CN109446683A - A kind of wind turbine cabin cover strength calculation method - Google Patents

A kind of wind turbine cabin cover strength calculation method Download PDF

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Publication number
CN109446683A
CN109446683A CN201811311285.5A CN201811311285A CN109446683A CN 109446683 A CN109446683 A CN 109446683A CN 201811311285 A CN201811311285 A CN 201811311285A CN 109446683 A CN109446683 A CN 109446683A
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cover
wind turbine
turbine cabin
cabin cover
finite element
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王杰
孟庆鑫
李壮
睢广坤
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Nanjing Zhongren Energy Technology Co Ltd
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Nanjing Zhongren Energy Technology Co Ltd
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    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • G06F30/23Design optimisation, verification or simulation using finite element methods [FEM] or finite difference methods [FDM]
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/17Mechanical parametric or variational design
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02BCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B10/00Integration of renewable energy sources in buildings
    • Y02B10/30Wind power

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  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
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  • General Physics & Mathematics (AREA)
  • Evolutionary Computation (AREA)
  • General Engineering & Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • Computational Mathematics (AREA)
  • Mathematical Analysis (AREA)
  • Mathematical Optimization (AREA)
  • Pure & Applied Mathematics (AREA)
  • Wind Motors (AREA)

Abstract

The present invention provides a kind of wind turbine cabin cover strength calculation method, comprising: establishes the geometrical model of wind turbine cabin cover;Geometrical model is imported into finite element analysis software, using the pretreatment function of finite element emulation software, laying modeling is carried out to cover shell;The material properties and section attribute for defining each component of engine room cover, establish the finite element model of wind turbine cabin cover, wherein when definition material attribute, need to define the Young's modulus and Poisson's ratio of glass layer different directions respectively;Boundary condition and load are applied to the finite element model of wind turbine cabin cover;Calculate the single layer ess-strain of wind-force wind turbine cabin cover glass steel part;Its intensity is assessed using composite material strength failure criteria.The present invention models composite plys, and the orthotropy definition material attribute based on material is determined that engine room cover force simulation is truer, and calculated result is more acurrate using maximum tension and compression strain criterion and Tsai-Wu.

