Ultra Aircraft Structural Analysis

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CHAPTER – 1 INTRODUCTION 1.What is the purpose of the ultralight aircraft structural analysis? 2.what is means by ultralight aircraft? Ultra light is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Sometime differentiate between weight-shift control and conventional 3-axis control aircraft with ailerons control, elevator control and rudder control , calling the former "micro light" and the latter "ultralight". During the past, mostly stimulated by the hang power gliding movement, many people sought affordable powered flight. As a result, many given definitions of lightweight, slow-flying aircraft that could be subject to minimum regulations. The resulting aircraft are commonly called "ultra light aircraft" or "micro lights",…show more content…
Temperature condition : Atmospheric temperature we have consideration. 3. Aircraft specification Take off weight: 450 kg Stalling speed: 80 km/h 1 prop 1 engine Cruse speed=103 km/ hr. Stall speed=56 km/ hr. for engine specification. (448 fixed pitch 40 hp. 30 kW.) Wing span=22.2ft, wing area125.2 sq. ft., bottom flat aerofoil , Wing load =23.6kg/sq 4. Increase in life span We are dealing with high quality of material. It is rain forced material. So atmospheric conditions are not effected & we also provide rigid mounting of aircraft with land to decrease vibrations at higher speed. 3. LITERATURE REVIEW In the research paper we are to decide the assembly detail and other parameter like shape and size of the structural. 1. The structural is made by the hollow pipe and light in weight more stiffness and strength. 2. Detail assembly of the wing are detail in A , B , C ,D A. Wing rib assembly B. Wing spare mounting. C. Wing compression struts D. Wing hinge with the controlling parts like aileron control 3. Detail assembly of the fuselage are detail A,B A. Front side assembly. B. Landing gear mounting. 4. Detail assembly of the rudder. A. Horizontal support B. Horizontal fin 5. Detail assembly of…show more content…
 Ss-301 is Equal to or exceeding that of Grade 304. Subject to pitting and crevice corrosion in warm chloride environments, and to stress corrosion cracking above about 50°C. 302HQ is considered resistant to potable water with up to about 200mg/L chlorides at ambient temperatures, reducing to about 150mg/L at 60°C. Consult Atlas Technical Assistance for specific environmental recommendations.  Ss-304 is Very good in a wide range of atmospheric environments and many corrosive media. Subject to pitting and crevice corrosion in warm chloride environments, and to stress corrosion cracking above about 60°C. Considered resistant to pitting corrosion in potable water with up to about 200mg/L chlorides at ambient temperatures, reducing to about 150mg/L at 60°C. Consult Atlas Technical Assistance for specific environmental recommendations. There is usually no difference in corrosion resistance between 304 and 304L. Application of the material.  Rail car structural components - often roll formed, brake pressed or stretch formed to profiles but also used flat. Airframe sections. Highway trailer components. Automotive wheel covers, wiper blade holders and clips. Toaster springs, stove element clips. Screen frames, curtain

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