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The Seventh Asia-Pacific Conference on<br />

Wind Engineering, November 8-12, 2009,<br />

Taipei, Taiwan<br />

A STUDY OF WIND-RESISTANT SAFETY DESIGN OF WIND<br />

TURBINES TOWER SYSTEM<br />

Ching-Wen Chien 1 , Jing-Jong Jang 2<br />

1 Ph.D. Candidate, Department <strong>of</strong> Harbor and River Engineering, National Taiwan Ocean<br />

University/ E&C Engineering Corporation Keelung, Taiwan, Taiwan,<br />

d93520010@ntou.edu.tw<br />

2 Pr<strong>of</strong>essor, Department <strong>of</strong> Harbor and River Engineering, National Taiwan Ocean<br />

University Keelung, Taiwan, Taiwan, jangjj@ntou.edu.tw<br />

ABSTRACT<br />

During the last decade, many <strong>wind</strong> turbine <strong>tower</strong>s damage were caused by typhoons strike repeatedly. As the<br />

cost impact <strong>of</strong> buckling failure, this <strong>study</strong> starts to investigate the characteristics <strong>of</strong> <strong>wind</strong> turbulence and buckling<br />

resistance procedure is presented. The theories <strong>of</strong> the dynamic <strong>wind</strong> loading in along-<strong>wind</strong> and across-<strong>wind</strong><br />

with/without the torsional force are applied to analysis the total <strong>wind</strong> force. Furthermore, the finite element<br />

analysis is used to obtain the across-<strong>wind</strong> force <strong>of</strong> the response. Some basic features <strong>of</strong> the analysis and the<br />

<strong>design</strong> <strong>of</strong> the prototype <strong>of</strong> a steel 660 KW <strong>wind</strong> turbine <strong>tower</strong> in Taiwan are presented. These results <strong>of</strong> this<br />

research highlight the following: First, the 660 KW <strong>wind</strong> <strong>turbines</strong> <strong>tower</strong> should be <strong>design</strong>ed with natural period<br />

less than one second, and the gust effect factor, G, equal to 2.38. Second, at low mean <strong>wind</strong> velocities, due to the<br />

vortex shedding resonance with the fundamental mode <strong>of</strong> vibration, the across-<strong>wind</strong> response is higher than the<br />

along-<strong>wind</strong> response. Third, the turbulence intensity is observed to 25~44% in Typhoon Jangmi, and the along<strong>wind</strong><br />

response exceeds the total <strong>wind</strong> response. Fourth, the total <strong>wind</strong> force without considering torsional force<br />

will be underestimated 4.2%, therefore when the maximum deflection is closed to 1 %, the torsional force should<br />

not be ignored for the <strong>safety</strong> <strong>design</strong>.<br />

KEYWORDS: TORSIONAL WIND FORCE, WIND TURBINE TOWER, TOTAL WIND FORCE,<br />

TURBULENCE INTENSITY<br />

Introduction<br />

There are many different configurations <strong>of</strong> <strong>wind</strong> turbine generator <strong>system</strong> (WTGS) have<br />

been built in large amounts around the world. As the tubular <strong>tower</strong> occupies area smaller than<br />

the lattice steel <strong>tower</strong>, then the distance <strong>of</strong> the blade between the shaft is increased to reduce<br />

the aerodynamic effect (Chien and Jang, 2008a). Moreover, the tubular <strong>tower</strong>s are <strong>design</strong>ed as<br />

truncated cones with their diameter increasing towards the base in order to increase their<br />

strength and at the same time to save material (Stathopoulos and Baniotopoulos 2007).<br />

Consequently, the tubular <strong>tower</strong> has a large ratio <strong>of</strong> height to least horizontal dimension that<br />

makes it a particularly more slender and <strong>wind</strong>-sensitive than any other structures. On the one<br />

hand, from structural characteristics <strong>of</strong> the tubular <strong>tower</strong>, it is a statically-determinate<br />

structure, due to lack <strong>of</strong> the cumulated experience for the <strong>design</strong> in a proper way with respect<br />

to serviceability, strength and <strong>safety</strong> criteria. Therefore, such structures are easier failure than<br />

common structures. As in these areas with typhoon application <strong>of</strong> IEC-61400-1 codes or<br />

