Please use this identifier to cite or link to this item: https://scholarhub.balamand.edu.lb/handle/uob/3722
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dc.contributor.advisorRishmany, Jihaden_US
dc.contributor.authorMekkaoui, Ibrahimen_US
dc.contributor.authorKhazma, Mohamaden_US
dc.date.accessioned2020-12-23T14:38:02Z-
dc.date.available2020-12-23T14:38:02Z-
dc.date.issued2015-
dc.identifier.urihttps://scholarhub.balamand.edu.lb/handle/uob/3722-
dc.descriptionIncludes bibliographical references (p. 34-35).en_US
dc.descriptionSupervised by Dr. Jihad Rishmany.en_US
dc.description.abstractThe aim of this project is to satisfy the costumers demand of designing an efficient Quad-Copter capable of carrying a certain payload of a specified weight. This QuadCopter will be more durable and sustainable than the conventional designs. A wind turbine will be placed to charge the batteries, instead of using the electric connection. The goals to be met are, lightweight, simple fabrication, easy maintenance, as well as keeping cost low. A limited speed reached by the wind turbine is 105rpm. To produce 12 volts the generator must reach 3000rpm. To translate the speed of wind turbine to the required generator speed a ratio for a gearbox is developed. The charge and discharge rates were calculated and compared concluding that charging while grounded before flight is effective. After running simulations, finite element analysis results ensured the durability under stress. Frequency analysis results revealed the natural frequencies of the structure as well as its resistance to the frequency generated by the motor, which is 157Hz. CFD flow analysis indicated low drag on the body and turbine signifying low ambient forces produced under high winds on the system.en_US
dc.description.statementofresponsibilityby Ibrahim Mekkaoui, Mohamad Khazmaen_US
dc.format.extentix, 35 p. :ill., tables ;30 cmen_US
dc.language.isoengen_US
dc.rightsThis object is protected by copyright, and is made available here for research and educational purposes. Permission to reuse, publish, or reproduce the object beyond the personal and educational use exceptions must be obtained from the copyright holderen_US
dc.subject.lcshQuadrotor helicopters--Design and construcionen_US
dc.titleDesign and fabrication of an eco-friendly Multi-Copter prototypeen_US
dc.typeProjecten_US
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.contributor.facultyFaculty of Engineeringen_US
dc.contributor.institutionUniversity of Balamanden_US
dc.date.catalogued2015-06-09-
dc.description.degreeMS in Mechanical Engineeringen_US
dc.description.statusPublisheden_US
dc.identifier.ezproxyURLhttp://ezsecureaccess.balamand.edu.lb/login?url=http://olib.balamand.edu.lb/projects_and_theses/GP-Mec-134.pdfen_US
dc.identifier.OlibID161022-
dc.provenance.recordsourceOliben_US
Appears in Collections:UOB Theses and Projects
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