Description

A kind of wind turbine cabin cover strength calculation method
Technical field
The invention belongs to wind power generating set strength of parts analysis technical fields, and in particular to a kind of wind turbine cabin cover Strength calculation method.
Background technique
With the continuous development of modern society, demand of the people to the energy also rapid growth.The tradition of non-renewable energy resources The energy is because environment and stockage are constantly restricted, and actively simultaneously renewable energy is cleaned in development for country and government, to replace Traditional non-renewable energy resources.
Wind energy is a kind of important clean energy resource, is of great significance for solving global environment and energy crisis.In recent years Come, domestic wind power generating set is quickly grown, therefore the safety problem of Wind turbine is also most important, can in order to guarantee equipment By property, it is necessary to which structure and fatigue to Wind turbine all parts carry out calculating analysis.
Shell of the engine room cover as wind power generating set exempts from sunlight, rain for protecting in cabin mechanically and electrically component Water and ice and snow etc. influence, while safeguarding that below deck equipment provides security protection and working space for staff.Engine room cover safely may be used Important prerequisite by being Wind turbines normal operation, the Strength co-mputation of composite material engine room cover are the key that measure part reliability Factor.
Application No. is the application for a patent for invention of CN201710666311.5, " a kind of engine room cover of wind turbine intensity is determining Method " a kind of engine room cover strength calculation method based on finite element modeling is disclosed, but simplify cover material when model modeling For orthogonal isotropic material, and the modeling of material laying is not carried out according to practical when finite element modeling, not with practical situations It is consistent.Further, since composite properties, which does not extract the single layer stress of material and tension and compression are strained according to failure standard The intensity of engine room cover is then measured, therefore, which does not consider composite properties, and excessive simplification is carried out to model, is led Calculated result is caused relatively large deviation occur.
Summary of the invention
The object of the present invention is to provide a kind of wind turbine cabin cover strength calculation methods, and the present invention is based on composite materials to have First emulation technology is limited, leads to engine room cover Strength co-mputation inaccuracy to the unreasonable simplification of material for solving current calculation method Problem.
The present invention provides the following technical solutions:
A kind of wind turbine cabin cover strength calculation method, comprising the following steps:
(1) geometrical model for establishing wind turbine cabin cover, cover shell, cover shell including glass fiber reinforced plastics composite material The guardrail and anemoclinograph of interior steel construction and cover cover top portion;
(2) geometrical model of wind turbine cabin cover is imported into finite element analysis software, using finite element emulation software Pretreatment function carries out laying modeling to cover shell;
(3) material properties and section attribute for defining each component of engine room cover, establish the finite element mould of wind turbine cabin cover Type;Wherein need the Young's modulus and Poisson's ratio that define glass layer different directions respectively;
(4) boundary condition is applied to the finite element model of wind turbine cabin cover;
(5) load is applied to the finite element model of wind turbine cabin cover;
(6) equivalent stress of the steelwork component of wind-force wind turbine cabin cover and the single layer strain of glass steel part are calculated Stress;
(7) the glass reinforced plastic strength of parts of engine room cover is assessed using composite material strength failure criteria.
Preferably, when carrying out laying modeling to cover shell, gel coating resin, glass layer and foam enhancing are defined respectively Layer;Definition steel construction is structure steel layer.
Preferably, in the finite element model of wind turbine cabin cover, glass layer is simulated using shell unit, structure steel layer It is simulated using shell unit, foam enhancement layer is simulated using shell unit, and gel coating resin is simulated using shell unit.
Preferably, in the finite element model of wind turbine cabin cover, definition anemoclinograph is quality point, quality point and peace Constraint equation is established in dress face.
Preferably, it is mutually bonded between cover shell and steel construction, is defined in the finite element model of wind turbine cabin cover Contact surface multi-point constraint;Wind turbine cabin cover is integrally attached on pedestal, in the finite element model of wind turbine cabin cover Define fixed constraint.
Preferably, the load finite element model of wind turbine cabin cover applied include wind load, gravitational load or Changing load;Apply concentrated force in the loser and guardrail of wind turbine cabin cover, the direction of concentrated force is that each possibility is fallen Direction.
To the wind load of the finite element model of wind turbine cabin cover are as follows: distinguish each wind-engaging end face of cabin cover outer surface Apply limited airflow pressure load.
The changing load that the finite element model of wind turbine cabin cover is applied are as follows: to engine room cover travel region, standing area Apply well-distributed pressure with horizontal protective region.
Preferably, described to the equivalent stress of engine room cover of wind turbine steelwork component and the single layer of glass steel part The operating condition that strain stress is calculated includes: that gravitational load is superimposed with changing load;Gravitational load is superimposed with wind load, to consider most Rough sledding calculates the ultimate strength of engine room cover.
