CN109083814B - Noise suppression method for downwind wind turbine based on slotting with variable helix angle - Google Patents
Noise suppression method for downwind wind turbine based on slotting with variable helix angle Download PDFInfo
- Publication number
- CN109083814B CN109083814B CN201810991612.XA CN201810991612A CN109083814B CN 109083814 B CN109083814 B CN 109083814B CN 201810991612 A CN201810991612 A CN 201810991612A CN 109083814 B CN109083814 B CN 109083814B
- Authority
- CN
- China
- Prior art keywords
- slotting
- noise
- fluting
- helix angle
- pylon
- 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.)
- Active
Links
- 238000000034 method Methods 0.000 title claims abstract description 27
- 230000001629 suppression Effects 0.000 title claims abstract description 8
- 238000006243 chemical reaction Methods 0.000 abstract description 31
- 230000000694 effects Effects 0.000 abstract description 23
- 230000009467 reduction Effects 0.000 abstract description 6
- 230000002401 inhibitory effect Effects 0.000 abstract description 5
- 230000036961 partial effect Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 8
- 230000008859 change Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 230000003993 interaction Effects 0.000 description 3
- 230000002829 reductive effect Effects 0.000 description 3
- 230000003044 adaptive effect Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000004907 flux Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 230000003313 weakening effect Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 244000145845 chattering Species 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000011089 mechanical engineering Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
- F03D13/00—Assembly, mounting or commissioning of wind motors; Arrangements specially adapted for transporting wind motor components
- F03D13/20—Arrangements for mounting or supporting wind motors; Masts or towers for wind motors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/96—Preventing, counteracting or reducing vibration or noise
-
- 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
- Y02E10/728—Onshore wind turbines
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
Abstract
Based on the down-wind type of WECS noise suppressing method for becoming helical angle fluting, it is related to cylinder pylon wind energy conversion system.Slotting position and slotting length are determined on cylinder pylon；On cylinder pylon, fluting helical angle size is determined；Design the depth and width of fluting and the geometry of fluting.It can not only inhibit the development of cylindrical wake Karman vortex street, moreover it is possible to play the role of drag reduction.Become the helical angle groove feature larger for blade tip partial noise, the more preferable low-frequency noise for inhibiting blade tip part.Described simple based on the wind energy conversion system low frequency aerodynamic noise suppressing method structure for becoming helical angle fluting, it is convenient to realize, does not need the control system of additional complexity, noise reduction effect is significant, is a kind of potential down-wind type of WECS noise suppression proposal.
Description
Technical field
The present invention relates to cylinder pylon wind energy conversion systems, more particularly to based on the down-wind type of WECS noise suppression for becoming helical angle fluting
Method processed.
Background technique
Wind energy is increasingly taken seriously as a kind of clean renewable energy, and each state is all greatly developing wind in the world
Electric cause.With the continuous expansion of installed capacity of wind-driven power, the noise problem of wind energy conversion system becomes increasingly conspicuous.If half-hearted research solution
Certainly, a major obstacle for restricting wind-power electricity generation development will be become.Wind energy conversion system noise according to source can be divided into mechanical noise and
Aerodynamic noise.As wind energy conversion system designs and manufactures horizontal raising, the mechanical noise of wind energy conversion system has been substantially reduced, and pneumatically makes an uproar
Sound is still an insoluble problem.Wind energy conversion system aerodynamic noise can be divided into according to production principle: low frequency aerodynamic noise, incoming flow
Turbulent flow interference noise and blade self noise [1].It is more to the research of blade self noise, incoming flow turbulent flow interference noise at present, to wind
The research of power machine low frequency aerodynamic noise is less.With the continuous increase of wind energy conversion system size, wind energy conversion system low frequency aerodynamic noise problem will
[2] more and more prominent will become the major obstacle for restricting wind-powered electricity generation career development if do not solved, therefore it is low to need development wind energy conversion system
Frequency aerodynamic noise inhibits research.