National standard <strong>wind</strong> codes and the fact that information on external conditions is limited<br />

may result in either too high cost or too high risk (Clausen and Pagalilawan, 2006). In 2003,


The Seventh Asia-Pacific Conference on Wind Engineering, November 8-12, 2009, Taipei, Taiwan<br />

the supporting <strong>of</strong> self-standing <strong>system</strong> were collapsed or partially damaged by Typhoon<br />

Maemi in Okinawa, Japan. The authors have investigated some failures from geometric<br />

properties <strong>of</strong> <strong>wind</strong> turbine <strong>tower</strong> due to typhoon strike (Jang, and Chien, 2009), developed the<br />

procedure <strong>of</strong> Wind-Resistant Design (WRD) for the support structures subjected to <strong>wind</strong>induced<br />

excitation from vortex shedding and gust buffeting (Chien and Jang, 2008b).<br />

The <strong>study</strong> is aimed at analyzing the Typhoon Jammie speed from the Central Weather<br />

Bureau to compare the <strong>design</strong> basis <strong>of</strong> <strong>wind</strong> turbine <strong>tower</strong>s. The authors deal with the<br />

classical problems <strong>of</strong> the dynamic along<strong>wind</strong> response and the equivalent static forces,<br />

referred to as the gust factors, aimed at determining the maximum response for engineering<br />

application to <strong>wind</strong> turbine <strong>tower</strong>s <strong>design</strong>. The authors have also obtained the regression<br />

formulas <strong>of</strong> natural period with/without turbine based on the theory <strong>of</strong> Generalized<br />

Coordinate System Method and FEM analysis (Chien and Jang, 2005). As the natural period<br />

is a good verification in the discrimination <strong>of</strong> 1sec. <strong>of</strong> natural periods to rigidity and flexible<br />

structure or not for a <strong>wind</strong> turbine <strong>tower</strong> than the ratio <strong>of</strong> Height/Diameter method (Chien and<br />

Jang, 2008b). On the other hand, the structure is usually assumed to undergo aerodynamic<br />

actions partly distributed along the axis <strong>of</strong> the shaft and partly concentrated in the geometrical<br />

center <strong>of</strong> the masses, therefore torsion load is always ignored (Solaria, 1999). As a matter <strong>of</strong><br />

fact, due to the turbulence or typhoon strike, the torsion <strong>of</strong> the shaft in the across<strong>wind</strong> planes<br />

should not be ignored. However, it’s still not found the application <strong>of</strong> torsion theory at present,<br />

only there are torsion theories in Japan's code (AIJ 1996). In the ASCE7 code adopts the<br />

eccentricity e for rigid structures to consider the torsional loads (ASCE7 2005). As for more<br />

accurate prediction <strong>of</strong> damage due to typhoon strike, it is important to compare the along<strong>wind</strong><br />

force to total <strong>wind</strong> force with/without the torsional force. A benchmark model is based<br />

on the VESTA’s 660 Kw (VESTA, 1998) prototype with Finite Element analysis performed<br />

by applying appropriately linearly elastic laws for the analysis <strong>of</strong> across-<strong>wind</strong> response.<br />

Furthermore, the <strong>design</strong> <strong>of</strong> the steel <strong>tower</strong> for gravity and <strong>wind</strong> loadings is according to the<br />

relevant Taiwan code the results <strong>of</strong> the analyses to perform. The <strong>study</strong> includes three parts:<br />

(1); along-<strong>wind</strong> response analysis; (2); across-<strong>wind</strong> response with/without torsional force<br />

analysis; (3) develops the procedure <strong>of</strong> WRD for a <strong>wind</strong> turbine <strong>tower</strong>.<br />

Turbulence Intensity and Typhoon Speed<br />

The turbulence intensity, also <strong>of</strong>ten referred to as turbulence level, is defined as<br />

