Aeronaves Y Vehículos Espaciales Tema 1 – Introducción General Del Entorno Aeroespacial

Total Page:16

File Type:pdf, Size:1020Kb

Aeronaves Y Vehículos Espaciales Tema 1 – Introducción General Del Entorno Aeroespacial Aeronaves y Vehículos Espaciales Tema 1 – Introducción General del Entorno Aeroespacial Sergio Esteban Roncero Francisco Gavilán Jiménez Departamento de Ingeniería Aeroespacial y Mecánica de Fluidos Escuela Superior de Ingenieros Universidad de Sevilla Curso 2011-2012 Introducción a la Ingeniería Aeroespacial Contenido Clasificación General de los Vehículos Aeroespaciales. Clasificación General de los Sistemas de Propulsión . Infraestructuras Terrestres. TáfiTráfico Aé reo. Industria Aeronáutica. Introducción a la Ingeniería Aeroespacial 2 Índice Clasificacióíón General de los Vehículos Aeroespaciales. Aeronaves Vehículos Espaciales Vehículos Cohete Clasificación General de los Sistemas de Propulsión. Infraestructuras Terrestres. Tráfico Aéreo. Industria Aeronáutica. Introducción a la Ingeniería Aeroespacial 3 Clasificación General de los vehículos aeroespaciales La clasificación de los vehículos aeroespaciales puede hacerse siguiendo distintos criterios. A continuación se da una posible clasificación general. Aeronaves Aerostatos Aerodinos Vehículos Espaciales Satélites / Estaciones orbitales Sondas interplanetarias Módu los d e d escenso Vehículos Cohetes Lanzadores Misiles Introducción a la Ingeniería Aeroespacial 4 Aerostatos Aeronave qqppqpue se sirve del principio de Arquímedes para volar. Constan de un gran recipiente donde se almacena un gas ligero. La densidad total de la aeronave es menor que la del aire que lo rodea. Dos tipos: Globos: no tienen ningún tipo de propulsor, se ”dejan llevar” por las corrientes de aire , aunque sí hay algunos tipos que pueden controlar su elevación. Dirigibles: aerostato con propulsión y capacidad de maniobra. 3 2 1 Introducción a la Ingeniería Aeroespacial 5 Aerostatos - Globos Un aerostato es una aeronave provista de uno o más recipientes llenos de un gas más ligero que el aire atmosférico, lo que la hace flotar o elevarse en el seno de este. Compuestos por: Una bolsa que encierra una masa de gas más ligero que el aire. Estructura sólida (barquilla) o se le puede "atar" cualquier tipo de cuerpo. No tienen ninggpún tipo de p ppropulsor: se "dejan llevar" pp(or las corrientes de aire (controlar su elevación). Usos comunes: Aeronavegación deportiva, turística y lúdica. Meteorología – globos estratosféricos. Anuncios publicitarios Hermanos Montgolfier (1782) Glo bos met eoro lógi cos Globo aerostático Aire caliente Introducción a la Ingeniería Aeroespacial 6 Aerostatos – Dirigibles Un dirigible es un aerostato con propulsión y con capacidad de maniobra para ser gobernado libremente como una aeronave. Su forma suele ser de globo alargado ovalado para ofrecer menos resistencia aerodinámica en el avance. Como gas sustentador para el globo se suele usar gas helio. Glob o di ri gibl e Frances Diiirigibl e f uturos? Hindenburg Introducción a la Ingeniería Aeroespacial 7 Aerodinos Aeronaves más densas que el fluido en el que se mueven. Consiguen la sustentación mediante el desarrollo de fuerzas fluidodinámicas generadas en alas fijas o alas giratorias. Clasificación: Sin M ot or Veleros Planeadores Con Motor Aeronaves de ala fija: Aeroplanos. Anfibios Hidroaviones Aviones de baja velocidad Aviones subsónicos AiAviones supersó óinicos Aviones hipersónicos Aeronaves de ala rotatoria Autogiro Girodino Helicópteros Convertibles Ornitóptero Introducción a la Ingeniería Aeroespacial 8 Aeroplanos – Anfibios Un aeronave anfibia es aquella que puede aterrizar tanto en tierra, hierba o en agua. Canadair CL-215 Beriev Be-200 PBY Catalina Dornier Do X Introducción a la Ingeniería