Propulsion Unit of a 3DOF Helicopter
Independent thesis Basic level (degree of Bachelor), 12 credits / 18 HE creditsStudent thesis
This Bachelor thesis is a part of a bachelor project which includes building, programming and controlling a 3DOF tandem helicopter. This particular report deals with the propulsion units, i.e. the motors and propellers of the helicopter. It covers the process of how to determine the most suitable propulsion units for the rig that eventually will enable it to run. To achieve this, different data have been processed. Torque and thrust are two important parameters that have been studied. The data have been acquired by different tests, e.g. thrust measurements from a thrust rig. Also more complex analysis such as Blade Element Theory and Actuator Disk Theory have been carried out in order to determine the behaviour of the propulsion units. Study data sheets and databases was also a part of the work. The result of this work was two equal propulsion units which were mounted in the helicopter. They proved to work satisfactory and provided wanted dynamics to the system.
Place, publisher, year, edition, pages
2015. , 44 p.
propulsion unit, helicopter, rig, dynamics, thrust rig, mechatronics, 3DOF, tandem helicopter, DC motor, brushless DC motor, brushed DC motor, APC, Maxon, propeller mount, tandem helicopter
IdentifiersURN: urn:nbn:se:liu:diva-120799ISRN: LIU-IEI-TEK-G–15/00854—SEOAI: oai:DiVA.org:liu-120799DiVA: diva2:848667
Subject / course
Fluid and Mechanical Engineering Systems
Martin, Hochwallner, PhD
Magnus, Sethson, Lecturer
ProjectsDesign & Implementation of a 3DOF Helicopter