Skyranger Dissertation Essay

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Aviation Engineering with Pilot Studies (BEng) School of Engineering and Design Analysis and Improvement of the SkyRanger’s Fuselage By Edward Johns 0800884 Tutor: Dr Ray Kirby ME3309 ME3309 Major Individual Project Student Number: 0800884 0800884 SkyRanger Dissertation Supervisor: Dr Ray Kirby Title: Research and Analysis into the SkyRanger structure, weight limitations and sizing’s to design a more efficient, aesthetically pleasing fuselage to increase sales potential and performance. Abstract: The SkyRanger is a very popular aircraft on the current micro light market. Its desirable performance and ability to function at high and low speeds mean that sales are ever increasing. For one of the most modern three-axis aircraft available, the fuselage has a very dated design that has the potential to be redesigned into a more appealing, aesthetically pleasing product. The weight of the fuselage is currently 130kg uncovered, taking up 28.8% of the final weight, which can be reduced. Objectives: Through a series of stress and strain analysis of the fuselage skeleton, I will determine if the SkyRanger has been overdesigned for its purpose as a relatively low speed aircraft. With the data and research into safety regulations for the structure, I will attempt to redesign the aluminium frame, within reason. Investigation into moments about the aircraft will determine if the rear weight may be reduced, and if so I could possibly increase sale appeal. I will try to ensure that any changes are practical and don’t result in the kit price increasing anymore than 10%. Conclusion: To improve on the current design, within reason, by researching into available materials and required sizing’s of the structure to ensure the aircraft can perform safely in a range of conditions by not significantly increasing the price. 2 ME3309 0800884 SkyRanger

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