Wind energy conversion system can be divided into windward formula wind energy conversion system according to the relative position of wind wheel and pylon (wind wheel is in the upstream of pylon)
With down-wind type of WECS (wind wheel is in the downstream of pylon).Wind energy conversion system in power generation process, wind by pylon due to pylon obstruction,
It will affect the size and Orientation of wind, while will cause the load fluctuation on pneumatic equipment bladess surface, here it is the tower shadow of wind energy conversion system effects
Answer [3].The low frequency aerodynamic noise of wind energy conversion system refer to due to pneumatic equipment bladess by the speed of pylon lose region or wake zone with
The unsteady load noise that the Shedding Vortex interaction of pylon generates, the non-stationarity of tower wake is wind energy conversion system in tower shadow effect
The main reason for generating low-frequency noise.For down-wind type of WECS since air-flow will first flow through the leaf that pylon then flows into wind energy conversion system
Piece, therefore the tower shadow effect of down-wind type of WECS is seriously much than windward formula wind energy conversion system.For windward formula wind energy conversion system, tower shadow effect
The low frequency aerodynamic noise that should be generated is smaller, and for down-wind type of WECS, the low frequency aerodynamic noise that tower shadow effect generates is very big, is
Need key problems-solving.
The means for weakening wind energy conversion system tower shadow effect at present mainly have stator flux oriented vector control [4], adaptive
Trailing edge technology [5] etc..Wherein stator flux oriented vector control is to be avoided using complicated control system due to tower shadow
Effect leads to generated output chattering；It using adaptive trailing edge technology, is dropped using the aeroeleastic deformation of aerofoil profile trailing edge
Load fluctuation of the low wind energy conversion system under tower shadow effect effect.However these methods be all using active control technology, and not
The influence of tower shadow effect is reduced from source.Since most pylon is using cylinder pylon, at present both at home and abroad for cylinder
Wake control has carried out a large amount of research work, achieves a series of achievements.The present invention uses cylindrical wake control means
The low frequency levels of aerodynamic noise of wind energy conversion system is reduced by weakening the non-stationarity of windmill tower frame wake flow.
For down-wind type of WECS, wind energy conversion system tower shadow effect is that the wake flow of cylinder pylon acts on wind machine oar leaf generation,
Therefore the low frequency aerodynamic noise that reduce wind energy conversion system substantially seeks to control the wake flow of cylinder pylon.Existing research refers to
Flow control method can be used by inhibiting cylinder tower wake card in down-wind type of WECS biggish for low frequency aerodynamic noise out
The development of door vortex street weakens surface load fluctuation when blade passes through tower wake, so that the low frequency for reducing wind energy conversion system is pneumatically made an uproar
Sound.The development for inhibiting cylinder tower wake Karman vortex street, reduces the low frequency aerodynamic noise of down-wind type of WECS, there is active control side
Method and passive control methods.Active Control Method: it using/air-breathing scheme is blown such as on windmill tower frame, then needs in pylon
Surrounding arrangement blows/getter device, while installing complicated control system, and this adds increased the costs of equipment and equipment to be out of order
Probability, and need biggish energy input.According to passive control methods, then the control method must be considered to wind first
Wheel is all effective in each orientation of pylon, and the methods of installation diaphragm plate, installation radome fairing are all just for one direction of cylinder pylon
Wake flow have control effect, therefore be also not suitable for using.Spiral grooves are the novel cylindrical wake controls of one kind proposed in recent years
Method [6,7] processed, has control effect to the incoming flow of all directions, also can effectively inhibit cylindrical wake under high reynolds number
Karman vortex street structure, has good drag-reduction effect, these features reduce wind energy conversion system for the tower shadow effect of decrease wind energy conversion system
Low frequency levels of aerodynamic noise is all very favorable.
Bibliography:
1.WagnerS,BareibR,GuidatiG.Wind turbine noise[M].Berlin:Springer,
1996:200-210。
2. Li Xiaodong, Xu Yingbo, river Min wind energy conversion system Study of Aerodynamic present condition and developing tendency [J] applied mathematics and power
It learns, 2013,34 (10): 1083-1090.
