This document discusses testing methods for analyzing the bending and torsional behavior of wind turbine blades. It describes testing a wind turbine blade box girder section under bending-torsional loading to better understand the material properties and structural response. The testing apparatus applies bending or torsional loads individually or together to the blade section sample, which is simply supported at its ends. Strain responses are measured to analyze the nonlinear deformation behavior and effects of various parameters on structural performance.
Experimental investigation of reinforcement couplers as replacement of bent-barrk pandey
In structural concrete, the provisions for anchorage of straight bars and hooks normally present detailing problems due to conjunction of reinforcement bar. Mechanical anchorage device eliminates detailing problems when conjunction of reinforcement bar. This paper represents the various method of mechanical anchorage and past work carried out on mechanical anchorage which shows the effectiveness of mechanical anchorage method over the most commonly used method.
Design & Analysis of Composite Propeller ShaftIJSRD
A Propeller Shaft is the connection between the transmission and the rear axle of the vehicles. The function of propeller shaft is to transmit the power from engine to the rear wheel in case of front engine drive vehicle. High quality steel (Steel SM45) is most commonly used material. The steel drive shaft consists of three universal joints, a center supporting bearing and a bracket, which increase the total weight of a system. The Power transmission can be improved through reducing its weight. According to previous researches many have done the various experiments to reduce the weight by changing the ply thickness, fiber orientation angle, number of plies but until now no one has studied the effect on the properties of the composite formed by changing volume fraction of carbon fiber & epoxy resin. The focus of this work will be to investigate either replacing steel structure of propeller shaft by composite structure such as carbon fiber & epoxy resin to minimize the cost and weight, also to check the suitability of composite structures by experimental method and software testing.
Material Optimization of Leaf Spring of Tractor Trolley by FEAIJMER
Leaf Spring (LS) is an indispensable machine element of the automobile sector. In this
particular work we are analyzed a LS with the help of Finite Element Method when subjected to static
loads and appropriate boundary conditions. The LS taken into consideration is that of a Tractor Trolley
having a Gross Vehicle Weight of 20 ton. According to the existing dimension of simple leaf spring it
has modeled in solid works 2013.after that cad model has used to discretized in to small no of element
and nodes to perform the required finite element analysis. Initially analysis has done for three different
materials and taken the most economic and suitable material for leaf spring in the optimization stages.
Comparision of material was perform on the basis of result obtained from the analysis of leaf spring like
von mises stress, strain and deflection.
Optimization of Multi Leaf Spring by using Design of Experiments & Simulated ...IJMER
This work carried out on a multi leaf spring of a tractor trolley with maximum load
carrying capacity of 5 Tones. The CAD model of this MLS has been modeled in CATIA V5. After
successfully preparing the CAD model, MLS is then tested in Static Structural Analysis workbench for
stress and deflection computations. The finite element analysis of the leaf spring has been performed by
converting the model into number of nodes and elements and then applying the relevant boundary
conditions under the static loading conditions. After implementation of FEA it was observed that the red
area close to shackle was undergoing maximum value of stress. This observation leads us to the
workbench of Knowledge ware and this aided us in studying the response of crucial output parameters of
MLS in the form of Stress and Deflection via Design of experiments. DOE paved the way for SAA where
optimization was carried out in order to reach the minimal stress. The corresponding values of camber
and leaf span were recorded for minimal stress
Modeling and analysis of naca 66 206 aerofoil propellereSAT Journals
Abstract
NACA aerofoil shapes have been successfully used over the years as wing and tail sections for general aviation and military aircraft, as well as propellers and helicopter rotors. The aircraft performance is highly affected by induced drag caused by wingtip vortices to improve fuel efficiency. In this research work, the analysis of NACA 66-206 aerofoil propellers was investigated for high-speed aircraft propulsion.CFD analysis is performed on the NACA aerofoil to verify the aerodynamic characteristics and enhancing the lift of the aircraft by changing the orientation of angle of attack 00, 100 and 200 and to determine the drag and lift coefficients by applying inlet velocities. An auxiliary part, winglets are added on propeller blade tip in order to improve the performance of propeller. By adding this auxiliary equipment the weight of propeller are significantly increased. To decrease the weight without compromising the performance of the propeller the fiber reinforced composite materials are used. The effects of stacking sequence layers of composite materials, which were fabricated from Kevlar, carbon, glass fibres, and epoxy resin have been used to increase the strength to weight ratio. To validate the strength of the propeller, Structural and buckling analysis is performed.
