Stress Engineer
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- 22559 Hamburg
- Europa
- cs | en | de
- 31.10.2014
Kurzvorstellung
Qualifikationen
Projekt‐ & Berufserfahrung
10/2012 – 12/2012
Tätigkeitsbeschreibungworked onsite of Airbus Toulouse on A350–1000 Plateau – participation on the skin and stringer optimization performing CSPS and LDC ISAMI GFEM linked models analyses of complete Section 18
2/2012 – 9/2012
Tätigkeitsbeschreibungworked onsite Airbus Bremen on stress analyses of A400M Section 15 – checking certification reports, writing chapters of certification reports defining the method of calculation, ISSY analyses of riveted frame joints.
5/2010 – 11/2011
Tätigkeitsbeschreibung
worked onsite Airbus Hamburg on stress analyses of A350 Section 18 upper and lower shell – ISAMI analyses of frame and clips, shear ties, panel buckling of panels with cut outs, filled and open hole analyses. Patran/Nastran analyses of detailed FEM.
worked on site of Airbus Hamburg on A350 Section 18 upper shell – created the presentation of all results.
worked on site of Airbus Hamburg on A350 - checking the quality and correctness of FE models (delivered by PAG to Airbus) of surrounding structure of Bulk Cargo Door and Cargo Door of Section 18
9/2005 – 4/2010
Tätigkeitsbeschreibung
worked onsite Airbus Hamburg in A380 Section 13 stress department on following topics:
- cooperation on analysis of bonded window frames of Section 13/15FUU and 18 of A380 MSN105.
- analysis of Belly Fairing Brackets of Sections 13 and 18 of A380-800 MSN1, MSN10, MSN23 and MSN105. Hand calculations (HSB) used for analyses of simple brackets and Patran/Nastran analyses (nonlinear) used for more complex brackets.
- certification report of window belt area of Section 13/15FUU and 18 of A380 MSN23.
- checking and managing the creation of certification report of A380 MSN23, Section 13, upper shell. Report was prepared by ABEC
worked on project A380-800 Assessment of Window Belt Stress Sizing. Comparison of the critical load cases identified by Global FE model analysis (coarse mesh) and load cases identified by the fine FE model using ISSY (PMOD and GMOD) and Patran and Nastran
worked on project A380-800 Assessment of Window Belt Stress Sizing. Comparison of the critical load cases identified by Global FE model analysis (coarse mesh) and load cases identified by the fine FE model using ISSY (PMOD and GMOD) and Patran and Nastran.
worked on site Airbus Bremen
performed static strength analysis of structural details of Airbus A380F Section 13 Upper Shell (Cargo Door Surroundings)
5/2002 – 8/2005
Tätigkeitsbeschreibungperformed static strength analysis of Airbus A380-800 bulk cargo door. Responsible for all structural calculations, for creating and managing FEM model of the door and for certification reports.
11/2000 – 4/2002
Tätigkeitsbeschreibung
accomplished the strength analysis of manifolds of saw engines (using FEM program Mentat/Marc).
dynamic response analysis of crankshafts of combustion engines (using Pro/ENGINEER and Pro/MECHANICA)
11/1998 – 10/2002
Tätigkeitsbeschreibungstrength analysis and certification of baggage compartment replaceable bulkhead made from the honeycomb sandwich of LET L-420 and the strength analysis of Aires LM-200 wing (using MSC Patran/Nastran).
Ausbildung
Brno, Czech Republic
Weitere Kenntnisse
Persönliche Daten
- Englisch (Gut)
- Deutsch (Grundkenntnisse)
- Tschechisch (Muttersprache)
- Europäische Union
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