3.Jung S S,Cheung W S,Cheong C L,et al.Experimental identification of
acoustic emission characteristics of large wind turbines with emphasis on
infrasound and low-frequency noise[J].Journal of the Korean physical society,
2008,53(4):1897-1905。
4.Miyakawa T,Shinohara K,Yamamoto K,et al.A suppression method of
tower shadow effect in wind power system using a wound rotor induction
generator[A].Electric machines and drives conference[C].Miami,Florida,2009。
5.Buhl T,Gaunaa M,Bak C.Potential load reduction using airfoils with
variable trailing edge geomery[J].Journal of solar energy engineering,2005,
127(4):503-516。
6.Huang S.VIV suppression of a two-degree-of-freedom circular
cylinder and drag reduction of a fixed circular cylinder by the use of
helical grooves[J].Journal of fluids and structures,2011,27:1124-1133。
7.Alonzo Garcia A,C del Gutierrez,Jimenez Bernal J A.large eddy
simulation of the subcritical flow over a U-grooved circular cylinder[J]
.Advances in mechanical engineering,2014,ID 418398。
Summary of the invention
The present invention is intended to provide based on the down-wind type of WECS noise suppressing method for becoming helical angle fluting.
The present invention the following steps are included:
1) slotting position and slotting length are determined on cylinder pylon；
It is described to determine that the specific method of slotting position and slotting length on cylinder pylon in step 1) are as follows: according to
Pylon and pneumatic equipment bladess positional relationship are that starting is slotted with cylinder pylon top end；According to wind wheel blade diameter
Determine slotting length.
2) on cylinder pylon, fluting helical angle size is determined；
In step 2), the determining fluting helical angle size specific method can are as follows: since wind machine oar leaf is close to blade tip
Partial linear velocity is big, and the noise of generation is big, therefore reduces helical angle size in helicla flute of the cylinder pylon close to blade tip part, adds
The circle number of close fluting, the more preferable Karman vortex street structure for inhibiting the cylindrical wake near blade tip are opposite using far from blade tip part
Compared with the groove of large helix angle.
3) depth and width of design fluting and the geometry of fluting.
In step 3), the specific method of the geometry of the depth and width and fluting of the design fluting can are as follows: root
According to cylinder tower diameter size and wind machine oar leaf diameter, and guarantee geometry intensity, rigidity and the stabilization of cylinder pylon
Property require, determine groove depth, width, need to reduce friction loss according to groove, avoid stress concentrate requirement determine fluting
Shape.
It is more preferable to the effect for the main region noise reduction for generating noise that the present invention becomes helical angle fluting.First on cylinder pylon
Spiral mode of grooving is selected, the Karman vortex street intensity of cylinder tower wake is inhibited.Then change the helical angle of different location,
It encrypts to close to blade tip part, to preferably weaken noise caused by blade and Karman vortex street interaction, realizes
Reduce the purpose of noise.
Advantages of the present invention is as follows:
Spiral grooves of the invention can not only inhibit the development of cylindrical wake Karman vortex street, moreover it is possible to play the role of drag reduction.
Become the helical angle groove feature larger for blade tip partial noise, the more preferable low-frequency noise for inhibiting blade tip part.It is of the present invention
Simple based on the wind energy conversion system low frequency aerodynamic noise suppressing method structure for becoming helical angle fluting, it is convenient to realize, does not need additional complexity
Control system, noise reduction effect is significant, is a kind of potential down-wind type of WECS noise suppression proposal.
Detailed description of the invention
Fig. 1 is down-wind type of WECS typical case flowing and the tower shadow effect schematic diagram of the embodiment of the present invention.
Fig. 2 is that the down-wind type of WECS typical case flowing that the change helical angle of the embodiment of the present invention is slotted is illustrated with tower shadow effect
Figure.
Fig. 3 is the change helical angle fluting wind energy conversion system schematic diagram of the embodiment of the present invention.
Fig. 4 is the position of the fluting of the embodiment of the present invention, length schematic diagram.
Fig. 5 is the big logotype of helical angle of the embodiment of the present invention.
