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Sec.4: Ultimate Limit States (ULS) [Table of Contents] Sec.6: Accidental Limit States (ALS)

DNV-OS-C103 Structural Design of Column Stabilised Units (LRFD method)

[-] Sec.5: Fatigue Limit States (FLS)

SECTION 5
Fatigue Limit States (FLS)

Sec.5
A. General

Sec.5
A 100   General

Sec.5 A
101
   General requirements for the fatigue limit states are given in DNV-OS-C101 Sec.6. Guidance concerning fatigue calculations are given in DNV-RP-C203.

Sec.5 A
102
   Units intended to follow normal inspection requirements according to class requirements, i.e. 5 yearly inspection in sheltered waters or drydock, may apply a Design Fatigue Factor (DFF) of 1.0.

Sec.5 A
103
   Units intended to stay on location for prolonged survey period, i.e. without planned sheltered water inspection, shall comply with the requirements given in Appendix A.

Sec.5 A
104
   The design fatigue life of the unit shall be minimum 20 years.

Sec.5 A
105
    The fatigue capacity of converted units will be considered on a case-by-case basis, and is a function of the following parameters:
results and findings form surveys and assessment of critical details
service history of the unit and estimated remaining fatigue life.


Sec.5 A
106
   Local effects, e.g. due to:
slamming
sloshing
vortex shedding
dynamic pressures
mooring and riser systems.

shall be included in the fatigue damage assessment when relevant.

Sec.5 A
107
   In the assessment of fatigue resistance, relevant consideration shall be given to the effects of stress concentrations including those occurring as a result of:
fabrication tolerances, including due regard to tolerances in way of connections involved in mating sequences or section joints
cut-outs
details at connections of structural sections, e.g. cut-outs to facilitate construction welding
attachments.


Sec.5 A
108
   Local detailed finite element analysis of critical connections, e.g. pontoon and pontoon, pontoon and column, column and deck and brace connections, should be undertaken in order to identify local stress distributions, appropriate SCF's, and/or extrapolated stresses to be utilised in the fatigue evaluation. Dynamic stress variations through the plate thickness shall be checked and considered in such evaluations, see DNV-RP-C203, for further details.

Sec.5 A
109
   For well known details the local finite element analysis may be omitted, provided relevant information regarding SCF are available.

Sec.5 A
110
   Principal stresses, see DNV-RP-C203 Sec.2.2, should be applied in the evaluation of fatigue responses.

Sec.5
B. Fatigue Analysis

Sec.5
B 100   General

Sec.5 B
101
   The basis for determining the acceptability of fatigue resistance, with respect to wave loads, shall be in accordance with the requirements given in Appendix B. The required models and methods are dependent on type of operation, environment and design type of the unit.

Sec.5
B 200   World-wide operation

Sec.5 B
201
   For world wide operation the analyses shall be undertaken utilising environmental data, e.g. scatter diagram, spectrum, given in DNV-RP-C205. The North Atlantic scatter diagram shall be utilised.

Sec.5
B 300   Restricted operation

Sec.5 B
301
   The analyses shall be undertaken utilising relevant site specific environmental data for the area(s) the unit will be operated. The restrictions shall be described in the operation manual for the unit.

Sec.5
B 400   Simplified fatigue analysis

Sec.5 B
401
   Simplified fatigue analysis may be undertaken in order to establish the general acceptability of fatigue resistance, or as a screening process to identify the most critical details to be considered in a stochastic fatigue analysis, see 500.

Sec.5 B
402
   Simplified fatigue analyses should be undertaken utilising appropriate conservative design parameters. A two-parameter, Weibull distribution, see DNV-RP-C203, Sec.2.14, may be utilised to describe the long-term stress range distribution. In such cases the Weibull shape parameter 'h', see 403 for a two-pontoon semisubmersible unit should have a value of h = 1.1.

Sec.5 B
403
   The following formula may be used for simplified fatigue evaluation:

raster

n0 total number of stress variations during the lifetime of the structure 
raster  extreme stress range (MPa) that is exceeded once out of n0 stress variations. 
 
 
  
The extreme stress amplitude raster is thus given by

raster  

the shape parameter of the Weibull stress range distribution 
raster  the intercept of the design S-N curve with the log N axis (see DNV-RP-C203 Sec.2.3) 
raster  is the complete gamma function (see
DNV-RP-C203 Sec.2.14) 
the inverse slope of the S-N curve (see
DNV-RP-C203 Sec.2.14) 
DFF Design Fatigue Factor. 



Sec.5 B
404
   A simplified fatigue evaluation shall be based on dynamic stresses from design waves analysed in the global analysis as described in Sec.4 B. The stresses should be scaled to the return period of the minimum fatigue life of the unit. In such cases, scaling may be undertaken utilising the appropriate factor found from the following:

raster

ni the number of stress variations in i years appropriate to the global analysis 
raster  the extreme stress range (MPa) that is exceeded once out of ni stress variations. 

Sec.5
B 500   Stochastic fatigue analysis

Sec.5 B
501
   Stochastic fatigue analyses shall be based upon recognised procedures and principles utilising relevant site specific data or North Atlantic environmental data.

Sec.5 B
502
   Simplified fatigue analyses should be used as a "screening" process to identify locations for which a detailed, stochastic fatigue analysis should be undertaken.

Sec.5 B
503
   Fatigue analyses shall include consideration of the directional probability of the environmental data. Providing that it can be satisfactorily checked, scatter diagram data may be considered as being directionally specific. Scatter diagram for world wide operations (North Atlantic scatter diagram) is given in DNV-RP-C205. Relevant wave spectra and energy spreading shall be utilised as relevant. A Pierson-Moskowitz spectrum and a cos4 spreading function should be utilised in the evaluation of column-stabilised units.

Sec.5 B
504
   Structural response shall be determined based upon analyses of an adequate number of wave directions. Transfer functions should be established based upon consideration of a sufficient number of periods, such that the number, and values of the periods analysed:
adequately cover the wave data
satisfactorily describe transfer functions at, and around, the wave "cancellation" and "amplifying" periods (consideration should be given to take into account that such "cancellation" and "amplifying" periods may be different for different elements within the structure)
satisfactorily describe transfer functions at, and around, the relevant excitation periods of the structure.


Sec.5 B
505
   Stochastic fatigue analyses utilising simplified structural model representations of the unit, e.g. a space frame model, may form basis for identifying locations for which a stochastic fatigue analysis, utilising a detailed model of the structure, should be undertaken, e.g. at critical intersections. See also Appendix B for more details regarding models and methods.
Sec.4: Ultimate Limit States (ULS) [Table of Contents] Sec.6: Accidental Limit States (ALS)