Keywords: Aerofoil, Propeller, fiber reinforcement and strength etc…
Experimental investigation of reinforcement couplers as replacement of bent-barrk pandey
In structural concrete, the provisions for anchorage of straight bars and hooks normally present detailing problems due to conjunction of reinforcement bar. Mechanical anchorage device eliminates detailing problems when conjunction of reinforcement bar. This paper represents the various method of mechanical anchorage and past work carried out on mechanical anchorage which shows the effectiveness of mechanical anchorage method over the most commonly used method.
Design & Analysis of Composite Propeller ShaftIJSRD
A Propeller Shaft is the connection between the transmission and the rear axle of the vehicles. The function of propeller shaft is to transmit the power from engine to the rear wheel in case of front engine drive vehicle. High quality steel (Steel SM45) is most commonly used material. The steel drive shaft consists of three universal joints, a center supporting bearing and a bracket, which increase the total weight of a system. The Power transmission can be improved through reducing its weight. According to previous researches many have done the various experiments to reduce the weight by changing the ply thickness, fiber orientation angle, number of plies but until now no one has studied the effect on the properties of the composite formed by changing volume fraction of carbon fiber & epoxy resin. The focus of this work will be to investigate either replacing steel structure of propeller shaft by composite structure such as carbon fiber & epoxy resin to minimize the cost and weight, also to check the suitability of composite structures by experimental method and software testing.
Material Optimization of Leaf Spring of Tractor Trolley by FEAIJMER
Leaf Spring (LS) is an indispensable machine element of the automobile sector. In this
particular work we are analyzed a LS with the help of Finite Element Method when subjected to static
loads and appropriate boundary conditions. The LS taken into consideration is that of a Tractor Trolley
having a Gross Vehicle Weight of 20 ton. According to the existing dimension of simple leaf spring it
has modeled in solid works 2013.after that cad model has used to discretized in to small no of element
and nodes to perform the required finite element analysis. Initially analysis has done for three different
materials and taken the most economic and suitable material for leaf spring in the optimization stages.
Comparision of material was perform on the basis of result obtained from the analysis of leaf spring like
von mises stress, strain and deflection.
Optimization of Multi Leaf Spring by using Design of Experiments & Simulated ...IJMER
This work carried out on a multi leaf spring of a tractor trolley with maximum load
carrying capacity of 5 Tones. The CAD model of this MLS has been modeled in CATIA V5. After
successfully preparing the CAD model, MLS is then tested in Static Structural Analysis workbench for
stress and deflection computations. The finite element analysis of the leaf spring has been performed by
converting the model into number of nodes and elements and then applying the relevant boundary
conditions under the static loading conditions. After implementation of FEA it was observed that the red
area close to shackle was undergoing maximum value of stress. This observation leads us to the
workbench of Knowledge ware and this aided us in studying the response of crucial output parameters of
MLS in the form of Stress and Deflection via Design of experiments. DOE paved the way for SAA where
optimization was carried out in order to reach the minimal stress. The corresponding values of camber
and leaf span were recorded for minimal stress
Modeling and analysis of naca 66 206 aerofoil propellereSAT Journals
Abstract
NACA aerofoil shapes have been successfully used over the years as wing and tail sections for general aviation and military aircraft, as well as propellers and helicopter rotors. The aircraft performance is highly affected by induced drag caused by wingtip vortices to improve fuel efficiency. In this research work, the analysis of NACA 66-206 aerofoil propellers was investigated for high-speed aircraft propulsion.CFD analysis is performed on the NACA aerofoil to verify the aerodynamic characteristics and enhancing the lift of the aircraft by changing the orientation of angle of attack 00, 100 and 200 and to determine the drag and lift coefficients by applying inlet velocities. An auxiliary part, winglets are added on propeller blade tip in order to improve the performance of propeller. By adding this auxiliary equipment the weight of propeller are significantly increased. To decrease the weight without compromising the performance of the propeller the fiber reinforced composite materials are used. The effects of stacking sequence layers of composite materials, which were fabricated from Kevlar, carbon, glass fibres, and epoxy resin have been used to increase the strength to weight ratio. To validate the strength of the propeller, Structural and buckling analysis is performed.
Keywords: Aerofoil, Propeller, fiber reinforcement and strength etc…
The objective of this project is to design a wind turbine that is optimized for the constraints that come with residential use. The main tasks of this project are:
> To study the design process and methodology of wind turbine
> Derive the Blade Element Momentum (BEM) theory then use it to conduct a parametric study that will determine if the optimized values of blade pitch and chord length create the most efficient blade geometry
> Analyse different air-foils to determine which one creates the most efficient wind turbine blade.
Tampere Wear Center concentrates on both scientific and practical aspects of wear and tribology.