Aeroespacial 9 Aeroplanos - Hidroaviones Un hidroavión es un avión qq,gue lleva, en lugar de ruedas, uno o varios flotadores para posarse sobre el agua. Esto le hace capaz de despegar desde y aterrizar en el agua (o amerizar). Spruce Goose DeHavilland Twin Otter DeHavilland Single Otter Harbour Kaspian Monster Introducción a la Ingeniería Aeroespacial 10 Aeroplanos – Hidroaviones Futuros Boeing Phantom Works: Pelican ULTRA (Large Transport Aircraft) Carga 1400 Tn Alcance 16.000 km Envergadura 152 m Length 400 ft US Aerocon Introducción a la Ingeniería Aeroespacial 11 Aviones de baja velocidad Aviones de baja velocidad en las que la propulsión suele ser mediante propulsores de hélice: Primer vuelo de los hermanos Wright el 11 de diciembre de 1903 El vuelo de motor de baja velocidad se ha convertido en una actividad muy asequible al público en general Avionetas Paramotor Ala delta con motor Cessna 182 Introducción a la Ingeniería Aeroespacial 12 Aviones Subsónicos En esta categggyoría se encuentra la gran mayoría de las aeronaves actuales. Pueden alcanzar velocidades cercanas a la del sonido (Mach ~ 0.85) Messerschmitt Me 262 B 787 B 737 B 747 A 380 Introducción a la Ingeniería Aeroespacial 13 Comparativas del tamaño de los aviones SGSpruce Goose B 747 An-225 A 380 Introducción a la Ingeniería Aeroespacial 14 Avión Supersónico - I Un avión supersónico, es un avión capaz de pasar la barrera del sonido (Número Mach). Es 1947 el piloto norteamericano Chuck Yeager rompe por primera vez la velocidad del sonido en su avión-cohete Bell X-1, demostrando que es posible viajar más rápido que el sonido. El Tupolev Tu-144 es un avión supersónico construido por el Bell X-1 fabricante ruso Tupolev. El pri mer vuel o d e un prot oti po d el T u-144 se llevó a cab o el 31 d e diciembre de 1968 cerca de Moscú, dos meses antes que el Concorde. El Tu-144 cruzó por primera vez la barrera del sonido el 5 de junio de 1969 y e l 15 de ju lio d e 1969 se conviióirtió en el pri mer transporte comercial que excedió el Mach 2. Concorde Grandes problemas medioambientales. Tu-144 Introducción a la Ingeniería Aeroespacial Avión Supersónico - II Lockheed SR-71 (Blackbird) : Avión de reconocimiento estratégico de largo alcance de Mach 3 (~3500 km/h @ 24000 m) . SpaceShipOne: El 4 de octubre de 2004, el SpaceShipOne consiguió alcanzar el espacio por segunda vez en 15 días, consiguiendo con ello ganar el premio Ansari X-Prize, dotado con 10 millones de dólares, y proclamarse el primer vehículo espacial tripulado de capital privado con una velocidad máxima de Mach 3. 09. SpaceShipOne SR-71 Introducción a la Ingeniería Aeroespacial Avión Supersónico - III Introducción a la Ingeniería Aeroespacial Avión Supersónico - IV Introducción a la Ingeniería Aeroespacial Aviones Hipersónicos - I Pueden alcanzar velocidades superiores a cinco veces la velocidad del sonido (~6120 km//)hr). Son conocidos como aviones cohete, ya que usan un cohete como propulsión, a veces junto con un reactores. Su tiempo de funcionamiento es muy corto, típicamente sólo unos minutos. Antecedentes X-15: Avión cohete de la década de los 70 que estableció varios récords de velocidad (Mach 8 ~7274 km/h) y de altura (107960m). X-43A Hyper – X 23 de marzo del 2004 supp(/)ero velocidades de Mach 9.6 (11200 km/h) X-15 Introducción a la Ingeniería Aeroespacial 19 Aviones Hipersónicos – II (X-43A) Introducción a la Ingeniería Aeroespacial 20 Aeronaves de alas giratorias - I Una aeronave de alas giratorias es un aerodino en el que las fuerzas de sustentación se logran mediante el giro de alas (o palas) alrededor de un eje. Autogiro Se clasificación en: Autogiro Girodino Girodino Helicóptero Convertibles: Alas inclinadas (tilt-wing) Rotores inclinados (tilt-rotor) Convertibles Helicóptero Introducción a la