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Design of fore part of fuselage and engine mounting of TL-4000 aircraft
Löffelmann, František ; Jebáček, Ivo (referee) ; Vaněk, František (advisor)
The thesis solves mounting of Continental IO-55ON to four-seat all composite aeroplane. Weight analysis of weights carried by engine mounting was done and loads of mounting and nose gear attached directly to mounting was computed according to CS-23 regulation. Mounting was designed based on affordable information about similar aeroplanes and it was sized due to Nastran/Patran system strength analysis. Further reinforcing of fire wall, engine covers and forms for their manufacture was suggested.

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