Fig. 6 is the cylinder pylon trench profile position view of the embodiment of the present invention.
Fig. 7 is the cylinder pylon trench profile scale diagrams of the embodiment of the present invention.
Fig. 8 is the groove dimensions information schematic diagram of the embodiment of the present invention.
Fig. 9 is the half slot schematic diagram of the embodiment of the present invention.
Figure 10 is the oval groove schematic diagram of the embodiment of the present invention.
Specific embodiment
Fig. 1 shows the principles of the tower shadow effect of down-wind type of WECS: the horizontal incoming flow 1 in infinity flows through down-wind type of WECS
When, the obstruction due to the air-flow near cylinder pylon by down-wind type of WECS cylinder pylon 3 forms Tathagata stream by circle
Speed loss 2 after column pylon.Changes will occur for the air-flow size and direction vector blocked by pylon, cylinder pylon two sides
It forms incoming flow and flows through the whirlpool 4 that pylon falls off.Tower wake area can generate unsteady Karman vortex street, after formation incoming flow flows through pylon
Speed lose region 6.The unsteady wake flow area of pylon flows through pneumatic equipment bladess 5, and incoming flow flows through the whirlpool 4 and blade that pylon falls off
Interaction is so that blade surface can generate load fluctuation, generation low-frequency noise.Fig. 2 and Fig. 3 is the leeward for becoming helical angle fluting
Formula wind energy conversion system tower shadow effect inhibits principle and schematic diagram, and (in Fig. 2, label 7 is speed of the incoming flow after cylinder pylon of slotting
Loss, 10 be the whirlpool that incoming flow flows through that change helical angle fluting pylon falls off, and 11 flow through the speed after becoming helical angle fluting pylon for incoming flow
Degree loss region): horizontal 1 a part of incoming flow in infinity blows to pneumatic equipment bladess 5 by radome fairing 12 and motor 13.Another portion
The down-wind type of WECS cylinder pylon 8 for dividing air-flow to slot by becoming helical angle, due to having spiral grooves 9 on pylon, effectively
The development of cylindrical wake Karman vortex street is inhibited, weakens surface load fluctuation when blade passes through tower wake, to reduce wind
The low frequency aerodynamic noise of power machine.Due to V=Ω R (V is linear velocity, and Ω is revolving speed, and R is radius), tip segment linear velocity is larger,
Noise is also larger, reduces helical angle in the spiral grooves encrypted area 14 apart from tip segment, increases fluting circle number, more preferably to inhibit
Noise at blade tip.Biggish helical angle is used far from tip segment.It is smoothly transitted becoming helical angle place using secondary.
Specific implementation step is as follows:
Step 1: on cylinder pylon, slotting position, slotting length are determined.Such as Fig. 4, started setting up from tower top
Section fluting, fluting total length L are (0.5~1.5) R.The length H of spiral grooves encrypted area 14 is (0.1~0.2) near blade tip
R.14 position of spiral grooves encrypted area are as follows: encryption fluting zone centerline 15 and 16 minimum point S of blade tip trajectory line are in same level
On face.Wherein R is pneumatic equipment bladess span diameter.
Step 2: on cylinder pylon, fluting helical angle size is determined.
With reference to Fig. 5, takes α and β to be all greater than 0, be at this time left hand helix slot.Helixangleβ at spiral grooves encrypted area 14 is
(10 °~30 °), non-encrypted area angle α are (30 °~60 °).It is at this time right hand helix slot when taking α and β to be smaller than 0, encrypted area angle beta
For (- 10 °~-30 °), non-encrypted area angle α is (- 30 °~-60 °).
Step 3: the depth and width of fluting and the geometry of slot are designed.Slot is cross-section slot.Slot should come with level
It is maximum to flow contact area, preferably to inhibit the effect of Karman vortex street.It is equipped with chamfering in slot bottom, chamfering and pylon need smooth mistake
It crosses.With reference to Fig. 6, groove is introduced by taking the section CGID on cylinder pylon as an example, the side CG of the section is overlapped with body diameter, side CD
It is overlapped with cylinder pylon bus 20, with grooves in O, F two o'clock.
