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Cascade Engineering

DEPENDABLE ENGINEERING Leading to CERTIFIED SOLUTIONS

Cascade Engineering takes the stress out of complex and critical structural engineering challenges. Our in-house team works alongside your project team to bring design solutions, analysis and optimisation to projects, driving them to successful certification, often realising time and cost-savings.

Over fifteen years we’ve worked on flagship programmes such as the Airbus A350XWB and A320neo, and supported strategic partners such as GE Aviation and ASSystem/Expleo to deliver certification on 100% of our projects, often finding solutions and savings which brought projects back to budget and deadline. More recently, we’ve helped clients such as Pilatus to prove airframe concepts and certify the PC-24, and we are long-standing team partners with clients such as QinetiQ, MES/Gattaca and Folland, bringing in resources and providing solutions when required.

We take projects, either modifications or new designs, from concept, through detailed design, analysis and optimisation on to final certification.

Contact Details

AddressThe Meads Business Centre, Kingsmead, Farnborough, GU14 7SR, U.K.
Telephone+44 1252 594121
Facsimile
Emailinfo@cascade-engineering.co.uk
Webwww.cascade-engineering.co.uk
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Client aircraft programs

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 XWB 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

Connections

Association memberships Farnborough Aerospace Consortium - U.K.

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