Principal requirements in repair of structures, inspection of the damage and accurate estimate of the type of repair required, important steps in repairing structural damage. If you continue browsing the site, you agree to … Such as aircraft aerodynamics; which indicates how smooth the aircraft flies thru the air (The Skelton of the aircraft greatly affects these aerodynamics and consist of frames and stringers.) Looks like you’ve clipped this slide to already. See our Privacy Policy and User Agreement for details. One of the requirements of an Aviation Structural Mechanic is to be familiar with the various terms related to aircraft construction. Basic Structure : Tire Markings < Conventional Radial Construction > Tire Terminology : 1. A history of aircraft structures from the early beginnings of wire-and-brace structures, to semi-monocoque and modern sandwich construction. The assignment involves studying the skeleton of your favorite aircraft or spacecraft to identify why certain structural elements were used by their designers. As of this date, Scribd will manage your SlideShare account and any content you may have on SlideShare, and Scribd's General Terms of Use and Privacy Policy will apply. Now customize the name of a clipboard to store your clips. True. 15 STRUCTURAL COMPONENTS The basic functions of an aircrafts structure: Transmit and resist the loads Provide an aerodynamic shape To protect passengers, payload, systems etc. Scribd will begin operating the SlideShare business on December 1, 2020 [Figure 2-5] The most popular types of fuselage structures used in today’s aircraft are the monocoque (French for “single shell”) and semimonocoque. Propeller Landing Gear Wing Left Aileron Fuselage Empennage Nacelle Right Aileron Wing Horizontal Stabilizer Vertical Stabilizer Rudder Elevator 4. 9. The term “stress” is often used interchangeably with the word “strain.” The degree of deformation of a material is strain. Slideshare uses cookies to improve functionality and performance, and to provide you with relevant advertising. See our User Agreement and Privacy Policy. AE332 Aircraft Structures II Course Instructor: Dr. PM Mohite 12 Functions of Skin or Cover 1. Fuselage structures can be of monocoque construction, or of semi-monocoque construction Monocoque Edit. C. Monocoque structure. The basic function of an aircraft’s structure are to transmit and resist the loads applied on aircraft so the structure can provide aerodynamic shape and protect the aircraft from environmental conditions encountered in flight. A. Fuselage B. Wings C. Empenage or Tail D. Landing Gear Aircraft Components 3. The fuselage is one of the major aircraft components with its long hollow tube that’s also known as the body of the airplane, which holds the passengers along with cargo. See our User Agreement and Privacy Policy. Fail-safe structures enable aircraft parts to be produced lighter. For detailed instructions regarding The airframe is the basic structure of an aircraft, design to withstand aerodynamic forces and stresses imposed. When repair of a damaged part is possible, first study the part carefully to fully understand its purpose or function. Test. See our Privacy Policy and User Agreement for details. BASIC STRUCTURAL ELEMENTS IN AIRCRAFT STRUCTURE 5 Figure 1.4 Curved panel under a state of constant shear stress. Terms in this set (9) ... What aircraft structure is designed to transmit engine loads, stresses, and vibrations to the aircraft structure? It develops shearing stresses which react to … An aircraft is a vehicle that is able to fly by gaining support from the air.It counters the force of gravity by using either static lift or by using the dynamic lift of an airfoil, or in a few cases the downward thrust from jet engines.Common examples of aircraft include airplanes, helicopters, airships (including blimps), gliders, paramotors and hot air balloons. The Our structure training is built on a firm basis that will enable the student to perceive: • knowledge about materials on modern transport aircraft and their application • design principles and their derivatives • categorization of different types of damage on aircraft structures • basic application of aircraft manuals .Aircraft science and manufacturing process 2. Diploma in Aircraft Structures and Repairs Course Code: ME3-A4-19 Course Duration: 12 Months Course Description (English) This MCAST Diploma is intended to train the learner for competences in Aircraft Structures and Repairs which are essential for structure repair mechanics. The aircraft design process is a loosely defined method used to balance many competing and demanding requirements to produce an aircraft that is strong, lightweight, economical and