The groove of chamfering is equipped with using bottom, with reference to Fig. 7 and Fig. 8., the depth N (0.01D~0.15D) of slot, the width of slot
M (0.001R~0.07R).It is equipped with chamfering in slot bottom, the wall surface 17,18 of slot should be tangent with chamfering, smoothly transits, and reduces friction.
Chamfer shape is designed using elliptic curve, by control parameter come the shape of control flume.The wall surface 18 (rectilinear form) of slot
Depth is n, and depth of chamfering a (0~N), (rectilinear form) width of wall surface 17 of slot is m, chamfering width b (0~0.5M).It is oval bent
Line meets elliptical equation (1).The 17 width m of wall surface of slot meets relational expression (2)；The 18 depth n of wall surface of slot meets relational expression
(3).In order to enable the horizontal incoming flow 1 in infinity flows into groove as far as possible, slot must be with infinite far water in the direction of exit tangent line 19
Flat 1 direction of incoming flow is consistent, i.e., vertical with cylinder pylon bus 20.In fig. 8, AB two o'clock respectively correspond elliptical long/short axis (or
Short/long axis) vertex, the elliptical a quarter camber line of constituted curve expression.R is pneumatic equipment bladess diameter, and D is that cylinder pylon is straight
Diameter.
M=m+2b (2)
N=n+a (3)
Referring to Fig. 8, by taking slot OF as an example, it is known that the coordinate of A point is (XA, YA), according to above-mentioned geometrical relationship: the coordinate of A
For (n, 0), the coordinate of B is (a+n, b).Therefore, the length that need to only give a, b, n, m, that is, may know that the coordinate of A, B two o'clock, i.e.,
Required groove size and shape can be obtained.
Work as n=m=0, when a=b=N=M/2, the coordinate (O, 0) of A, the coordinate (a, b) of B.A point and origin O weight at this time
It closes, slot is half slot, the radius r=N of slot, α=90 °, and semicircle groove shape meets equation (4).Shape and size such as Fig. 9 of slot.
This diameter of a circle is overlapped with cylinder pylon bus 20.Slot exit tangent line 19 and the horizontal incoming flow 1 in infinity are tangent, and channel bottom is equal
Even transition.The curve constituted is half circular arc.
x2+(y-b)2=a2 (4)
Work as n=m=0, when a ≠ b, the coordinate (O, 0) of A, the coordinate (a, b) of B.A point is overlapped with origin O at this time, and slot is half
Oval groove meets equation (5), shape and size such as Figure 10 of slot.Slot of the oval groove at exit point O is in exit tangent line
19 is consistent with horizontal direction of flow, i.e., vertical with cylinder pylon bus 20.Channel bottom even transition, the curve constituted indicate
Elliptical half camber line.