I<br />

u<br />

u ' ( t)<br />

= (1)<br />

U<br />

where<br />

u ' ( t ) is the root-mean-square <strong>of</strong> the turbulent velocity fluctuations and U is the mean<br />

velocity. If the turbulent energy, k, is known<br />

u ' ( t)<br />

can be computed as<br />

1 2<br />

= + + = (2)<br />

3 3<br />

' 2 2 2<br />

u ( t) ( u( x, t) u( y, t) u( z, t) ) k<br />

U can be computed from the three mean velocity components U t ( x ) , U t ( y ) and U t ( z ) as<br />

U U x U y U z<br />

2 2 2<br />

= t ( ) + t ( ) + t ( )<br />

(3)<br />

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The Seventh Asia-Pacific Conference on Wind Engineering, November 8-12, 2009, Taipei, Taiwan<br />

Turbulence is the factor which describes short term <strong>wind</strong> variation/fluctuations. WTGS<br />

<strong>design</strong>ed according to the special <strong>safety</strong> class as defined in Table 1. As defined in the IEC<br />

61400-1 <strong>wind</strong> turbine <strong>design</strong>/<strong>safety</strong> standard, the largest <strong>wind</strong> speed to be considered is called<br />

“V e50 ” which is the maximum gust over a 50-year return period for a 3-second averaging time.<br />

A <strong>design</strong>ates the category for higher turbulence characteristics, B <strong>design</strong>ates the category for<br />

lower turbulence characteristics, I 15 is the characteristic value <strong>of</strong> the turbulence intensity at 15<br />

m/s, a is the slope parameter (IEC-61400-1, 1998). Generally, a WTGS is supposed to be<br />

<strong>design</strong>ed to stop rotation for their blades , for example, changing pitch <strong>of</strong> blades in order to<br />

reduce <strong>wind</strong> loads on a <strong>tower</strong> and blades in case <strong>of</strong> high <strong>wind</strong> more than 25 m/s. The<br />

maximum allowable extreme <strong>wind</strong> speeds are listed in Table 2. Fig. 1(a) shows the path <strong>of</strong><br />

Typhoon Jangmi strike in Taiwan. Fig. 1(b) shows the maximum mean <strong>wind</strong> speed, the<br />

maximum instantaneous <strong>wind</strong> speed were observed 32m/s, 46.1m/s respectively, in the<br />

Wuchi station by the Central Weather Bureau. The turbulence intensity is equal to 44% by Eq.<br />

(1) as shown in Table 3. Typically the turbulence intensity is between 5% and 20 %.<br />

Therefore, due to this circumstance the <strong>tower</strong> is prone to buckling failure. On the other hand,<br />

the <strong>wind</strong> speed <strong>of</strong> average was 56m/s on the last ten minutes, the maximum instantaneous<br />

<strong>wind</strong> speed during the Typhoon Jangmi was investigated exceed 70 m/s by the Taiwan Power<br />

Company (TPC). Fig. 1(c) shows the broken <strong>tower</strong> <strong>of</strong> <strong>wind</strong> <strong>turbines</strong> by Typhoon Jangmi<br />

strike in Taiwan. Those exceeded IEC’s 50 year <strong>design</strong> <strong>wind</strong> speed U 50 for class I <strong>wind</strong><br />

turbine. Therefore it cannot be expected that <strong>design</strong>s made according to the IEC 61400-1 will<br />

ensure sufficient structural reliability <strong>of</strong> <strong>turbines</strong> in regions <strong>of</strong> the world, where typhoons<br />

occur.<br />

Buckling Resistance<br />

As the thickness is less than the radius <strong>of</strong> the shaft, the <strong>wind</strong> turbine <strong>tower</strong> should be<br />

considered as a thin wall structure. However, the formula <strong>of</strong> moment in inertia is derived<br />

3<br />

as I = π R t ; R is the average <strong>of</strong> radius; t is the thickness <strong>of</strong> the shaft. Usually, the<br />

manufactory and owner increased the radius R than the thickness <strong>of</strong> the shaft to obtain<br />

stronger the stiffness <strong>of</strong> the structure under the same total amount <strong>of</strong> steel weight. Due to this<br />

circumstance the <strong>tower</strong> is prone to local buckling. Concerning the fatigue limit state, the<br />

width to their thickness ratio should be satisfied the following <strong>of</strong> buckling resistance<br />

requirements. First, geometric <strong>design</strong> should be based on the diameter-thickness (D/t) ratio<br />

less than 125 to avoid the local buckling <strong>of</strong> <strong>wind</strong> turbine <strong>tower</strong>. Second, if the ratio <strong>of</strong> D/t is<br />

large than 125, moreover by Eq. (4) to control the buckling failure as follow (Schilling, 1965)<br />