can carry an adequate payload while being sufficiently reliable to safely fly for the design life of the aircraft. Now customize the name of a clipboard to store your clips. STRUCTURAL STRESS LEARNING OBJECTIVE: Identify the five basic stresses acting on an aircraft. The strength of aircraft materials must be great enough to withstand maximum force of varying stresses. from environmental conditions encountered in flight. If you continue browsing the site, you agree to the use of cookies on this website. These factors determine the requirements to be met by any material used to construct or repair the aircraft. You can change your ad preferences anytime. provides the structural connection for the wings and tail assembly. Match. We use your LinkedIn profile and activity data to personalize ads and to show you more relevant ads. Full monocoque fuselages uses formers, frame assemblies and bulkheads to give shape to the fuselage. "As an undergraduate studying aerospace engineering, I have to say this blog is a great resource for gaining extra history and 1. The page is meant as a simple guide to understanding the basics of aeronautic structural design and the corresponding forces placed on different parts of the aircraft. The propeller or jet engine takes a large mass of air and accelerates it toward the rear of the aircraft. composite materials will constitute a greater percentage of an aircraft's structure, but metallic materials will cer-tainly continue to be used for many years. We use your LinkedIn profile and activity data to personalize ads and to show you more relevant ads. How Aircraft Structures are Made2 Aircraft structural design is a subset of structural design in general, including ships, land vehicles, bridges, towers, and buildings. The determination of such loads is called stress analysis. A. Damage tolerant structure. Basic aircraft structure 1. Structures are subject to one-way and oscillating stresses, the Write. AIRCRAFT CONSTRUCTION AND MATERIALS. Newton's law states; 'for every action, there is an equal and opposite reaction." Follow them closely. Stresses include the weight of fuel, crew, and payload; Although similar in concept, aircraft can be classified as fixed and rotary wing structures False. Apex strip: A triangular piece of stiff rubber which is fitted onto the bead core to taper the rigid bead into the flexible body plies in the sidewall. AIRCRAFT LIFE MONITORING There are 3 philosophical approaches to designing aircraft in order to ensure that they operate safely throughout their operational lives. Despite there being different types of fuselages, they all connect the major parts of an airplane together. This chapter serves as an introduction to the design, construction, inspection, and repair of basic airframe structures made from sheet metal. Stresses usually … Mickie_Mills. A. Aircraft Structures Definitions A Access panel - removable panel for inspection or maintenance Aft - near of in the direction of the rear of the aircraft Aerodynamics - the study of how the moving body (aircraft) interacts with air flowing around it, flies Aerodynamic centre - the point of application for additional aerodynamic loads 1. If you wish to opt out, please close your SlideShare account. Thrust is the force developed by the aircraft engines. The primary objective of aircraft repair is to restore damaged parts to their original condition. The basic functions of an aircraft's structure are to transmit and resist the applied loads and to provide an aerodynamic shape and protect passengers, payload, systems, and the likes from the environmental conditions encountered in flight. Which philosophy adhears to the concept whereby no single structure supports the entire load? Basic Structure. If you continue browsing the site, you agree to the use of cookies on this website. Aircraft Structure - An introduction to major airplane components. Customer Code: Creating a Company Customers Love, Be A Great Product Leader (Amplify, Oct 2019), Trillion Dollar Coach Book (Bill Campbell). .Aircraft science and If you wish to opt out, please close your SlideShare account. STUDY. Scribd will begin operating the SlideShare business on December 1, 2020 The basic aircraft structure serves multiple purposes. aircraft construction to work in an aviation rating. Slideshare uses cookies to improve functionality and performance, and to provide you with relevant advertising. APIdays Paris 2019 - Innovation @ scale, APIs as Digital Factories' New Machi... No public clipboards found for this slide. Clipping is a handy way to collect important slides you want to go back to later. An aircraft structure must be designed so that it accepts all of the stresses imposed upon it by