Strengthens research in the field of wear and tribology of materials
Special expertise areas heavy abrasion, impact wear, fretting and tribology of machine elements, such as gears, bearings, brakes, seals, and frictional joints
Increasing the Strength and Reliability of Press FitsDesign World
Retaining compounds increase the strength and reliability of traditional press and shrink fits. Retaining compounds improve the distribution of stress, which increases maximum load transmission and performance. They create a physical barrier that eliminates fretting, oxidation and galvanic corrosion, which increase service life.
Recent chemical advances in retaining address assembly process variables including gaps, surface finish and cleanliness ensuring consistent performance. Application equipment provides repeatable precision dispensing.
• Recent innovations in retaining: tolerance, higher temperature resistance, primerless formulas
• New data on retaining advancements: test results on strength, oil and chemical tolerance
• How to use retaining compounds to augment a press fit for increased reliability
• Application case histories for retaining including cost and performance
IJERA (International journal of Engineering Research and Applications) is International online, ... peer reviewed journal. For more detail or submit your article, please visit www.ijera.com
1. • Non-metal materials: FRP, Foam, Resin, Wood
• V-shaped notches
•Transversely shear stress-strain curve
• Shear modulus, shear strengthObjective
Bending-torsional
load
Bending-torsional
supported
National Lab of Wind Turbine Blade R&D Center, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190
• Material properties
• Geometric structure
• Load configuration
General
Parameters
Bending/
Torsional Load
PRODUCE
Local Strain
Response
ANALYZE
Nonlinear
Deformation
Structure Design
of Blades
INPROVE
CONTENT /
OBJECTIVE
Law of Structure
Properties
AFFECT
Patent NO.: 201410532785.7
TEST PLATFORM
• Test Sample
Box Girder of wind turbine composite blade
• Support
Simple support for bending loading
Torsional support for torsional loading
• Load
Only one hydraulic cylinder for applied load
Install a distributive beam to transfer bending
load and torsional load.
Test Sample
Support
INNOVATION • Results applied more widely
Suitable for various wind blades except their root and transition regions.
• More insights can be obtained
The type and mechanism of nonlinear deformation.
The relationship between the deformation and bending-torsional load.
The effect of general parameters on structure performance.
• Simple and versatile (pure bending, pure torsion, bending+torsion )
Root
region
Transition
region Applicable region for test
• As size of wind turbine increases, the bend-twist coupling effect of blade is more
significant. It is important to understand the bending and torsional behavior.
Structural test of wind blade box girder under bending-torsional loading is meaningful and promising.
BACKGROUND
• The shapes and materials of blade are complex, so it is difficult to establish general rules for structural property
characteristics.
• The Box Girder is the main load carrying element of a wind turbine blade.
Rotating
inner pipe
Fixed
outer pipe
Patent NO.: 201410752065.1
Patent NO.: 201410752062.8
Box girder
Root
Shear web
Trailing edge
Aft panel
Spar capLeading Panel
Leading edge
Some new material and component testing technologies and equipment developed at IET-Wind are presented here.
• Rotor blades are one of the most critical components in wind turbine system, they are thin-walled composite structures with airfoil
cross-sectional profiles. Aerodynamic and structural performance of rotor blades determines the overall performance of wind turbines.
In order to improve their structural performance, the primary job is to understand the material and structural properties of blades.
• Typical construction of blades
Leading panel & Aft panel: Sandwich constructions to provide aerodynamic profiles of blade cross section
Spar cap: Composite laminates to carry primary bending moments
Shear web: Sandwich constructions to support two spar caps and transfer shear forces
Box girder
• Transversely isotropic material
• Thin-walled tubular shape
Test Sample
Ⅰ
Ⅱ
Ⅲ
Sample
adhesion
Twisting
force
Transversely
pure shear
τ23
Approach
• Fixed the sample
Clamping angle plate fixed for thin-plate sample
Bonding plate fixed for thick-plate sample
Test
Sample
Approach
Test Section
Sample
Strain
rosette
Load
Clamping
angle plate
Thin-plate
Sample
Advantage
• More uniform shear stress
distribution.
• Reduce stress concentration.
• Easy handling and assembly.
• Applied load
Longitudinal Shear in test section.
• Sawtooth in blade leading edge
Reduce Slippage
Reduce material damage
Improve strain measurement accuracy
• Multiple notch in blade trailing edge
Adapt to the different dimensions of samples
Feature
Rubber band
Sample
Extensometer
fixture
ACKNOWLEDGEMENTS This study is partly financed by National Natural Science Foundation of China (NO.51405468) and
Scientific Research Foundation for the Returned Overseas Chinese Scholars, State Education Ministry.
Thin-plate Sample
Clamping angle plate
Applicable Scope : Low-density porous materials
Patent NO.: 201420578940.4
Sawtooth leading edge
Notch trailing edge
Blade
TANG Jing, CHEN Xiao*
*chenxiao@iet.cn