National Repository of Grey Literature 3 records found  Search took 0.01 seconds. 
Numerical modelling of the Formula student powertrain
Krmíček, Antonín ; Ušiak, Michal (referee) ; Šebela, Kamil (advisor)
This diploma thesis deals with system modelling of Formula Student powertrain unit. System models allow the interactions between the different parts of the powertrain to be tracked, allowing the components to be optimized for the desired drive cycle. A system model of the powertrain is built based on measured data or calculations of component parameters. This can predict limiting factors such as maximum available motor torque, component temperatures or battery discharge. The model is validated against runs on the test track. Furthermore, the model is modified to consider the changes expected in the next generation of the vehicle. It is assumed that the model will be used in the future not only for the design and optimization of powertrain components, but also for lap time simulations as part of a virtual vehicle model.
Rebuilding of VUT 051 RAY into twin-engine conception
Jílek, Jan ; Mališ, Michal (referee) ; Píštěk, Antonín (advisor)
The master’s thesis is dealt with the design of rebuilding of VUT 051 RAY which is equipped electric powerplant to twin-engine conception named VUT 051 RAY-DUO. In the thesis was verified the range of centre of gravity position of VUT 051 RAY-DUO then powerplant in ducted fan configuration was designed, performances of the airplane were appointed and controllability during fail one of the engines was analysed. The design of new powerplant was verified by strength analysis and then costing calculation was established.
Rebuilding of VUT 051 RAY into twin-engine conception
Jílek, Jan ; Mališ, Michal (referee) ; Píštěk, Antonín (advisor)
The master’s thesis is dealt with the design of rebuilding of VUT 051 RAY which is equipped electric powerplant to twin-engine conception named VUT 051 RAY-DUO. In the thesis was verified the range of centre of gravity position of VUT 051 RAY-DUO then powerplant in ducted fan configuration was designed, performances of the airplane were appointed and controllability during fail one of the engines was analysed. The design of new powerplant was verified by strength analysis and then costing calculation was established.

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