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O WINGIT WORKS
Wingit Works is a Czech engineering company founded in 2018 by a team of engineers with years of experience in aircraft development, with the goal of actively contributing to the advancement of the fascinating field of aviation.
TECHNOLOGY, PRECISION
AND DEVELOPMENT
Aircraft development, experience, knowledge, enthusiasm, consistency, cooperation.
WHAT WE HAVE BEHIND US
We have collaborated on the development and certification of a wide range of aerospace projects – from unmanned vehicles and experimental VTOL demonstrators to commercial aircraft for leading global manufacturers. Our work has included structural analyses of primary and secondary structures, aircraft interior design, evaluation of ground and flight tests, and processing of telemetry data. We have contributed to projects for Airbus, Boeing, and Czech manufacturers, as well as supported military and specialized applications, including the Mi-17 helicopter and the PRIMOCO ONE 150M program.
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Supported PRIMOCO UAV in obtaining STANAG certification for the unmanned aircraft PRIMOCO ONE 150M.
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Structural analyses of interior monuments of commercial aircraft – Airbus A320 family, A330, A350 and Boeing B777, B787 (Galley, Stowage, Crew-rest, FWD/AFT Complex, Class Dividers).
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Design and structural calculations of VIP kit components for the Mi-17 helicopter of the Czech Army.
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Sizing and structural verification of the VTOL demonstrator aircraft Zuri.
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Definition and evaluation of structural tests for primary and secondary aerospace structures.
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Definition and evaluation of flight tests, including telemetry data processing for unmanned aircraft.
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Structural static calculations of primary structure assemblies for the L-410NG aircraft.
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Structural static calculations of primary structure assemblies for the L-39NG aircraft.
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Structural analysis and optimization of the composite fuselage of the UL-39 ultralight aircraft.
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Development and construction of experimental unmanned vehicles for international student competitions.
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Structural static calculations of fixed leading-edge wing components for Bombardier C-Series (Airbus A220) aircraft.
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Structural static and fatigue calculations of various parts of primary and secondary metal and composite structures of Airbus aircraft: A380, A400M, A330, A350 XWB, A319/A320 NEO.
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Structural static calculations of primary and secondary parts of the Aero-270 aircraft.
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Aerodynamic calculations of the Aero-270 aircraft.