150 years Recurrent inspections of pressure vessels under cyclic stress Hans-Ulrich Moser Technische Anlagenüberwachung BASF BASF SE Ludwigshafen 11. Europäische Druckgerätetage 30.6. – 1.7.2015
150 years
Recurrent inspections of pressurevessels under cyclic stress
Hans-Ulrich MoserTechnische Anlagenüberwachung BASFBASF SE Ludwigshafen
11. Europäische Druckgerätetage30.6. – 1.7.2015
150 years
Structure
Fatigue
Technical rules
Damage mechanisms
Test methods
Example sending pressure vessel for pneumatic conveying
Example inspection concept pressure swing adsorber
Summary
2
150 yearsFatigueDefinition according to AD2000
design on staticload
continuouslyoperated
Apparatus/Reactors
Number ofload cycles10000
Agitated vessels(parts under
pressure)
Buffer vessel Kneader
..
Agitated vessels(Shaft, agitator)
MachineryPressure swing adsorber
design on limited lifespan
endurancedesign
2·106
..
Paddle dryer
3
150 years
Rules (1): Technical rules
TRB 801, No.15 Pressure vessels under cyclic stress (withdrawn):• Recurrent inspections at least after half of the calculated lifespan• Inspection prior putting into service: Identification of the most highly
stressed areas• Higher amount of inspections of welding seams during manufacturing• ........
TRBS 1201 part 2, internal inspection:• Identification of the most highly stressed areas• Inspection concept (Consideration of the occuring load cycles)• Testing on cracks e.g. by surface crack testing (penetration crack testing PT
or ultrasonic crack testing UT) • Welding seams must by inspectable, e.g. ground flush (externally marked)• Pre-service inspections could be necessary• ...............
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150 years
Rules (2): Manufacturing, designAD 2000 rules S1/S2 e.g.• Design e.g. avoidance of highly stressed areas• Manufacturing e.g. avoidance of weld stress and weld imperfections• Material• Design with low surface roughness• Recurrent inspections at least after half of the calculated lifespan• ........
DIN EN 13445-3 e.g.• Design• Calculation of lifespan• Design of the welding seams• Recurrent inspections at least after 20% of the calculated lifespan• ..........
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150 years
Influence parameters on fatigue
LoadsΔp ΔT ΔF ΔM
Amplitude of tensions
Number of loads untilrupture
Wall thicknessnotch effect, e.g. welds,shape deviatione.g. peaking
Geometry
Δσ
Average tensionMaterial
Surface roughness
Base material/ weld
MediumTemperature
6
150 years
Damage mechanism
Incipient crack
Number ofload cycles
Crack depth
Crack formation Crack pro-pagation
wal
l thi
ckne
ss
rupture
„Endurance“Fracture
mechanicalanalysis
7
150 years
Fracture mechanial analysis
Inci
pien
tcra
ckNumber ofload cycles
Crack propagation
rupt
ure
„endurance“Fracture
mech. analysis
Estimation of restlifespan
Leakage beforerupture?
Determination ofinspection intervals
Wal
l thi
ckne
ss
8
Crack depth
Crack formation
150 years
Crack test methods:Penetrating crack test (PT)
Principle: Coloured or fluorizing liquid
penetrates into cracks, crevicesor pores making them visible
Typical test arrangementUsual application:
Surface crack test for non
magnetic materials
Pressure vessels: welding seams9
150 years
Crack test methods:magnetic crack test (MT)
Principle: Formation of a magnetic field into a
ferromagnetic material. Imperfections close tothe surface create leakage flux that can beproved by fluorizing magnetic powder
Typical test arrangement:Usual application:
Surface crack test for ferromagnetic
materials
Pressure vessels: welding seams
10
150 years
Crack test methods:Ultrasonic crack test (UT)
Principle: A highly frequent ultrasonic impulse will be
reflected by a boundary
Typical test arrangement:
Advantages: Approachability from one side is sufficient Detection of imperfections is possible (position, length) Prove of cracks and weld imperfections
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150 years
Ultrasonic crack testing (UT) automatically Weld seams ground flush, marked from the outside UT-pre-service inspection of the welds (P-Scan) is necessary Internal inspection according to BetrSichV by UT (P-Scan)
from outside onstream possible (inspection concept)
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150 years
Example: Sending pressure vessel forpneumatic conveying
filling depres-surisation
conveying
time
pres
sure
Time of one cycle
Pressure amplitude0 – ca. 4 bar
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150 yearsRecurrent inspectionsExample Sending pressure vessel forpneumatic conveying
Usual inspectionconcept: Internal inspection withcrack test methods fromthe inside at highlystressed areas (MT, PT) e.g. atblock flanges, transition from thecylindrical to the conicalpart, reinforcement sheets, welds, .......
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150 years
15
Pressure Swing Adsorber (PSA) gas purification process
H2 Co-CurrentDepressurisation
Counter-Current Depressurisation
Adsorption
Feed Gas
Offgas
RepressurisationPurge
Step 1 Step 2 Step 5Step 3 Step 4
Time
Pres
sure
150 years
16
Present inspection concept
Inspection intervals3 – 5 years
Requires opening the vessel
Internal inspectionInner and outer vessel surface MT
Degradation of adsorbent when contact with humid air
Exchange of adsorbentafter 3 -5 years
Durability of adsorbent8 -15 years
conflict
150 years
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General procedure
Define operating conditions
Identify highly stressed areas
Fracture mechanical analysesfor each highly stressed area
Check minimum detectable crack size Determine load cycles until leak/ rupture
Sensitivity analysis
Influence of deviations from assumptions Safety margins
Max. allowable time between two succeeding inspection intervals
150 years
18
New inspection concept
UT from outside less sensitive Small cracks not detectable
Assessment of crack propagation assuming initial cracks equal to the smallest detectable cracks
Inspection intervalsdepending on crack growth velocity
Internal inspectionOuter vessel surface MTInner vessel surface UT from outside
No exchange of adsorbent
150 years
Inspection concept pressure swing adsorber
Internal inspection including MT of all welding seams from the inside whenadsorbent will be changed (every 15 to 20 years)
Pressure test every 10 years as a gas pressure test
Inspection of all longitudial welding seams and all butt-welds by UT fromthe outside, determined inspection interval of 2,5 years
Inspection by sound emission testing less suitable because of movementof the adsorbent particles
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150 years
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Summary
Main damage mechanism under cyclic stress: crack formation Indications to inspection intervals from technical regulations Support of the internal inspection by nondestructive crack testing
e.g. PT, MT, UT Conduction of inspection interval for inspection concept necessary Inspection concept for pressure vessels under cyclic stress is
possible
150 years
150 years
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