Preferably, the monolayer strengths of glass-reinforced plastic material are sentenced using maximum tension and compression strain criterion and Tsai-Wu criterion It is fixed;According to structural steel yield strength criterion, the steel construction intensity inside engine room cover is assessed.
The beneficial effects of the present invention are: being orthotropic composite material the present invention is based on the cover shell of engine room cover Material properties and actual production technique, carry out composite plys in finite element modeling, define orthotropic material Different directions material property parameter keeps the engine room cover Strength co-mputation deviation of this finite element model small, is more in line with reality;Finite element Model load and boundary condition are in strict accordance with the standard of calculating, and engine room cover stress condition is truer, and calculated result is more accurate;It adopts Calculated result is assessed with composite material strength failure criteria, determination method is more reasonable.
Detailed description of the invention
Attached drawing is used to provide further understanding of the present invention, and constitutes part of specification, with reality of the invention It applies example to be used to explain the present invention together, not be construed as limiting the invention.In the accompanying drawings:
Fig. 1 is wind turbine cabin cover geometrical model schematic diagram of the invention;
Fig. 2 is the steel construction schematic diagram inside wind turbine cabin cover of the invention;
Fig. 3 is material profile structural schematic diagram when carrying out laying modeling to cover shell.
Specific embodiment
A kind of wind turbine cabin cover strength calculation method, comprising the following steps:
(1) geometrical model of wind turbine cabin cover is established, as depicted in figs. 1 and 2, the cover including glass fiber reinforced plastics composite material Steel construction 4 in body case 1, cover shell and the guardrail 2 and anemoclinograph 3 for being fixed on cover cover top portion, wherein wind-powered electricity generation Set engine room cover is integrally attached on pedestal, is mutually bonded between cover shell 1 and steel construction 4.
(2) wind turbine cabin cover geometrical model suitably simplify, delete tiny threaded hole and chamfering;By wind-powered electricity generation The 3-D geometric model of set engine room cover imports finite element analysis software ANSYS Workbench.Since composite material is orthogonal Anisotropic material, application software pretreatment function, to engine room cover carry out laying modeling, as shown in figure 3, establish gel coating resin 11, Glass layer 12, foam enhancement layer 13;Definition steel construction 4 is structure steel layer.
(3) before finite element analysis software in processing, the material properties and section attribute of each component of engine room cover are defined, are established The finite element model of wind turbine cabin cover.
In definition material attribute, since glass fibre is orthotropic material, along machine direction and vertical fibre The material properties for tieing up direction is entirely different, needs to define the Young's modulus and Poisson's ratio of glass layer different directions respectively: all Such as be defined as follows material parameter: the Young's modulus of X-direction is 23850MPa, and the Young's modulus of Y-direction is 23850MPa, Z-direction Young's modulus be 839MPa, the Poisson's ratio in three directions is 0.3.The tensile strength for defining glass layer is 380MPa, compression Intensity is 150MPa, in-plane shear strength 48MPa.
When defining section attribute, glass layer is simulated using shell unit, and glass layer is by several layers of to ten several layers of Glass fibre composition, the differences such as thickness, ply stacking angle of each layer glass fibre need to define respectively;Structure steel layer is rectangle steel Pipe, is simulated using shell unit, and foam enhancement layer is simulated using shell unit, and gel coating resin is simulated using shell unit.
(4) boundary condition is applied to the finite element model of wind turbine cabin cover.Definition anemoclinograph is quality point, matter Amount point establishes constraint equation with mounting surface;It is mutually bonded between cover shell and steel construction, in the finite element of wind turbine cabin cover Contact surface multi-point constraint is defined in model;Wind turbine cabin cover is integrally attached on pedestal, in having for wind turbine cabin cover Fixed constraint is defined in limit meta-model.
(5) load, including wind load, gravitational load and changing load are applied to the finite element model of wind turbine cabin cover.
Wind load is to apply limited airflow pressure load respectively to each wind-engaging end face of cabin cover outer surface.Consider 3 kinds of operating conditions:
DLC6.1:50 mono- meets fitful wind, and airflow direction is in the Sector Range of front ± 15 °, load safety coefficient γF= 1.35;
DLC6.2:50 mono- meets fitful wind, and airflow direction is in all directions, load safety coefficient γF=1.1, electric network fault And yaw driving noenergy buffering;
DLC7.1:1 mono- meets fitful wind, and airflow direction is in all directions, load safety coefficient γF=1.1, electric network fault and Yaw driving has energy snubber.
According to aerodynamic principle, when some direction of engine room cover windward when, the direction is by positive wine pressure, cover remaining five Direction is by negative wind pressure.When engine room cover is by limit wind load, wind-engaging front end face and rear end face limit wind load usage factor CwRespectively 0.8 With 0.5, wind-engaging side end face limit wind load usage factor CwIt is 0.6.According to momentum theorem and fluid Bernoulli equation, by following Formula calculate separately wind-engaging front end face under the conditions of Limit of Wind Speed, wind-engaging rear end face, wind-engaging side end face unilateral side by limit wind load:
