producer, it is constant according to original design constant, original production streamline, simply according to Synergistic and energy-saving reduction of discharging side in the link of finished product assembling
Method is installed, and makes 1 ratio 1 low a little arrangement one week on wheel hub of each blade, and each blade is not in a plane
Entirety is gone up in the shape of a spiral.
3. company's production propeller, vane wheel oar, fan, the turbofan product of new registration, directly sets according to Synergistic and energy-saving discharge-reducing method
Meter production parts assembling finished product, made by low little by little arrangement one week of product blade 1 ratio 1 on wheel hub, each
Blade it is in one plane not overall in the shape of a spiral.
4. every field, various uses, all size, variously-shaped propeller, vane wheel oar, fan, turbofan product, potentiation section
The pass technology of building of energy discharge-reducing method is blade 1 ratio 1 low a little arrangement one week on wheel hub, and each blade is not at one
In plane it is overall in the shape of a spiral, Synergistic and energy-saving reduces discharging physics law is【Height spacing between blade and blade is from zero initial
Stop potentiation to optimal height distance values to be directly proportional, be inversely proportional to disappearance more than optimal height distance values initial potentiation】, in accordance with
This physics law finds respectively the optimal height distance values of potentiation in production practices, and enters in strict accordance with this height distance values
Row finished product is assembled.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710062545.9A CN106593959A (en) | 2017-02-03 | 2017-02-03 | Efficiency-increasing, energy-saving and emission-reducing method for propellers, ruston turbines, fans and turbofans for various uses |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710062545.9A CN106593959A (en) | 2017-02-03 | 2017-02-03 | Efficiency-increasing, energy-saving and emission-reducing method for propellers, ruston turbines, fans and turbofans for various uses |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106593959A true CN106593959A (en) | 2017-04-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710062545.9A Pending CN106593959A (en) | 2017-02-03 | 2017-02-03 | Efficiency-increasing, energy-saving and emission-reducing method for propellers, ruston turbines, fans and turbofans for various uses |
Country Status (1)
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| CN (1) | CN106593959A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2772959Y (en) * | 2005-01-14 | 2006-04-19 | 吴迪 | Screw propeller for propulser or oxygen supplier of ship |
| WO2006059094A1 (en) * | 2004-11-30 | 2006-06-08 | Malcolm Maclean Bowie | Apparatus for the generation of power from a flowing fluid |
| CN101918701A (en) * | 2007-11-16 | 2010-12-15 | 自然能技术有限公司 | A power generator |
| CN102787959A (en) * | 2012-08-28 | 2012-11-21 | 罗士武 | Turbine made of paddles arranged in spirally forward mode of water turbine |
-
2017
- 2017-02-03 CN CN201710062545.9A patent/CN106593959A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006059094A1 (en) * | 2004-11-30 | 2006-06-08 | Malcolm Maclean Bowie | Apparatus for the generation of power from a flowing fluid |
| CN2772959Y (en) * | 2005-01-14 | 2006-04-19 | 吴迪 | Screw propeller for propulser or oxygen supplier of ship |
| CN101918701A (en) * | 2007-11-16 | 2010-12-15 | 自然能技术有限公司 | A power generator |
| CN102787959A (en) * | 2012-08-28 | 2012-11-21 | 罗士武 | Turbine made of paddles arranged in spirally forward mode of water turbine |
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Application publication date: 20170426 |