50<br />

25<br />

0 5 10 15 20 25<br />

Max. Ave. Wind Speed<br />

40<br />

Max. Gust Wind Speed<br />

20<br />

Wind Speed(m/s)<br />

30<br />

15<br />

10<br />

20<br />

5<br />

10<br />

0 5 10 15 20 25<br />

Time (HR.)<br />

0<br />

Fig. 1: (a) Typhoon Jangmi (b) Wind Speeds in Wuchi Station (c) Broken WTGS<br />

3


The Seventh Asia-Pacific Conference on Wind Engineering, November 8-12, 2009, Taipei, Taiwan<br />

Table 1: Basic Parameters for WTGS Classes<br />

WTGS Class I II III IV<br />

U ref (m/s) 50 42.5 37.5 30<br />

U ave (m/s) 10 8.5 7.5 6<br />

A I 15 (-)<br />

0.18 0.18 0.18 0.18<br />

a (-) 2 2 2 2<br />

B I 15 (-)<br />

0.16 0.16 0.16 0.16<br />

a (-) 3 3 3 3<br />

Table 2: Wind Speed According to IEC/GL<br />

Max. 10 Max. 3 sec. Gust Stop <strong>wind</strong> speed<br />

min. mean mean max. acc.<br />

V47 – 660 kW 50 m/s 70 m/s 10 m/s 2 25 m/s<br />

Table 3: Wind Turbulence Intensity<br />

Stations Max. 10<br />

min. mean<br />

Max. 3 sec.<br />

mean<br />

Gust<br />

max. acc.<br />

turbulence<br />

intensity<br />

Wuchi station 32 m/s 46 m/s 14 m/s 2 44%<br />

TPC station 56 m/s 70 m/s 14 m/s 2 25%<br />

D<br />

< 0.1259⋅ E s , (4)<br />

t F y<br />

D is diameter <strong>of</strong> shaft, E s is modulus <strong>of</strong> elasticity, and F y is yield stress. Third, the ratio <strong>of</strong><br />

lateral deflection-height should be controlled less than 1% to avoid the buckling failure.<br />

Analysis <strong>of</strong> Along-Wind Load<br />

Davenport derives a factor, which the R.M.S. (Root Mean Square) component would be<br />

exceeded with a probability <strong>of</strong> 50%. After further refinement Davenport recommended the<br />

following expression for peak factor<br />

0.577<br />

g = 2× ln(3600 n)<br />

+<br />

, (5)<br />

2×<br />

ln(3600 n)<br />

where n is the natural frequency. Thus, maximum instantaneous <strong>wind</strong> velocity is then<br />

Umax = U + g ⋅ σ ( U ) , (6)<br />

The along-<strong>wind</strong> response is usually obtained by the gust effect factor method. This approach<br />

is based on the maximum response that can be represented by the corresponding mean<br />

response multiply a gust effect factor. The F<br />

d<br />

total drag force at any point for a <strong>wind</strong> turbine<br />

<strong>tower</strong> is given by Eq. (7), and the mean displacement <strong>of</strong> mean along-<strong>wind</strong> velocity at the<br />

average height point is obtained by Eq. (8)<br />

1<br />

H 2<br />

Fd = ⋅Cd ⋅ ρa<br />

⋅ ∫ V( z ) ⋅ B( z ) ⋅φ( z )dz<br />

0<br />

2<br />

, (7)<br />

Fd<br />

X ave = ; K 1 =m 1 (2πn 1 ) 2 ,<br />

K<br />

(8)<br />

1<br />

4


The Seventh Asia-Pacific Conference on Wind Engineering, November 8-12, 2009, Taipei, Taiwan<br />

On the one hand, the total along-<strong>wind</strong> displacement<br />

X<br />

a(max)<br />

( H ) can be divided into two parts:<br />

First, the average displacement x (H ) is caused by average <strong>wind</strong> speed. Second, the turbulent<br />

displacement x<br />

a(max)<br />

( H )is caused by the turbulence <strong>wind</strong> speed. Hence, the total along-<strong>wind</strong><br />

displacement <strong>of</strong> a structure subjected to along-<strong>wind</strong> force is given by Eq. (9), the gust effect<br />

factor G(z) is refered to Eqs. (8), (9) to obtain the Eq. (10):<br />

where<br />

X ( H ) = x( H ) + [( g σ ) + ( g σ ) ] = x( H ) + x<br />

a(max)<br />

( H ), (9)<br />

2 2 1/<br />

2<br />

a(max) B Bx R Rx<br />

x a (max)<br />

g = 2× ln( 3600n ) +<br />

R<br />

G( z) = 1+ x( z)<br />

, (10)<br />

0.<br />

577<br />

2×<br />

ln( 3600n )<br />

is the resonant peak factor, gB<br />

≅ 3.5 . σ<br />

BX is<br />

the R.M.S. value <strong>of</strong> the non-resonant displacement; σ<br />

RX is the R.M.S. value <strong>of</strong> the resonant<br />

displacement.<br />

Analysis <strong>of</strong> Across-Aind Load and Torsional Wind Load<br />

Due to vortex shedding, when the mean <strong>design</strong> <strong>wind</strong> speed (U H ) is greater than the critical<br />

across-<strong>wind</strong> speed (U cr ) that always falls in the resonance area. U H (m/sec) can be calculated<br />

by local <strong>wind</strong> code. When the <strong>wind</strong> velocity is located in vortex resonance area, <strong>design</strong> the<br />

<strong>wind</strong> turbine <strong>tower</strong> should be considered in the across-<strong>wind</strong> loads. Vortex resonance area is<br />

between 0.50 and 1.30U H as defined here. Lock-in effect is subjected to the vortex shedding<br />

frequency and structure natural frequency nearly; within certain range <strong>of</strong> <strong>wind</strong> velocities.<br />

With the round cylinder as an example when there is turbulence, it’s S t =0.2 and the U cr value<br />

can be obtained by Eq. (11):<br />

5D<br />

Ucr<br />

= , (11)<br />

T<br />

T j is the natural period <strong>of</strong> structure (j=1, 2….n). However, vortex shedding although can<br />

"lock-in" and continue as the velocity increases or decreases slightly, if the velocity changes<br />

by more than 30%, the vortex shedding will stop, and across-<strong>wind</strong> load is no need to consider<br />

at outside this range. The across-<strong>wind</strong> force is obtained by Eq. (12) (Tsai, et al., 2006).<br />

2 Z<br />

Wrz = Ucr ⋅ ⋅Cr<br />

⋅ A , (12)<br />

h<br />

W rz is the across-<strong>wind</strong> force at height z; C r is the <strong>wind</strong> force <strong>of</strong> vortex resonance; A is the<br />

project area <strong>of</strong> the structure. The tip displacement <strong>of</strong> the <strong>wind</strong> turbine <strong>tower</strong> in across-<strong>wind</strong><br />

force is obtained by Eq. (13) (Wang, 1995)<br />

2<br />

Ucr<br />

⋅ D ⋅φ( Z)<br />

X<br />

c<br />

=<br />

, (13)<br />

2<br />

8000⋅ξ<br />

⋅m⋅ω<br />

where ξ is the damping ratio <strong>of</strong> structure (=0.02); φ ( Z ) is a function <strong>of</strong> viration mode, the<br />

critical <strong>wind</strong> speeds for torsional <strong>wind</strong> force is obtained by Eq. (14) (Tsai, et al., 2006) form<br />

the torsion theories in Japan's code (AIJ 1996).<br />

j<br />

' Z 1<br />

Tz<br />

1.8 ( )<br />

T Z T<br />

1<br />

TR<br />

M = ⋅ q h ⋅ C ⋅ A ⋅ B ⋅ g R<br />

H<br />

⋅ ⋅ + β<br />

, (14)<br />

5


The Seventh Asia-Pacific Conference on Wind Engineering, November 8-12, 2009, Taipei, Taiwan<br />

q( h ) is a velocity pressure, C is the parameter <strong>of</strong> torsional <strong>wind</strong> force,<br />

'<br />

T<br />

A<br />

Z<br />

is the projected area at<br />

R is the coefficient <strong>of</strong><br />

height Z, g<br />

T<br />

is the coefficient <strong>of</strong> peak factor <strong>of</strong> torsional <strong>wind</strong> force,<br />

TR<br />

resonance factor <strong>of</strong> torsional <strong>wind</strong> force, β is the damping ratio, B is the projected breadth.<br />

The total dynamic <strong>wind</strong> load effect could be calculated as follow:<br />

X = X + X , (15)<br />

2 2<br />

t(max)<br />

a max c<br />

X t is total dynamic <strong>wind</strong> load; X a(max) and X c are effect <strong>of</strong> along-<strong>wind</strong> load and across-<strong>wind</strong><br />

load, respectively.<br />

Case Study and Procedure <strong>of</strong> Wind Resistat Design<br />

A benchmark <strong>of</strong> steel tubular <strong>tower</strong> is based on a VEST’s V47-660kw to set up where is<br />

located in the Wu-chi as shown in Figs. 2(a)~(c). Design <strong>of</strong> <strong>tower</strong> is made by steel structure<br />

with the piling foundation. As simplification calculation, the stepped cylindrical section is<br />

transformed into a uniform thickness. Therefore, the analysis is adopted the parameters <strong>of</strong> 2/3<br />

height for the <strong>wind</strong> turbine <strong>tower</strong>, the diameter is equal to 3(2.45) m, the thickness <strong>of</strong> shaft is<br />

15 (10) mm; the height is about 50m. The procedure <strong>of</strong> WRD as follow: First Step, the<br />

natural period <strong>of</strong> the benchmark is control in first mode by eignvalue analysis as shown in<br />

Table 4. As the benchmark is a symmetrical structure, their vibration periods are close to each<br />

other, the first two fundamental modes <strong>of</strong> the model are dominated by lateral translations.<br />

Second Step, the <strong>design</strong> <strong>wind</strong> speed is used by the Typhoon Jangmi (U 10 (C) =56m/s), the gust<br />

factor, along-<strong>wind</strong> displacement (X a ) is calculated by Eqs. (8)~(10) as shown in Table 5.<br />

Third Step, the analysis <strong>of</strong> across-<strong>wind</strong> resonance calculated by Eq. (11), one shall consider<br />

the across-<strong>wind</strong> force in the resonance area as shown in Table 4, and the results <strong>of</strong> across<strong>wind</strong><br />

force with/without torsional force is calculated by Eqs. (12), (14) as shown in Table 6.<br />

Fourth step, the across-<strong>wind</strong> force is applied into SAP2000 model to obtain the across-<strong>wind</strong><br />

displacement as shown in Fig. 3. As the maximum deflection is closed to 1 %, the ration is<br />

just satisfied to the buckling resistance requirements as shown in Table 5. Fifth step, Fig. 4<br />

compares the base moment <strong>of</strong> total <strong>wind</strong> force under U cr =15.6 (m/sec) with the only<br />

consideration <strong>of</strong> the along<strong>wind</strong> force under Typhoon Jangmi speed (U 10 =56m/s) or Taiwan<br />

<strong>wind</strong> code (U 10 =32.5m/s) for <strong>design</strong> the <strong>wind</strong> turbine <strong>tower</strong>.<br />

Figure 2: (a) Prototype <strong>of</strong> 660KW (b) Benchmark Model (c) Prototype (1 st mode shape)<br />

6


The Seventh Asia-Pacific Conference on Wind Engineering, November 8-12, 2009, Taipei, Taiwan<br />

Table 4 Analysis <strong>of</strong> Across-Wind Resonance (U h =U 10 (C)=56m/s)<br />

Numbers <strong>of</strong><br />

mode<br />

D<br />

(m)<br />

T j<br />

(sec)<br />

U cr<br />

(m/sec)<br />

U h<br />

(m/sec)<br />

Across-<strong>wind</strong><br />

resonance<br />

1 2.45, 3 1.039, 0.984 12, 15 71<br />

U h > U cr<br />

Lock-in<br />

2 2.45, 3 0.169, 0.223 73 , 67 71 U cr >20m/s<br />

Table 5 Analysis <strong>of</strong> Displacement and Gust Effect Factor (U 10 (C)=56m/s, D=3m, t=15mm)<br />

X ave X a(max) X c X t(max) Total<br />

Deflection<br />

G(Z)<br />

By equation Eq. (8) Eq. (9) Sap2000 Eq. (15) Eq. (15)/H Eq. (10)<br />

Unit (cm) (cm) (cm) (cm) %<br />

Benchmark 3.25 4.47 50.4 50.59 1 2.38<br />

60<br />

3000<br />

50.4<br />

D=3m , t=15mm<br />

Displacment(mm)<br />

40<br />

22.95<br />

36.38<br />

Base moment (t-m)<br />

2000<br />

Ma=Bending Moment(T-M)<br />

M a (U 10 =56 m/s)<br />

M a (U 10 =32.5m/s)<br />

M a (w/o Torsion force)<br />

M a (with Torsion force)<br />

20<br />

1000<br />

11.29<br />

3.11<br />

0<br />

0<br />

0<br />

0 10 20 30 40 50<br />

Height (m)<br />

Figure 3: Sap2000 Analysis <strong>of</strong><br />

Across-Wind Response (U cr =15m/s)<br />

0 10 20 30 40 50<br />

Height(m)<br />

Figure 4: Comparison <strong>of</strong> Basemoment<br />

Conclusions<br />

It’s recommended that the 660 KW <strong>wind</strong> <strong>turbines</strong> <strong>tower</strong> should be <strong>design</strong>ed with natural<br />

period less than one second, and the gust effect factor, G, equal to 2.38. Presently, the G value<br />

is greater than 1.77 for rigid structures according to the Taiwan building code 2006. As for<br />

results, Typhoon Jangmi speed (U 10 =56m/s) in along<strong>wind</strong> force is large than the total <strong>wind</strong><br />

force (U cr =15.6m/s, U 10 =11.37m/s in the along<strong>wind</strong> and cross<strong>wind</strong>) <strong>of</strong> WTGS. However, due<br />

to the large shaft flexibility, the torsional loading in the across<strong>wind</strong> response should not be<br />

ignored. It’s underestimated 4.2% in the total <strong>wind</strong> force without torsional <strong>wind</strong> force for<br />

<strong>safety</strong> <strong>design</strong>. When the maximum deflection is closed to 1 %, the torsional force should not<br />

be ignored for the stiffeners (stiffening rings, door tingers, ribs and frame) and the flanges to<br />

check against local buckling.<br />

7


The Seventh Asia-Pacific Conference on Wind Engineering, November 8-12, 2009, Taipei, Taiwan<br />

Table 6 Analysis <strong>of</strong> total <strong>wind</strong> force with/without torsional <strong>wind</strong> force for <strong>wind</strong>-power <strong>tower</strong><br />

(U cr =15m/s, U 10 =11m/s, D=3m, t=15mm)<br />

Height<br />

Dynamic<br />

along<strong>wind</strong><br />

force<br />

Across-<strong>wind</strong><br />

force w/o<br />

torsion force<br />

Torsional<br />

force<br />

Across-<strong>wind</strong><br />

force with<br />

torsional force<br />

Total <strong>wind</strong> force<br />

w/o torsional<br />

force<br />

Total <strong>wind</strong><br />

force with<br />

torsional force<br />

(m) (kg) (kg) (kg) (kg) (kg) (kg)<br />

50.00 325.97 14048.94 618.37 14667.31 14053 14671<br />

40.00 609.72 22478.30 989.40 23467.70 22487 23476<br />

30.00 559.31 16858.72 742.05 17600.77 16868 17610<br />

20.00 495.25 11239.15 494.70 11733.85 11250 11744<br />

10.00 382.15 5338.60 234.98 5573.58 5352 5587<br />

1.00 90.72 252.88 13.60 266.49 269 282<br />

total 2463.12 70216.58 3093.10 73309.69 70278.26 73368.67<br />

Acknowledgements<br />

The authors would like to thank the Taiwan Natural Science Council for finance support this<br />

research (NSC-98-2221-E-019-016).<br />

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8

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