Robert Taylor
Mechanical Systems Engineer - PC-21 / PC-9(M) / PC-7MkII at Pilatus Aircraft Ltd- Claim this Profile
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English Native or bilingual proficiency
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Italian Full professional proficiency
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German Professional working proficiency
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French Limited working proficiency
Topline Score
Bio
Credentials
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Elements of Structures
Massachusetts Institute of Technology edXApr, 2013- Oct, 2024
Experience
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Pilatus Aircraft Ltd
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Switzerland
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Aviation and Aerospace Component Manufacturing
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700 & Above Employee
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Mechanical Systems Engineer - PC-21 / PC-9(M) / PC-7MkII
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May 2014 - Present
Design, development, qualification and certification of mechanical components & systems.Technical liaison and vendor management with external suppliers.Design reviews and tracking of technical requirements to FAR/EASA-CS Part 23 regulations.Aircraft ground testing and support to flight testing. Design, development, qualification and certification of mechanical components & systems.Technical liaison and vendor management with external suppliers.Design reviews and tracking of technical requirements to FAR/EASA-CS Part 23 regulations.Aircraft ground testing and support to flight testing.
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BOMBARDIER
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Canada
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Aviation and Aerospace Component Manufacturing
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700 & Above Employee
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Design Engineer – Learjet 85 / Global 7000
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Jul 2010 - Aug 2012
Innovative conceptual design for Fuel System installation to meet FAR25 requirements for lightningstrike and composite structures - including Fuel Vent, Gauging and Inerting sub-systems. Innovative conceptual design for Fuel System installation to meet FAR25 requirements for lightningstrike and composite structures - including Fuel Vent, Gauging and Inerting sub-systems.
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Liebherr Group
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Germany
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Industrial Machinery Manufacturing
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700 & Above Employee
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Mechanical Engineer – AIRBUS A350 Nose Landing Gear
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Apr 2009 - Jul 2010
Design of the major structural forgings for the NLG Drag Brace Assembly and associated extension/retraction mechanisms. Development of high tolerance bespoke hydraulic valves. Design of the major structural forgings for the NLG Drag Brace Assembly and associated extension/retraction mechanisms. Development of high tolerance bespoke hydraulic valves.
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Mechanical Systems Engineer – Commercial Aircraft Division, Gulfstream G250
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Jan 2007 - Feb 2009
Total concept development for all center fuselage large- and small-bore system installations includingEnvironmental Control Systems (ECS), Water / Waste, Hydraulics and Fuel. Total concept development for all center fuselage large- and small-bore system installations includingEnvironmental Control Systems (ECS), Water / Waste, Hydraulics and Fuel.
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Airbus
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France
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Aviation and Aerospace Component Manufacturing
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700 & Above Employee
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Design Engineer – AIRBUS A400M
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Feb 2005 - Dec 2006
Conceptual design through to manufacture of large-bore ECS and Fire Extinguishing System installations including all associated fabricated secondary structure. Conceptual design through to manufacture of large-bore ECS and Fire Extinguishing System installations including all associated fabricated secondary structure.
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BAE Systems
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United Kingdom
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Defense and Space Manufacturing
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700 & Above Employee
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Senior Design Engineer – Eurofighter Typhoon
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1998 - 2004
Design representative and focal point for all design and production issues at Alenia Aeronautica Final Assembly and Flight line. “Hands-on” implementation of Design Change through Manufacturing Change Authorities and by Concession. (Concession Signatory on Eurofighter project). Design representative and focal point for all design and production issues at Alenia Aeronautica Final Assembly and Flight line. “Hands-on” implementation of Design Change through Manufacturing Change Authorities and by Concession. (Concession Signatory on Eurofighter project).
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Education
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Cranfield University
MSc Astronautics & Space Engineering, Engineering -
Bournemouth University
BEng Engineering Design, Mechanical Engineering