Aircraft Design, Aircraft Systems Technical University of ...
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Bachelor’s/Semester/Master’s Thesis Area: Aircraft Design, Aircraft Systems Redesign of the wiring system of the FLEXOP demon- strator Aircraft Technical University of Munich Department of Aerospace and Geodesy Institute for Aircraft Design Description At our Institute, we are responsible for the operation and maintenance of the FLEXOP technological demon- strator aircraft. Currently, we are operating one flight- ready aircraft. During final integration and successful flight tests, we were collected a lot of experience and ideas of a pos- sible redesign for the electrical system of the aircraft to make it safer and easier to operate. Building these ideas into the current working fuselage is not possible, due to current operation and space requirements. The goal of this thesis is to create a detailed design and prototype of the demonstrator payload area, which includes improved functionality compared to currently existing one. Proposed design changes are an electric switch board, improved power distribution system and BUS based communication system for actuators. The payload area prototype will be build into an electric mock-up system, where step-by-step system integra- tion detailed system testing is possible. The final design will be used to build a second fuselage. The student can participate in the ca- bling/building process in future work. Student Profile The student should be interested in the field of air- craft systems. The student should have some experi- ence with electrical schematic design and 3D mechan- ical design tools. The student should be able to work and learn independently. Intrinsic motivation for pre- cise and clean work is an advantage. Final Documen- tation is expected in L A T E X. Scope of Work WP1: Mapping the current wiring system of the demonstrator WP2: Design new layout with additional features WP3: 1:1 scaled payload area prototype building WP4: Integration and testing of proposed design WP5: Documentation Regular consultation and evaluation of the current pro- cess with the supervisor is expected. All the required hardware will be provided. Literature [1] S.Oberschwendtner: Redesign of FastTOL UAV Cable Harness Implementing Electromagnetic Compatibility Guidelines for Small to Medium Size Unmanned Aerial Vehicles Time Frame The thesis can be started any time. Duration is about 6 months. Supervision D´ aniel Teubl, Msc. Room: MW 3642 (089) 289 – 15984 [email protected]
Transcript of Aircraft Design, Aircraft Systems Technical University of ...
Bachelor’s/Semester/Master’s Thesis
Area:Aircraft Design, Aircraft Systems
Redesign of the wiring system of the FLEXOP demon-strator Aircraft
Technical University of Munich
Department of Aerospace and GeodesyInstitute for Aircraft Design
Description
At our Institute, we are responsible for the operationand maintenance of the FLEXOP technological demon-strator aircraft. Currently, we are operating one flight-ready aircraft.
During final integration and successful flight tests,we were collected a lot of experience and ideas of a pos-sible redesign for the electrical system of the aircraftto make it safer and easier to operate. Building theseideas into the current working fuselage is not possible,due to current operation and space requirements.
The goal of this thesis is to create a detailed designand prototype of the demonstrator payload area, whichincludes improved functionality compared to currentlyexisting one. Proposed design changes are an electricswitch board, improved power distribution system andBUS based communication system for actuators. Thepayload area prototype will be build into an electricmock-up system, where step-by-step system integra-tion detailed system testing is possible.
The final design will be used to build a secondfuselage. The student can participate in the ca-bling/building process in future work.
Student Profile
The student should be interested in the field of air-craft systems. The student should have some experi-ence with electrical schematic design and 3D mechan-ical design tools. The student should be able to workand learn independently. Intrinsic motivation for pre-cise and clean work is an advantage. Final Documen-tation is expected in LATEX.
Scope of Work
WP1: Mapping the current wiring system of thedemonstrator
WP2: Design new layout with additional featuresWP3: 1:1 scaled payload area prototype buildingWP4: Integration and testing of proposed designWP5: Documentation
Regular consultation and evaluation of the current pro-cess with the supervisor is expected. All the requiredhardware will be provided.
Literature
[1] S.Oberschwendtner: Redesign of FastTOL UAVCable Harness Implementing ElectromagneticCompatibility Guidelines for Small to Medium SizeUnmanned Aerial Vehicles
Time Frame
The thesis can be started any time. Duration is about6 months.
Supervision
Daniel Teubl, Msc.Room: MW 3642Ó (089) 289 – 15984R [email protected]
