Entwicklung von
Flugzeugfahrwerks-
systemen
Airbus Bristol, UK
- A321 neo XLR Landing Gear System Concept studies for MLG Main Fitting and Uplock
Airbus Defense & Space Manching
- Jet Main Landing Gear Concept Development, Analysis and Optimization
DIEHL Aircabin, Laupheim
- Cabin Modules, structural analysis on, crew rest compartments, and air ducting
Dornier Seawings GmbH, Oberpfaffenhofen
- Dornier Seastars Landing Gear, structural integration,stress analysis and optimization of attachment structures for the (GFRP laminate sizing etc.) according FAR requirements, check of LGS suppliers stress reports
- Dornier Seastars Bleed Air Duct, CFE‘s first flying hardware delivered with CoC & DDP Design, development, analysis, industrialization, manufacturing (with manufacturing partner: CoC, EASA Part 21G), qualification testing & documentation
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Seastar-Bleedair-Duct_VibTest
GOMOLZIG Aircraft Services GmbH, Schwelm
- Bell 407 Police Helicopter Operator Rack, design, development and analysis of an operator rack for two adjustable moitors and other electrical equipment
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Bell407 Operator Rack
Bell407 Operator Rack FEM-Plot
Kopter Group AG, Wetzikon, Schweiz
- SH09 skid landing gear analysis and optimization + several analyses and optimizations for stowage box, front- and rear ballast structure
- SH09 skid landing gear development of a crash loads routine, including elastic-plastic stiffness of gear and helicopeter structure, sizing and optimization of skid landing gear and interface brackets to A/C
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KG Skid Landing Gear
- SH09 main rotor gearbox analysis and documentation static &fatigue
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KG Main Gear Box FEA Plot
Liebherr Aerospace Lindenberg GmbH
Landing Gear Systems:
- Airbus A220/230 [Bombardier CSeries CS100/300] Landing Gear System: Stress Team Lead (team size ~20 FTE) focal point for customer, organization and education of stress engineers, capacity planning, development of analytical und numerical methods of analysis, from first concept phase until drawing release and qualification test campaign, complete responsibility of landing gear system static and fatigue strength
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Bombardier CSeries / Airbus A220 Nose- and Main Landing Gear
- Airbus A220/230 [Bombardier CSeries CS100/300] Landing Gear System: CS100 & CS300 Development & Weightreduction Campaign, Design & Analysis, very successful massive reduction of structures weight which was allowing requalification by written evidence, avoiding new strength test campaign
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CSeries Main Landing Gear FEM Plot Stress
- A350 Nose Landing Gear System FEM Analysis, Development and Optimization
- A350 Nose Landing Gear System Hydraulic Fatigue Test Spectrum definition (RA, UA, Valve-Blocks)
- AW139 Landing Gear System Fatigue Analysis for 7 ton Version
- AW139 Landing Gear System FEM Analysis & Design Optimization for 7 ton Version
- ARJ21 Landing Gear System Doorlinkage FEM Analysis & Fatigue Analysis & Fatigue Test Spectrum definition
- C919 Landing Gear System Doorlinkage Analysis & Development
- C919 Landing Gear System Complete Assembly FEM Random Vibration Fatigue Analysis & Frequency Response Analysis
- C919 Landing Gear System Vibration Test Rig Analysis & Development
- C919 Landing Gear System Fuse Pins Pintle Pin and Side Brace Pin FEM Analysis and Fatigue Test Spectrum development
- C919 Landing Gear System Test Rig Development Design & Analysis, Strength + Fatigue combined Rig
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C919-Test-Rig-CAD-Model
- C919 Landing Gear Iron Bird NLG and MLG, Development Design & Analysis, Strength + Fatigue for ext./retr., Drawings and Manufacturing with our partner
- C919 Landing Gear RAG for manufacturing roll around NLG and MLG, Development Design & Analysis, Strength, Drawings and Manufacturing with our partner
- ERJ170, ERJ190, M346, Landing Gear Systems in-service issues evaluation, analysis for concessions, load increase, …
Highlift Systems:
- EJet Highlift System Station Gearboxes and Rotary Actuators FEM Analysis & Structural Optimization
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EJet Geared Rotary Actuator FEM Model Mesh
EJet Geared Rotary Actuator FEM Model Plot
- A380, A350, RRJ Highlift Systems Geared Rotary Actuators FEM Analysis& Structural Optimization
- A350 Highlift System Design to Cost, Product Improvementconcept realization studies, Design & Analysis
HEGGEMANN AG, Büren (Paderborn)
- CS23 Landing Gear NLG & MLG development - concept development, design, loads & performance, stress, drawings, design to cost, weight and manufacturing, qualification support and documents, certification support and documents
- CS25 Landing Gear System NLG & MLG & hydraulics components development - concept development, design, loads & performance, stress, drawings, design to cost, weight and manufacturing, qualification support and documents, certification support and documents
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SAFRAN LANDING SYSTEMS GLO, UK
- A350 Main Landing Gear, complete fatigue analysis for 275T and 280T several loads loops
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A350XWB Aircraft – Landing Gear extended
- A350 Main Landing Gear, Torque Links weight reduction analysis
- A320 Main Landing Gear, Single Aisle Repair concessions signatory approval for design and stress
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