Project History2018-09-12T11:22:40+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 drawings. 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