P=V2CWγFρ/2
Wherein P: unit area practical limit wind load, V: wind speed is standardized according to Germanischer Lloyds, is selected under different wind regime Limit of Wind Speed, Cw: limit wind load usage factor, γF: load safety coefficient, ρ: atmospheric density.
Changing load is the well-distributed pressure applied to engine room cover travel region, standing area and horizontal protective region.To cabin Top/bottom walkable region applies 3kN/m2Well-distributed pressure, load safety coefficient 1.5;People standing area is in 20cmx20cm Apply the concentrated force of 1.5kN in region, load safety coefficient is 1.5;It is used to provide the structure member of horizontal protective, example to all Such as guardrail, horizontal load zone of action height be higher than floor or standing line 1.1m, load be distributed span 20cm or The region of 20cmx20cm, load are the concentrated force of 1.5kN, and load safety coefficient is 1.5.
Gravitational load be engine room cover from gravitational load safety coefficient under heavy load, DLC6.1 operating condition be 1.35, Qi Tagong Condition safety coefficient is 1.1.
Apply concentrated force 20kN in the loser and guardrail of wind turbine cabin cover, the direction of concentrated force is each possible generation The direction fallen.
(6) equivalent stress of the steelwork component of wind-force wind turbine cabin cover and the single layer strain of glass steel part are calculated Stress;Operating condition includes that gravitational load is superimposed and gravitational load is superimposed two kinds of limiting conditions with wind load with changing load, to calculate The ultimate strength of engine room cover.Such as following two groups of operating condition tables, table 1 is gravitational load and changing load composite condition table, and A, B, C are to stand Location point, AX, AY, AZ are that standing place corresponds to horizontal protective point;Table 2 is gravitational load and wind load composite condition.
Finite element analysis software is submitted to calculate respectively the finite element model of the above operating condition and limit wind load.
1 gravitational load of table and moving loads operating condition
2 gravitational load of table and wind load composite condition
Operating condition Explanation Load combinations
DLC6.1_N DLC6.1 wind is just blown 1.35*DLC6.1_N+1.35*gravity+dis
DLC6.1_T 15 ° of DLC6.1 windage yaw are just blown 1.35*DLC6.1_T+1.35*gravity+dis
DLC6.2_N DLC6.2 wind is just blown 1.1*DLC6.2_N+1.1*gravity+dis
DLC6.2_L DLC6.2 wind is side-blown 1.1*DLC6.2_L+1.1*gravity+dis
DLC6.2_B DLC6.2 wind back is blown 1.1*DLC6.2_B+1.1*gravity+dis
DLC7.1_N DLC7.1 wind is just blown 1.1*DLC7.1_N+1.1*gravity+dis
DLC7.1_L DLC7.1 wind is side-blown 1.1*DLC7.1_L+1.1*gravity+dis
DLC7.1_L DLC7.1 wind back is blown 1.1*DLC7.1_B+1.1*gravity+dis
(7) the glass reinforced plastic strength of parts of cover shell is assessed using composite material strength failure criteria, is applied Maximum tension and compression strain criterion and Tsai-Wu criterion determine its intensity.
Maximum tension and compression strain criterion are as follows: if without corresponding strength character data, using GL standardize specified in minimal design Allowable value, it may be assumed that design compressive strain is 0.25%, and design stretching strain is 0.35%.Material safety factor for compressive stress is design compressive strain With the ratio of the compressive strain FEM calculation value of ANSYS Workbench;Material tensile-strength safety factor be design stretching strain and The ratio of the stretching strain FEM calculation value of ANSYS Workbench shows cabin if two safety coefficient ranges are all larger than 1 Cover intensity is met the requirements.Calculate the two safety coefficient ranges be 1.5-2.5, be all larger than 1, engine room cover intensity is met the requirements.
Tsai-Wu criterion are as follows: read in the tensile strength in three direction of glass fiber material defined in pre-treatment, compression by force Degree and in-plane shear strength calculate the Failure Factor F.I. of Tsai-Wu criterion in conjunction with the engine room cover equivalent stress that software calculates, Show that engine room cover intensity is met the requirements if F.I. is less than 1.F.I. is calculated according to Tsai-Wu criterion and is distributed in 0.1-0.62 Between, less than 1, engine room cover intensity is met the requirements.
According to structural steel yield strength criterion, the intensity of steelframe structure inside engine room cover is assessed.
Test value is compared practical survey using Mr. Yu's 2W Wind turbines by engine room cover strength calculation method of the present invention Test result is it is found that the calculating deviation using this method is no more than 15%, as a result reliably.
Comparative example:
" a kind of engine room cover of wind turbine intensity is determining for the patent of invention that request for utilization number is CN201710666311.5 Method " disclosed in method calculate the engine room cover intensity of Wind turbines, cover material is reduced to orthogonal respectively to same by when model modeling Property material, not to cover shell carry out laying modeling, the deviation maximum of this strength calculation method result is more than 100%, tie Fruit is unreliable.
Therefore, the finite element simulation technology that the present invention uses includes composite plys modeling and Strength Failure assessment, base In orthotropic material property definition material properties, finite element model is more in line with reality, the calculating to engine room cover intensity As a result more accurate.
The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, although referring to aforementioned reality Applying example, invention is explained in detail, for those skilled in the art, still can be to aforementioned each implementation Technical solution documented by example is modified or equivalent replacement of some of the technical features.It is all in essence of the invention Within mind and principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.