Claims (3)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810991612.XA CN109083814B (en) | 2018-08-29 | 2018-08-29 | Noise suppression method for downwind wind turbine based on slotting with variable helix angle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810991612.XA CN109083814B (en) | 2018-08-29 | 2018-08-29 | Noise suppression method for downwind wind turbine based on slotting with variable helix angle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109083814A CN109083814A (en) | 2018-12-25 |
| CN109083814B true CN109083814B (en) | 2019-06-21 |
Family
ID=64795097
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810991612.XA Active CN109083814B (en) | 2018-08-29 | 2018-08-29 | Noise suppression method for downwind wind turbine based on slotting with variable helix angle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109083814B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113987713B (en) * | 2021-11-04 | 2022-05-20 | 华北电力大学 | Wind turbine generator gearbox helical angle optimization method and system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202483805U (en) * | 2011-12-30 | 2012-10-10 | 江苏道达海洋装备技术有限公司 | Marine wind generation wind vibration preventing device |
| CN106321366A (en) * | 2016-10-09 | 2017-01-11 | 上海理工大学 | Vertical axis wind machine tower of fractal structure |
| CN107461304A (en) * | 2017-09-11 | 2017-12-12 | 北京金风科创风电设备有限公司 | Surrounding body and equipment for inhibiting vibration of enclosure structure and method for hoisting tower drum |
| CN107956650A (en) * | 2017-11-21 | 2018-04-24 | 北京金风科创风电设备有限公司 | Building enclosure with vibration inhibiting function and method for inhibiting vibration of building enclosure |
| WO2018083054A1 (en) * | 2016-11-07 | 2018-05-11 | Siemens Aktiengesellschaft | Vortex-shedding-arrangement |
-
2018
- 2018-08-29 CN CN201810991612.XA patent/CN109083814B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202483805U (en) * | 2011-12-30 | 2012-10-10 | 江苏道达海洋装备技术有限公司 | Marine wind generation wind vibration preventing device |
| CN106321366A (en) * | 2016-10-09 | 2017-01-11 | 上海理工大学 | Vertical axis wind machine tower of fractal structure |
| WO2018083054A1 (en) * | 2016-11-07 | 2018-05-11 | Siemens Aktiengesellschaft | Vortex-shedding-arrangement |
| CN107461304A (en) * | 2017-09-11 | 2017-12-12 | 北京金风科创风电设备有限公司 | Surrounding body and equipment for inhibiting vibration of enclosure structure and method for hoisting tower drum |
| CN107956650A (en) * | 2017-11-21 | 2018-04-24 | 北京金风科创风电设备有限公司 | Building enclosure with vibration inhibiting function and method for inhibiting vibration of building enclosure |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109083814A (en) | 2018-12-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Liu et al. | Enhancing wind energy harvesting performance of vertical axis wind turbines with a new hybrid design: A fluid-structure interaction study | |
| JP4736003B2 (en) | Fluid machine, windmill, and internal flow speed increasing method of fluid machine using unsteady flow | |
| CN105020106A (en) | Wind turbine low frequency aerodynamic noise suppression device based on rotatable fairing | |
| US20140271216A1 (en) | Horizontal axis wind or water turbine with forked or multi-blade upper segments | |
| Guang et al. | Hydrodynamic performance of a vertical-axis tidal-current turbine with different preset angles of attack | |
| JP2016525186A (en) | Wind power generation tower with gyromill type wind turbine | |
| Kumar et al. | Investigation on performance of improved savonius rotor: An overview | |
| CN205578183U (en) | Self -adaptation becomes vertical axis wind -force drive arrangement and aerogenerator of oar | |
| Yoon et al. | Study of several design parameters on multi-blade vertical axis wind turbine | |
| CN109083814B (en) | Noise suppression method for downwind wind turbine based on slotting with variable helix angle | |
| CN204900165U (en) | Wind energy conversion system low frequency aerodynamic noise suppression device based on rotatable radome fairing | |
| CN101509464B (en) | Passive jet method and device for enhancing vertical shaft wind mill performance | |
| Velázquez et al. | Design and experimentation of a 1 MW horizontal axis wind turbine | |
| JP6407996B2 (en) | Wind power tower | |
| CN205445888U (en) | Wind collecting type wind driven generator | |
| KR101236888B1 (en) | Vertical axis turbine for wind power generation having double blade of wing type | |
| Mohamed et al. | CFD investigation of the multiple rotors Darrieus type turbine performance | |
| CN205297825U (en) | Wind -tunnel formula double round vertical axis aerogenerator | |
| CN208686526U (en) | A variable helix angle slotting device for suppressing downwind wind turbine noise | |
| JP2017166324A (en) | T-type leading end blade for turbine | |
| CN112424469A (en) | Rotor blade for a wind turbine and wind turbine | |
| CN103299069B (en) | Awe and be provided with the wind power generation plant of this awe and the method for designing of awe | |
| CN105508130B (en) | Wind collection type wind driven generator | |
| CN103573530B (en) | A kind of energy by ocean current generating has the turbine impeller of air guide sleeve | |
| KR101291663B1 (en) | Turbine blade and wind turbine equipped whit the same |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |