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7/23/2019 PLated Transition Piece and Comparison
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odeInnovation - Transition Piece Foundations can account for 25% of the overall cost and may
use up to 50% of the fabrication time Increasing fabrication costs over the last decade;
supply chain constraints and volatility in the price of material
ost optimi!ation is essential
TP provides the main load transfer from the turbine to"er to the#ac$et substructure
TP is a critical component of the "ind turbine structure
Therefore the integrity and cost of the TP is critical to the "holedesign
&'( has designed several innovative transition piece conceptsfrom "hich t"o have the potential to reduce the overall cost of"ind turbines support structures;
-
Plated Transition Piece- onical Transition Piece
7/23/2019 PLated Transition Piece and Comparison
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odeInnovation ) &'( Plated TP
*rea of highest +tress
concentration dramatically
affecting fatigue life and
hence plated design
7/23/2019 PLated Transition Piece and Comparison
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odeonventional vs Plated TPsonventional TP
Heavy weight Oval section/Complex castings / welding
operations required. The need for specialist fabricators limiting
supply chain options
High stress concentrations at central column /support arms interface, requiring heavy
sections to achieve load transfer efficiency to
meet acceptable fatigue life criteria ifficult to inspect the overlaid weld and tube
internal weld
Plated TP
relatively light simple conventional plate fabrication methods !imple fab " #vailable local supply chain !pecial fatigue resistant detail $%!tress
&elieving 'ings( greatly improved fatigue life
) factor of * to + #bility to reduce stress locally without need
for complete T resi-ing ase of maintenance / inspection with weld
open for access eading to extended life and reduce costs of
wind turbine support structures
7/23/2019 PLated Transition Piece and Comparison
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odeT"isted #ac$et vs Plated TP ,ac$ets .T"isted #ac$et
0. Heavy weight
1. Complex 2 tubular
fabrication / welding operations
required as shown in the
mainstream pro3ect
2. The need for specialist
fabricators limiting supply
chain options
*. High stress concentrations at
central column / support brace
interface, requiring heavy
sections to meet acceptable
fatigue life criteria
+. lac4 of redundancies hence
fatigue crac4 can lead to
system failure during operation
Plated TP Jacket
0. relatively light
1. simple conventional plated
fabrication
2. !imple fab " #vailable localsupply chain
*. !pecial fatigue resistant
detail $%!tress &elieving
'ings( greatly improved
fatigue strength, a factor of *
to +, hence steel saving can
be made+. 5ood redundancy hence
early fatigue crac4 is
tolerance during operation.
7/23/2019 PLated Transition Piece and Comparison
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odeT"isted #ac$et vs Plated TP ,ac$ets 2.T"isted #ac$et
0. !mall base width hence larger
and longer piles required
1. ile in large battered angle
which can lead to reduced
piling efficiency and piling
refusal/lateral vibration or
movement2. &emedial measures for pile
refusal such as drilling is
difficult
*. ow natural frequency in the
torsional vibration mode can
bring fatigue problem during
the detailed design stage+. iling is to be done together
with structure, which brings
scheduling problem
Plated TP Jacket
0. 6ac4et base width can be
ad3usted to reduce piling
needs1. ile efficiency high hence
chance of piling refusal low
2. &emedial measure for pile
refusal such as drilling are
available in conventional
technique
*. High natural vibration modefor torsional mode
+. re piling can be conducted
to optimi-e offshore
operation
7/23/2019 PLated Transition Piece and Comparison
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odeInnovation ) &'( Plated Transition Piece
+imple load transfer via
plates
(asy fabrication
/elatively light "eight
igh fatigue strength from
reduced stress due to acombination of1
+imple load transfer
stress relieving "ing
detail /educed *P( cost
(asy maintenance and repair
leading to reduced &P( cost
Figuratively representative TP.
Patent Applied
7/23/2019 PLated Transition Piece and Comparison
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ode
Inclined Plate Central C lumn
Without Wing With Wing Fatigue Factor Without Wing With Wing Fatigue Factor
Maximumstress at 40 mmrom intersection
!4" MPa
#4$%&0!psi'
(&.4 MPa
#)"%*!)psi'
346 "4* MPa
#!*%*!4psi'
)"$ MPa
#)(%+)0psi'
40
Position omaximum stress
Weldtermination point
,on-eldtermination point
Weldtermination point
,on-eldtermination point
atigue limitingstress at )0/+cycles
4).*" Mpa
#&%0""psi'
*).&! Mpa
#+%4((psi'
427 4).*" Mpa
#&%0""psi'
*).&! Mpa
#+%4((psi'
)."4
ompounded 742 2436
Innovation +tress oncentrations 8 Fatigue
(9uivalent Fatigue loading used for analysis is supplied
by +iemens for :eneris Fatigue load under urricane
condition
7/23/2019 PLated Transition Piece and Comparison
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odeInnovation - Plated TP :eometric Features1
Top section 1olted to the WT2
toer 1ase
Middle platorm provide easy
operational space
Access into the loer section o
the transition piece possi1le. 3ec plate can 1e grated to
urther reduce eight.
5ottom section connected to the
legs o 6acet structure% directly
transerring loads
Flexi1le 6acet leg spacing.
7/23/2019 PLated Transition Piece and Comparison
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ode+tructural 'ra"ings ) Transition piece
7/23/2019 PLated Transition Piece and Comparison
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ode+tructural 'ra"ings - Isometric
7/23/2019 PLated Transition Piece and Comparison
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ode+tructural Illustration