Airbus A320 |
Analysis |
Computer-aided Analysis: Conducted design & certification static and F&DT analysis for numerous wing components (A320 - NEO and Sharklet; A321); Technical/Eng/Scientific Studies: Conducted design exceedance and optimisation studies for numerous wing components (A321; A320 - NEO and Sharklet); Stress Analysis: Conducted design & certification static and F&DT analysis for numerous wing components (A320 - NEO and Sharklet; A321) |
Airbus A350 |
Analysis |
Composite Design Consultants: Design, analysis and development of primary structural carbon-fibre sandwich panels (A350-900; A350-1000); Computer-aided Analysis: Provided advice and interpretation on use of OEM analysis tool-sets to fixed trailing edge supply-chain (A350-900; A350-1000); Computer-aided Simulation: Created entire fixed trailing edge FE models and delivered fully correlated load cases into supply-chain (A350-900; A350-1000); Engineering Design Services: Led teams providing sizing, development, optimisation, integration, instruction throughout fixed trailing edge development (A350-900; A350-1000); Technical/Eng/Scientific Studies: Provided sizing, development, optimisation, integration, instruction throughout fixed trailing edge development (A350-900; A350-1000); Stress Analysis: Supported the entire Wing Fixed Trailing Edge development programme from A-Scheme, through to completion of certification (A350-900; A350-1000) |
Airbus A380 |
Analysis |
Technical/Eng/Scientific Studies: Conducted modification static and F&DT analysis of numerous wing fixed trailing edge components (A380-800); Stress Analysis: Conducted certification F&DT analysis and approval of numerous wing fixed trailing edge components (A380-800) |
Airbus A400M |
Analysis |
Computer-aided Analysis: Created and used wing FE models for the flap track attachment fittings (A400M Atlas); Engineering Design Services: Led teams to develop design solutions for the flap track attachment fittings (A400M Atlas); Stress Analysis: Conducted static & F&DT design & certification analysis for the flap track attachment fittings (A400M Atlas) |
Avicopter AC311 |
Analysis |
Computer-aided Simulation: Local FE Model of composite fairings for engine air filter; Stress Analysis: Certification static stress analysis and formal reports for composite fairings for engine air filter |
Avicopter AC313 |
Analysis |
Composite Design Consultants: Advised on manufacturing to retain strength and on a strength testing programme; Stress Analysis: Provided manufacturing support to allow alternative suppliers to produce components for engine air filter |
Boeing 737 |
Analysis |
Computer-aided Simulation: Created entire wing & fuselage stores pylons FE models and delivered fully correlated load cases (737-800 - P-8A Poseidon); Engineering Design Services: Led teams providing sizing, development, optimisation, integration, instruction throughout wing & fuselage stores pylons development (737-800 - P-8A Poseidon); Technical/Eng/Scientific Studies: Provided sizing, development, optimisation, integration, instruction throughout wing & fuselage stores pylons development (737-800 - P-8A Poseidon); Stress Analysis: Supported the entire wing & fuselage stores pylons development programme from concept, through to completion of certification (737-800 - P-8A Poseidon) |
Eurofighter Typhoon |
Analysis |
Computer-aided Simulation: Conducted dynamic computer simulation analysis for fin mounted antenna ; Technical/Eng/Scientific Studies: Correlated dynamic computer simulation with physical test data for fin mounted antenna |
HAL LUH |
Analysis |
Computer-aided Simulation: Local FE model of composite fairings for engine air filter; Stress Analysis: Certification static stress analysis and formal reports for composite fairings for engine air filter |
KAI LAH/LCH |
Analysis |
Computer-aided Simulation: Created and used FE models for the birdstrike analysis for the engine intake bypass door; Technical/Eng/Scientific Studies: Studies into simulated dynamic/impact material failure scenarios compared to physical test data; Stress Analysis: Conducted birdstrike analysis for the engine intake bypass door |
Leonardo AW101 |
Analysis |
Stress Analysis: Conducted certification static stress analysis and reporting for the SAR racks |
MIL Mi-17/171 |
Analysis |
Computer-aided Simulation: Created and used FE models for the entire engine intake filter; Technical/Eng/Scientific Studies: Provided sizing, development, optimisation, instruction throughout engine intake filter development; Stress Analysis: Provided the entire structural design & analysis effort for the engine intake filter development |
Pilatus PC-12 |
Analysis |
Computer-aided Simulation: Developed and used entire aircraft FE models and delivered fully correlated load cases; Engineering Design Services: Led teams providing sizing, development, optimisation, integration, instruction throughout equipment bay development; Stress Analysis: Provided the entire structural design & analysis effort for the introduction of the forward fuselage equipment bay and the introduction of a radar, plus various other equipment |
Pilatus PC-24 |
Analysis |
Engineering Design Services: Provided sizing, development, optimisation, advice throughout rear fuselage and vertical tail development; Technical/Eng/Scientific Studies: Provided sizing, development, optimisation, advice throughout rear fuselage and vertical tail development; Stress Analysis: Conducted design, development & certification static stress analysis for the rear fuselage and vertical tail |