Ingeniería Aeroespacial 21 Aeronaves de alas giratorias - II FiFairey RtdRotodyne La Cierva C.19 AtAutog iro Girodino HliótHelicóptero V22 - Osprey Convertible Ka-50/52 Introducción a la Ingeniería Aeroespacial 22 Autogiro Dispone de un dos sistemas de alas giratorias. Uno de ellos es accionado por un motor y proporciona el empuje necesario para vencer la resitistenc ia al avance. El otro sistema de alas giratorias no consume potencia y proporciona sustentación mediante el proceso de autorrotación por el cual es el aire en el que comunica energía a las alas giratorias. Es ta aeronave no tiene capac idad d e reali zar vuel o est aci onari o o a punt o fij o. La Cierva C.4 Aurogyro-ELA-07-Casarrubios La Cierva C.19 x Introducción a la Ingeniería Aeroespacial 23 Girodino Dispone también de dos sistemas de alas giratorias. AbAmbos si stemas son accidionados me ditdiante un mot or: Uno de los sistemas es el principal responsable de generar la sustentación. El otro genera el empuje necesario. Fairey Rotodyne Introducción a la Ingeniería Aeroespacial 24 Helicópteros Dispone también de dos sistemas de alas giratorias y también accionados por un motor . El sistema de alas giratorias (rotor principal) es el responsable de crear la sustentación y a su vez es el responsable de crear el empuje necesario para el vuelo. El otro sistema de alas giratorias (rotor antipar) se encarga de proporcionar el par necesario para contrarrestar el par que crea el rotor ppprincipal. Existen configuraciones especiales dónde no existe rotor antipar (NOTAR) o dónde coexisten varios rotores principales. NOTAR Bell 206B Jet Ranger III Introducción a la Ingeniería Aeroespacial 25 Helicópteros – Configgppuraciones de rotor principal Monorrotores. Birrotores. Entrelazados. En tandem. Multirrotores. Introducción a la Ingeniería Aeroespacial 26 Aeronaves Convertibles Único sistema de alas giratorias para proporcionar sustentación y empuje. El cambio de funcionalidad lo consigue mediante el cambio de orientación. Despegue las alas giratorias proporcionan el empuje en dirección vertical, tracción, colocando las alas giratorias en
Recommended publications
  • Police Aviation News SPECIAL EDITION
    Police Aviation News SPECIAL EDITION ©Police Aviation Research SPECIAL EDITION JULY 2012 PAR Police Aviation News July 2012 2 PAN—Police Aviation News is published monthly by POLICE AVIATION RESEARCH, 7 Wind- mill Close, Honey Lane, Waltham Abbey, Essex EN9 3BQ UK. Contacts: Main: +44 1992 714162 Cell: +44 7778 296650 Skype: BrynElliott E-mail: [email protected] SHOWS JULY 2012 FARNBOROUGH AIR SHOW Farnborough, Hampshire, UK 9-10 July 2012 Farnborough, one of the major shows in the aerospace calendar and yet in the main one not too kind to the Airborne Emergency Service sector of business. The large size and im- personal nature of Farnborough and its ilk are the main spur for the niche air events – not always shows – including PAvCon, NBAA and Heli-Expo. Visitors are drawn to see displays covering nearly 3,500 square meters from hundreds of international companies housed under cover in a number of vast halls and chalets con- structed at great expense – others being left to the vagaries of the weather without cover or in their own tents and caravans. And this year the vagaries were decidedly nasty as Britain endured the worst summer in living memory. The poor weather clearly affected visitor num- bers early in the week. As the browned grass testifies, Farnborough 2010 was a far drier affair than this year. © Aviation-images.com via FI2012 Front Cover Image: The Bell 525 Relentless has ‘Oil Industry’ written all over it and it may never feature as an emergency services aircraft. That said it has features that could one day appear more widely—including the pilots seats.
