Ship Reliability Analysis

Download Report

Transcript Ship Reliability Analysis

Reliability analysis of Ship Structures
Fatigue and Ultimate Strength
Fabrice Jancart
François Besnier
PRINCIPIA MARINE
[email protected]
ASRANet Colloquium 2002
Summary
 Uncertainties identification
 Rule based design and rational design
 Industrial applications using PERMAS reliability
capabilities
 Optimisation and reliability
 Fatigue
 Ultimate strength
 Conclusions
ASRANet Colloquium 2002
2
A major concern: safety
 On a competitive market
 New ship concepts
 Cost / Weight reduction
 Considerations on sea safety are
increasing
ASRANet Colloquium 2002
3
Designing in an uncertain world:
from models…
 Modelling uncertainties: due to imperfect knowledge of
phenomena and idealization and simplification in
analysis procedure
 Loading
Hydrodynamic forces (physical and mathematical models)
 Damage evaluation
 Structural response
Finite element model
Approximations, simplifications
From global to local:
 Uncertainties on fabrication effects
 Fabrication tolerance, residual stresses
 “ Natural” uncertainties
ASRANet Colloquium 2002
4
Load modelling
MODIFIED HULL, 0 knots
2,00E+04
0,00E+00
-100
-80
-60
-40
-20
0
20
40
60
80
100
Wave bending moment (t.m)
-2,00E+04
L1
-4,00E+04
L1(bis)
L2
L3
-6,00E+04
L4
L5
L6
-8,00E+04
L7
L8
-1,00E+05
-1,20E+05
-1,40E+05
X (m)
 Numerical wave bending moment scatter according to
the same hypothesis
from 5.104 T*m to 12 104 T*m
ASRANet Colloquium 2002
5
From global to local
50 000 dof
300 000 dof
ASRANet Colloquium 2002
6
Designing in an uncertain world:
From material stochastic properties
 Material properties scatter
 True or nominal values
 S-N curves approximated by

log10 ( N )  log10 (C)  m. log10 ( )
P(f)=50%
N
ASRANet Colloquium 2002
7
Designing in an uncertain world:
From “natural” stochastic properties
 Natural uncertainties: due to statistical nature of ship mission
 Environmental loading
Short term sea states
Long term sea states distribution
Missions and routes
Scatter Diagram
250
100
m(
150
s)
Occurence
200
dT
50
Signi 0
ficativ 1
e Heig 2
ht...
Pe
rio
0
16-18
Example of block decomposition
10-12
4-6
introduce scatter in prediction
3
Wave scatter diagram for one block
ASRANet Colloquium 2002
8
Rule based design:
method and limits
 Rule based approach with
 Historical hidden safety margins
 Calibrated by experience on large conventional ships
 Incompatible with innovative ship or structural concepts
 Cannot be applied on structural optimisation process
 Incompatible with uncertainties on the complex ship
environment and structural behavior
 Difficulty to determine the safety margins and their evolution
 Conflicting with first principal or rational design
 Need to update the safety partial coefficients with first principles
ASRANet Colloquium 2002
9
Reliability approach:
risk quantification
 Stochastic definition of the problem:
 Closer to reality
 Computes the probability that solicitations L exceed
strength of the structure R
Deterministic
LD
LR
R
L
R
RD
RR
R
 LL
R
Pf ( R  L)  Pf ,t arget
Probabilistic
ASRANet Colloquium 2002
10
Use of PERMAS
reliability capabilities
 Work mainly done during EC supported ASRA Esprit project
 Objective : Optimisation under reliability constraints with
Permas software
 Numerical calculation of failure probability
 Comparison of various methods:
 FORM/SORM gradient based methods
 Response surface methods (RSM)
 Crude and adaptive Monte Carlo
 Stochastic calibration of partial safety factors
 Sequences of reliability - optimisation – reliability
ASRANet Colloquium 2002
11
Industrial Application:
reinforced opening
 Optimisation of reinforced passengers ship doors
 Many occurrences of this costly detail
 Submitted to alternate shear forces
 Reinforced for fatigue criteria
F
Door
-F
ASRANet Colloquium 2002
Gangway
12
Industrial Application:
reinforced opening
Limit stress
Scantling Load
 Maximum shear stress criterion
 Evolution of reliability with optimisation
ASRANet Colloquium 2002
13
Industrial Application
reinforced opening
 Optimisation:
 Mass decreases by 10%
 Reliability of initial and optimised designs
 Stochastic loading, normal distribution
 Failure function G = lim - FE
 lim stochastic variable, normal distribution
 Failure probability increases from 1.7 10-5 to 2.8 10-3
Optimisation without reliability constraints
jeopardises safety
ASRANet Colloquium 2002
14
Industrial Application:
High speed craft
 Exploitation of high speed crafts (fast mono hulls) reveals:
Fatigue problems under alternate bending and repeated slamming
Ultimate strength problems (local and deck buckling )
Impact (slamming)
sagging
First principle design reliability based approach compared
to traditional (rule based) approach
ASRANet Colloquium 2002
15
Industrial Application:
High speed craft
Fatigue failure &
buckling collapse
Confirmed to be very critical design criteria
and subjected to significant uncertainties
 Loading uncertainties (models and stochastic nature)
 Structural strength uncertainties
 Fatigue limit
 Ultimate buckling stress
 Missions, routes and service life
 Heavy weather countermeasures
ASRANet Colloquium 2002
16
High speed craft
Buckling
High speed vessel on large
wave crest
Significant bending
moment inducing buckling
ASRANet Colloquium 2002
17
High speed craft
Buckling
Buckling reliability at mid-ship section
Failure state function
G   u     (Mextr )
 Uncertainties on
 Ultimate buckling stress u due to scatter on in-yard fabrication
tolerances, built in stresses, described by a log-normal
distribution
 Extreme value of wave bending moment Mextr, with a Gumbel
max probability density law depending on ship service time T
 : load modelling effect due to FEM approximations, with a
normal distribution
u
 (Mextr)
ASRANet Colloquium 2002
T
18
Fatigue
Reliability analysis
Large number of welded
connections, where cracks
may initiate
Typical welded structural
detail, fatigue prone
ASRANet Colloquium 2002
19
Fatigue
Reliability analysis
Historic S
K (S-N curve)
Loading
N
T
S
Detail loaded by displacements of
global model
2
1
Local mesh for stress
extrapolation (hot spot)
ASRANet Colloquium 2002
20
Fatigue
Reliability analysis
 Fatigue reliability due to global wave loads
 Failure state function
 Uncertainties on
C( T ) m
G  Dc 
S
K
 Critical damage Dc with a log-normal distribution
 S-N curve (K) due to variable fabrication conditions described by
a log-normal distribution
 Load modelling S
due to hydrodynamic numerical and navigation condition
hypothesis
due to effort in avoiding numerical singularities with the
extrapolation near the weld
described by log-normal distributions
C(T): function of service time T
ASRANet Colloquium 2002
21
Fatigue
Reliability analysis
m
 More complex failure function:

C1
m
G  Dc 
.(  1).C 2  . K Lm . S m
Kp

Dc:critical damage, taken from Classification Society recommendation and
defined by a lognormal law,
Kp associated to the S-N curve definition Sm.N=Kp,and defined by a lognormal
law
m parameter of the S-N curve
w,
parameters of the Weibull distribution
S
f (S)   
ww
 1
  S  
e xp    
 w 


C1 deterministic coefficient associated to the time at sea considered,
C2 deterministic coefficient used in the long term loading distribution
KL associated to the local stress effect
S is the stress variation during wave loading.
 gamma function :   S  

a 1  t
S
 e dt
0
ASRANet Colloquium 2002
22
Fatigue and buckling
Reliability analysis
 Buckling reliability for 1 year of exploitation
FORM
SORM
RSM_LIN
RSM_AXIAL
 - index
Pf
Tps CPU
0,947
0.89
17,2%
18,7%
29 mn
29 mn
0,95
0.95/0.89
17,1%
0.17/0.187
60 mn
72 mn
 Fatigue reliability for 15 years of exploitation
 - index
Pf
Tps CPU
Rule (SN curve)
2,05
2%
-
SORM
RSM_LIN
1,02
0.976
15,3%
16.45%
26 mn
50 mn
RSM_CCD
1,01
15,7%
84 mn
ASRANet Colloquium 2002
23
Fatigue and buckling
Elasticity
 Ultimate strength
Variable
Vs Mean value
Vs Std dev.
Loading
-5.88
-0.24
9
0.69
u
Fatigue
Variable
Vs Mean value
Vs Std dev
K (S-N curve)
Sollicitation S
1.75
3.29
-0.47
-0.58
Critical damage Dc
1.525
-0.24
ASRANet Colloquium 2002
24
Fatigue and service time
Introduction of time-variant effects in the reliability
approach :
Fatigue strength evolution
Effects of aging and corrosion
ASRANet Colloquium 2002
25
Conclusions
 « Considering alea in the design process introduces an
additional accuracy» Hasofer
 Rule based design is not always conservative
 Reliability approach can lead to an optimised and robust design.
 Simulation methods (Monte Carlo) are too costly for industrial
applications.
 Use of an existing tool coupling structural and reliability calculations
 Gradient based and RSM methods efficient
 Application on innovative ship structural concepts
ASRANet Colloquium 2002
26
Thank you for your attention
ASRANet Colloquium 2002
27