Patrick Braun

A350: DTR for Development/Stress/Weight in accordance to AP1020.3. Patran/Hyperworks, Nastran, Optistruct, providing all required steps to develop CAD&FEM file, static pre-, post-preparation,static EASA&FAA justification of ATA21 components, Qualification Tests A350, Stress analysis metallic & composite materials, Approval of Design solutions, Concessions, Static Stress Reports, Similarity Statements, Engineering Judgements and so on...

A380, A400M: Analysis of A380 flap tracks 1-6, provide evidence of A400M vertical tail plane fittings 1, 2 and 5, FEM Analysis & Handcalculation in accordance to HSB, Fokker, ESDU for modifications

A300, A318-321, A330/340, A330 GMF, A380: Responsible for coordination of NC, BB, eTLB, TLB, DQN and Concessions for passenger doors and cargo doors of all Airbus programs, coordinator for St. Nazaire, Toulouse, Tanjin and Hamburg

A380: PDR and CDR assembly analysis in CATIA V5 DMU for proper installation of ATA 21, ATA 25, ATA 92 and ATA 53 parts.

A330/A340: Steering of design solutions for brackets and floor panels in TAKSY, VPM, CATIA V5 and ZAMIZ, positioning of parts in global and local aircraft coordinate system

Flight Mechanic for Inflight entertainment systems, Mock up and electrical components, testing, installation and verification

Education in heavy and line maintenance of several aircraft types (Airbus, Boeing, Bombardier, Fokker, Dornier), certifying staff in accordance to EASA 66 Category A

Aircraft Design and Lightweight structures

- structures - power plants - aerodynamics - aircraft design - FEM analysis - economics