henk van capelle

Checking of stress reports of parts of Saab Gripen E fighter.

* Dimensioning and design stress analysis for Airbus A380-800 Freighter wing fixed leading edge structure, such as slat track support ribs. * Design stress analysis on metal structure/system parts of Boeing 787 large cargo door. * Conceptional design stress and FEM analysis on wing of Airbus A350XWB aircraft (detached to Filton, UK). * Checking of Airbus A400M crew door mechanical system stress reports. * Finite element modelling of Saab Gripen NG fighter structures. * Dimensioning and design stress analysis for Saab Gripen NG structure (e.g. fuselage frame and landing gear attachment structure). * Checking and approving of Gripen NG stress reports. Stress signatory for Gripen NG production drawings (CATIA Models).

Dimensioning and design stress analysis for Airbus A380-800 wing fixed leading edge structure, such as slat track support ribs, de-icing system support ribs and intermediate ribs.

Finite element modelling and analysis of aileron of Nimrod MRA.4 maritime patrol aircraft. Design stress analysis of hinge support brackets and actuator support brackets for aileron and flaps of Nimrod MRA.4.

Stress support for production and fleet sustaining of 757 and 737 door structures. Dimensioning and design and certification stress analysis for Boeing 737 automatic overwing exit mechanisms.

Static stress and fatigue and damage tolerance analyses of Fokker 50 fuselage parts Design, dimensioning and stress analysis of interior parts and military systems and their attachments for Fokker 50 and Fokker 100. Design of and stress and fatigue analysis of structural repairs on aircraft. Design stress analysis of tail surfaces and parts of them for Gulfstream V corporate jet. Finite element modelling and analysis of stabilizer of the Gulfstream V. Coordination of stress certification reporting for Gulfstream V and liaison of subcontracted reporting in the UK.

Stress engineer on the tail surfaces of the Gulfstream G650. Detail static stress, fatigue and damage tolerance analyses on metal parts in the horizontal stabilizer, such as ribs, hinges and attachments. This includes making and checking detail FEM analyses (Patran, Nastran) and writing and checking of stress reports.

Aircraft engineering, specialisation aircraft structures. Activities and Societies: Sipke Wynia