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Conceptual Design Analysis of Medium Size Wings Type Surveillance UAV

14 Pages3297 Words447 Views
   

Central Queensland University

   

Systems Science and Engineering (COIT20275)

   

Added on  2020-03-02

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COIT20275 - The main aim of this report is to analyze the conceptual design of the medium sized wings type surveillance UAV. To achieve this aim two important sessions are provided such as aerodynamic computational analysis and the structural load analysis. In this analysis, some existing research work is carried out by analyzing the required materials and with appropriate methodologies.

Conceptual Design Analysis of Medium Size Wings Type Surveillance UAV

   

Central Queensland University

   

Systems Science and Engineering (COIT20275)

   Added on 2020-03-02

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System Science And Engineering
Conceptual Design Analysis of Medium Size Wings Type Surveillance UAV_1
AbstractThe UAV (Unmanned Aerial Vehicles) has many applications in the field of civil and special operations in military. These vehicles are applied especially in the dull, dirty and dangerous mission. According to the performance rate, cost of the maintenance, design and efficiency is decided. The main aim of this report is to analyze the conceptual design of the medium sized wings type surveillance UAV. To achieve this aim two important sessions are provided such as aerodynamic computational analysis and the structural load analysis. In this analysis, some existing research work is carried out by analyzing the required materials and with appropriate methodologies. The theoretical research on aerodynamics, design methodologies of the aircraft structure is studied and the results are compared with the historical wing design trends. In the preliminary design, the requirements of load and design lift are calculated. The advantages and the disadvantages of the wing design are discussed in detail.
Conceptual Design Analysis of Medium Size Wings Type Surveillance UAV_2
Table of ContentsAbstract......................................................................................................................................................11.Introduction.......................................................................................................................................32.Needs definition.................................................................................................................................33.Conceptual design..............................................................................................................................43.1Problem Definition.....................................................................................................................43.2System Requirement..................................................................................................................43.3Preliminary System Design.......................................................................................................53.4Detailed system design development........................................................................................54.Analysis..............................................................................................................................................75.Structural Analysis............................................................................................................................96.Recommendation.............................................................................................................................107.Conclusion........................................................................................................................................10References................................................................................................................................................11
Conceptual Design Analysis of Medium Size Wings Type Surveillance UAV_3
1.Introduction UAV is an aerial vehicle which takes the pivotal point in certain independent operations.It has been in the aeronautical area for last few decades. The system should be designed to liftthe vehicles to fly, automatically. The conceptual design of the wing deals mainly with the shapeof the wing and relevant characteristics. The main objective of this report is to provide theconceptual design, parameters of the wing, the design, and structure, characteristics ofaerodynamic, load responses, characteristics of the fluid flow and the basic idea of construction.This report helps in focusing on the convergence for the appropriate design for the requirementof the given mission. To enhance the outcome, two unique perspectives of design will beapproached. The needs definition and the conceptual design will be investigated. Further, theproblem definition, the system requirement, the preliminary system design will be studied. Thedetailed system design will be analyzed and discussed. Finally, appropriate recommendationswill be provided.2.Needs Definition 1)The Unmanned Aerial Vehicles are used in the maintenance, inspection andsurveillance work. It is used with the enhanced performance and reliability accordingto the company needs. According to the complexity of the operation and its need,there are many types of aircrafts that are used. 2)If we want to cover the long distances, the fixed wing are more resistant to gatherinformation. So, to collect data from very long distances, the multi-copter were used.There are various types of aircraft wing used such as, elliptic and rectangular wings. 3)Based on the needs of customer, the drones need to be designed with well-equippedthermal cameras, video equipment with high definition and sensors.4)To collect accurate data without any conflicts and disrupting, the droning tool needsto be designed. The traditional droning aircraft wings are not suitable for gatheringinformation in very dangerous places and the employees need to be kept in the safeplace. 5)To overcome this issue, the optimized design is required. The tool needs to conduct adetailed installation to inspect in very hard access sites. To reduce the work related
Conceptual Design Analysis of Medium Size Wings Type Surveillance UAV_4

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