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C. Garion Aluminum bellows for C. Garion Aluminum bellows for

C. Garion Aluminum bellows for - PowerPoint Presentation

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C. Garion Aluminum bellows for - PPT Presentation

LHC experiments C Garion TEVSC Outline C Garion Material requirements amp choice Design EJMA and Manufacturing requirements Mechanical bellows properties Manufacturing process Tests ID: 1006419

manufacturing bellows forming temperature bellows manufacturing temperature forming diameter life atlas membrane amp stress aluminum fatigue strain tests properties

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1. C. GarionAluminum bellows for LHC experimentsC. Garion, TE/VSC

2. OutlineC. GarionMaterial requirements & choiceDesignEJMA and Manufacturing requirementsMechanical bellows propertiesManufacturing processTestsStatus and next stepsConclusion

3. C. GarionMaterialRequirements:Formability (high ductility)Weldability (also with 2219)Low Heat affected zoneAvailable in thin foilsGood mechanical properties at elevated temperatures (>180 C)5083 H111, 0.2 and 0.3mm thick, 200 mm widthWeld reliability

4. C. GarionDesignAlgorithm of optimization of bellows expansion joints (Based on EJMA)Minimise the objective function: inequality constraints: bellows convoluted length inner diameter outer diameter bellows maxi compression membrane stress membrane stress membrane & bending stress fatigue life column buckling in-plane squirm Atlas constraints (technical specification EDMS 429891):Lbmax = 100 mmDmin ~ 60 mmDmax = 80 mmStroke = -24/+8mmNf > 500 cycles

5. C. GarionDesignManufacturing requirementsPlastic strain during forming process Forming at elevated temperature required

6. C. GarionDesign13 convolutions, bellows length: ~96mm, Inner diameter: 60 mm, outer diameter: 80 mm

7. C. GarionDesignBellows properties – FE modelForce/displacement curveElastic-plastic buckling analysisPlastic and total strain fields+ Manson Coffin equation: Fatigue life estimationFE model

8. C. GarionBellows manufacturing process(courtesy of L. Prever Loiri, EN/MME)Aluminum foilRolled tube & longitudinal weld (EB)Welds of the end fittings (EB)Forming @242°C combining pressure and displacement loadingCut of the end fittingsCleaning with phosphor nitric acid [VSC/SCC] Optimization of the temperature distribution Automatic displacementLeak test after “bake out”

9. C. GarionBellows manufacturing processSome Pictures (EN/MME)Tubes equipped with the end fittingsTubes and pressure systemDie systemForming system

10. Tests (courtesy of H. Rambeau)C. GarionFatigue testsPrototypeSeries 1Series 2RT<N>=2300<N>=19503019150 C<N>=1000200 C1185250 C193All bellows with welding defectsCollapse of the convolutions @ 250 C

11. C. GarionStatus and next stepsATLAS (VA chamber): Bellows manufactured Fatigue life qualification done and will be continued Tests on NEG coating ongoingLHCb: Z=2800, same bellows as ATLAS VA, design of compensator to be redone UX85-2/3: design done (limitation by the sheet width) forming tooling being manufactured/assembled first tubes doneCMS (End cap pipe compensator): Under consideration

12. C. GarionConclusionDesign and manufacturing of aluminum bellows are mastered.Aluminum bellows are suitable and have been qualified for UHV applications.Bellows are qualified for a temperature of 200 C.Bellows for ATLAS VA chamber are ready for installation (after leak test).Manufacturing of the bellows for LHCb are in progress.

13. C. GarionRT150 C200 C250 CTensile curves0.3 mm, RD

14. C. GarionS-N curveFatigue of deep rolled AlMg4.5Mn (AA5083) in the temperature range 20–300 ◦C, P. Juijerm et al., Materials Science and Engineering A 379 (2004) 286–292