Claims (8)

1. a kind of wind turbine cabin cover strength calculation method, which comprises the following steps:
(1) geometrical model for establishing wind turbine cabin cover, cover shell, the cover shell including glass fiber reinforced plastics composite material The guardrail and anemoclinograph of interior steel construction and the cover cover top portion;
(2) geometrical model of the wind turbine cabin cover is imported into finite element analysis software, using finite element emulation software Pretreatment function carries out laying modeling to the cover shell;
(3) material properties and section attribute for defining each component of wind turbine cabin cover, establish wind turbine cabin cover Finite element model;Wherein when definition material attribute, the Young's modulus and Poisson's ratio of glass layer different directions are defined respectively;
(4) boundary condition is applied to the finite element model of the wind turbine cabin cover;
(5) load is applied to the finite element model of the wind turbine cabin cover;
(6) it calculates the equivalent stress of steelwork component of the wind turbine cabin cover and the single layer of glass steel part answers allergic effect Power;
(7) the glass reinforced plastic strength of parts of engine room cover is assessed using composite material strength failure criteria.
2. wind turbine cabin cover strength calculation method according to claim 1, which is characterized in that the cover shell When carrying out laying modeling, gel coating resin, glass layer and foam enhancement layer are defined respectively;Defining the steel construction is structural steel Layer.
3. wind turbine cabin cover strength calculation method according to claim 2, which is characterized in that in the Wind turbines In the finite element model of engine room cover, the glass layer is simulated using shell unit, and the structure steel layer is simulated using shell unit, The foam enhancement layer is simulated using shell unit, and the gel coating resin is simulated using shell unit.
4. wind turbine cabin cover strength calculation method according to claim 2, which is characterized in that in the Wind turbines In the finite element model of engine room cover, defining the anemoclinograph is quality point, and the quality point and mounting surface establish constraint equation.
5. wind turbine cabin cover strength calculation method according to claim 4, which is characterized in that the cover shell and It is mutually bonded between the steel construction, defines contact surface multi-point constraint in the finite element model of the wind turbine cabin cover;Institute It states wind turbine cabin cover to be integrally attached on pedestal, defines and fixed about in the finite element model of the wind turbine cabin cover Beam.
6. wind turbine cabin cover strength calculation method according to claim 1, which is characterized in that the Wind turbines The load that the finite element model of engine room cover applies includes wind load, gravitational load or changing load;In the wind turbine cabin The loser and guardrail of cover apply concentrated force, and the direction of concentrated force is the direction that each possibility is fallen.
7. wind turbine cabin cover strength calculation method according to claim 6, which is characterized in that described to wind-power electricity generation It includes: that gravitational load is superimposed with changing load that the intensity of set engine room cover, which calculate,;Gravitational load is superimposed with wind load, to consider Least favorable situation calculates the ultimate strength of engine room cover.
8. wind turbine cabin cover strength calculation method according to claim 7, which is characterized in that answered using maximum tension and compression Become criterion and Tsai-Wu determines the glass layer intensity of the cover shell;According to structural steel yield strength criterion, Assess the steel construction intensity inside the wind turbine cabin cover.
CN201811311285.5A 2018-11-06 2018-11-06 A kind of wind turbine cabin cover strength calculation method Pending CN109446683A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109977619A (en) * 2019-04-26 2019-07-05 南京中人能源科技有限公司 A kind of engine room cover rigidity and stability determine method
CN110096789A (en) * 2019-04-26 2019-08-06 南京中人能源科技有限公司 A kind of pod rigidity and stability determine method
CN111709177A (en) * 2020-08-24 2020-09-25 华仪风能有限公司 Method for evaluating strength of engine room cover of wind generating set
CN113281168A (en) * 2021-05-20 2021-08-20 云度新能源汽车有限公司 Method for detecting firmness of carbon fiber accessory for automobile
US11608158B1 (en) 2022-07-25 2023-03-21 Joon Bu Park Negative Poisson's ratio materials for propellers and turbines