the flight and ground loads without any permanent deformation. You can change your ad preferences anytime. It transmits the aerodynamic forces to the longitudinal and transverse supporting members by plate and membrane action 2. The FAA route to certification adopted by civil aircraft manufacturers is based on the well-known test pyramid for aircraft structures, as set out for composite aircraft in FAA AC 20-107B (2010), which foresees five levels of tests from material characterisation test specimens, through structural elements of increasing complexity up to full aircraft structures. Part 4: Loads and Stresses Covers the loads that act on the different aircraft parts, the paths these loads travel on through a structure, and how this affects design choices when designing wings and fuselages. This page shows the parts of an airplane and their functions. Every part of the aircraft must be planned to carry the load to be imposed upon it. A knowledge of the basic stresses on aircraft structures will help you understand why aircraft are built the way they are. Older types of aircraft design utilized an open truss structure constructed of wood, steel, or aluminum tubing. If you continue browsing the site, you agree to the use of cookies on this website. All structures must be designed with care because human life often depends on their performance. The sequence of assembly of the basic structure of the airplane (fuselage, wings and tail) will depend on the instructions included in the kit. Spell. The primary factors to consider in aircraft structures are strength, weight, and reliability. Learn more. Slideshare uses cookies to improve functionality and performance, and to provide you with relevant advertising. Gravity. This page is an overview of the structural requirements and solutions in the recent history of aircraft design. Airplanes come in many different shapes and sizes depending on the mission of the aircraft. manufacturing process. STRUCTURAL STRESS LEARNING OBJECTIVE: Identify the five basic stresses acting on an aircraft. Airplanes are transportation devices which are designed to move people and cargo from one place to another. Chapter Objective: Upon completion of this chapter, you will have a basic working knowledge of aircraft construction, structural stress, and materials used on both fixed- and rotary-wing airfraft. The primary factors to consider in aircraft structures are strength, weight, and reliability. The airplane shown on this slide is a turbine-powered airliner which has been chosen as a representative aircraft. Learn. IoT in Manufacturing Market grow at 20% CAGR from 2017 to 2024, No public clipboards found for this slide. Clipping is a handy way to collect important slides you want to go back to later. D. Semi-monocoque structure. The first four are commonly called basic stresses; the last two, combination stresses. If you continue browsing the site, you agree to the use of cookies on this website. The skin of the aircraft carries most of the structural load of the aircraft… 16 17 FUSELAGE • The fuselage is the main structure or body of the fixed-wing aircraft. Chapter 4: Aircraft Basic Construction. You need to understand the stresses encountered on the main parts of an aircraft. Here are some general tips that apply to all such assemblies: 1) Dry fit the parts before gluing. Created by. i hope his slide is useful!!!!!!!!!!!!!!!!!! Aircraft: Design & Structure. Looks like you’ve clipped this slide to already. 8. Flashcards. PLAY. As of this date, Scribd will manage your SlideShare account and any content you may have on SlideShare, and Scribd's General Terms of Use and Privacy Policy will apply. According to the current Title 14 of the Code of Federal Regulations (14 CFR) part 1, Definitions and Abbreviations, an aircraft is a device that is used, or intended to be used, for flight. Learn more. This area includes the cockpit, so the pilots are in the front of the fuselage. Aircraft structural members are designed to carry a load or to resist stress. Basic Aircraft Structure Slideshare uses cookies to improve functionality and performance, and to provide you with relevant advertising. These factors determine the requirements to be met by any material used to construct or repair the aircraft. Fuselage Landing gear Nacelle Tires. Slideshare uses cookies to improve functionality and performance, and to provide you with relevant advertising. decomposed into a horizontal component Vx and a vertical component Vy as Vx = τta (1.4) Vy = τtb (1.5) Thus, the components of the resultant force of the shear stress τ have the relation CHAPTER 1. B. Fail-safe structure. B.

basic aircraft structure

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