Project History 2018-05-08T15:35:46+00:00

Project History

Space

A350

• Design and Analysis of ‘confidential’ rocket upper stage Payload Fairings, Inter-Stage Adapter and Aft-Stub Adapter
structure, systems (electrical/pyro/bonding).
• Radarsat RX receiver antenna (RX).
• Ariane 5 Launcher – Payload Fairing Sub-System.
• Ariane 5 ESC-A line interface analysis.
• Ariane 5 analysis test verification of CONE-3936 Payload structure.
• Ariane 5 ME Upper Stage, Equipped Lines: CdCF (requirements document), static analyses.
• Ariane 5 ME Upper Stage, Engine Thrust Frame: FEM, design trade-offs, definition of loading specifications for
subcomponents.
• Ariane 5 ESC-A Upper Stage, Vehicle Equipment Bay: model update, static analyses.
• Ariane 5 ESC-A Upper Stage, Inter-Stage Skirt: static analyses.

Aircraft

A350

• Dynamic and static stress analysis of A350 Composite belly fairing from Plateau Pre sizing, to Assembly and detailed FEM
analysis to detailed stress reports.
• Design and analysis of A350 Flap Track Fairings and Support Structure for SAAB – Linkoping.
• Evaluation of A350 CFRP Wing Design Concept.
• A350 XWB-900 Spoiler, Aileron, Droop Panel, Flap Support structure, Fairing Integration, Kinematical Elements design
concepts.
• A350-900 High Lift Conformance Verification.
• A350-900 Installation drwgs. Inbd/Outbd flap, Leading Edge devices, Flight controls/Flap Support Structure.
• Design of A350 Composite belly fairing from plateau phase pre sizing, to assembly and detail design.
• Dynamic and static stress analysis of A350 Composite belly fairing from Plateau Pre sizing, to Assembly and detailed FEM
analysis to detailed stress reports.
• Concept design and stress analysis of A350 CFRP Winglet.
• A320 NEO Composite Multi Flap Spar (CMF) design Principles and Maturity A.
• A320 Outer Flap Load introduction and test requests for CFRP Multi Spar Flap.
• A400M Composite Wing Covers manufacturing recurring cost reduction through composite structure redesign.
• Design and Stress Analysis of A400M Composite Wing Covers with up to 60 Engineers.
• Design/Stress of A400M Root Joint machined fittings.
• A400M Composite Wing Cover Concessions.
• Design/Stress Analysis of A380 PAX composite flaps.
• Design/Stress Analysis of A380 Freighter CFRP flaps.
• Atlas and Vulcan Rockets upper stage payload fairings, inter-stage and payload fairing adaptors.
• Development of Pilatus PC-24 Business Jet.
• Aircraft interiors