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CN107169191A (en) * 2017-05-10 2017-09-15 上海电气集团股份有限公司 A kind of fan blade modeling method
CN107256320A (en) * 2017-07-28 2017-10-17 中科机器人科技有限公司 A kind of small-sized hand based on composite plys throws the finite element method of unmanned plane
CN107577846A (en) * 2017-08-07 2018-01-12 许继集团有限公司 A kind of engine room cover of wind turbine strength determining method

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Publication number Priority date Publication date Assignee Title
CN102880764A (en) * 2012-10-18 2013-01-16 南车株洲电力机车研究所有限公司 Method for calculating front frame strength of wind generating set
CN107169191A (en) * 2017-05-10 2017-09-15 上海电气集团股份有限公司 A kind of fan blade modeling method
CN107256320A (en) * 2017-07-28 2017-10-17 中科机器人科技有限公司 A kind of small-sized hand based on composite plys throws the finite element method of unmanned plane
CN107577846A (en) * 2017-08-07 2018-01-12 许继集团有限公司 A kind of engine room cover of wind turbine strength determining method

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109977619A (en) * 2019-04-26 2019-07-05 南京中人能源科技有限公司 A kind of engine room cover rigidity and stability determine method
CN110096789A (en) * 2019-04-26 2019-08-06 南京中人能源科技有限公司 A kind of pod rigidity and stability determine method
CN111709177A (en) * 2020-08-24 2020-09-25 华仪风能有限公司 Method for evaluating strength of engine room cover of wind generating set
CN111709177B (en) * 2020-08-24 2020-12-04 华仪风能有限公司 Method for evaluating strength of engine room cover of wind generating set
CN113281168A (en) * 2021-05-20 2021-08-20 云度新能源汽车有限公司 Method for detecting firmness of carbon fiber accessory for automobile
US11608158B1 (en) 2022-07-25 2023-03-21 Joon Bu Park Negative Poisson's ratio materials for propellers and turbines
US11952090B2 (en) 2022-07-25 2024-04-09 Joon Bu Park Negative Poisson's ratio materials for propellers and turbines

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