    [Show full text]
  • Textron: Action & Results
    130124 5/14/03 2:16 PM Page FC1 Textron: Action & Results 2002 Fact Book 130124 5/14/03 2:16 PM Page IFC2 Textron is an $11 billion multi-industry company with approximately 49,000 employees in 40 countries. We leverage our global network of businesses to provide customers with innovative solutions and services in industries such as aircraft, fastening systems, industrial products and components, and finance. Textron is known around the world for its powerful brands, such as Bell Helicopter, Cessna Aircraft, Kautex, Lycoming, E-Z-GO and Greenlee, among others. Stock and Contact Information Stock Exchange Listings General Information Ticker Symbol – TXT This Fact Book is one of several sources of information available to Textron Inc. shareholders and the investment community. To receive Annual Common Stock Reports, 10-K, 10-Q reports and/or press releases, please call (888) TXT- New York, Chicago and Pacific Stock Exchanges LINE or visit our website at www.textron.com Preferred Stock ($2.08 and $1.40) New York Stock Exchange Contacts Investors Mandatorily Redeemable Preferred Securities of Subsidiary Trust (7.92%) Douglas R. Wilburne New York Stock Exchange Vice President, Communications & Investor Relations [email protected] Capital Stock (401) 457-2353 (as of December 28, 2002) (401) 457-3598 (fax) Common stock: par value $0.125; 500,000,000 shares authorized; Marc Kaplan 136,499,608 shares outstanding. Director, Investor Relations $2.08 Cumulative Convertible Preferred stock, Series A: [email protected] 120,515 shares outstanding. (401) 457-2502 (401) 457-3598 (fax) $1.40 Convertible Preferred Dividend stock, Series B: 56,394 shares outstanding.
    [Show full text]
  • Initial Tiltrotor Aeroacoustic Code (TRAC) Predictions for the XV-15 Flight Vehicle and Comparison with Flight Measurements
    56th American Helicopter Society Annual Forum 2000 Virginia Beach, Virginia, USA 2 – 4 May 2000 Volume 1 of 3 ISBN: 978-1-61782-937-6 Printed from e-media with permission by: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 Some format issues inherent in the e-media version may also appear in this print version. Copyright© (2000) by the American Helicopter Society All rights reserved. Printed by Curran Associates, Inc. (2011) For permission requests, please contact the American Helicopter Society at the address below. American Helicopter Society 217 N. Washington Street Alexandria, VA 22314-2538 Phone (703) 684-6777 Fax: (703) 739-9279 [email protected] Additional copies of this publication are available from: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 USA Phone: 845-758-0400 Fax: 845-758-2634 Email: [email protected] Web: www.proceedings.com TABLE OF CONTENTS VOLUME 1 ACOUSTICS Initial Tiltrotor Aeroacoustic Code (TRAC) Predictions for the XV-15 Flight Vehicle and Comparison with Flight Measurements.....................................................................................................................................................1 Prichard, Devon S. Prediction and Validation of Helicopter Descent Flyover Noise...................................................................................... 18 Janakiramram, Ram D.; Khan, Hamza Structure of the Blade Pressure Fluctuations Generated by Helicopter Rotor Blade-Wake Interaction..................... 36 Bouchet, Eric; Rahier, Gilles Validation
    [Show full text]
  • The Power to Grow
    The Power to Grow 2004 Fact Book Textron Inc. is a $10 billion multi-industry company with more than 44,000 employees in nearly 40 countries. The company leverages its global network of aircraft, industrial and finance businesses to provide customers with innovative solutions and services. Textron is known around the world for its powerful brands, including Bell Helicopter, Cessna Aircraft, Jacobsen, Kautex, Lycoming, E-Z-GO and Greenlee, among others. Stock and Contact Information Stock Exchange Listings General Information Ticker Symbol – TXT This Fact Book is one of several sources of information available to Textron Inc. shareholders and the investment community. To receive Common Stock Annual Reports, 10-K, 10-Q reports and/or press releases, please New York, Chicago and Pacific Stock Exchanges call (888) TXT-LINE or visit our website at www.textron.com. Preferred Stock ($2.08 and $1.40) New York Stock Exchange Contacts Investors Capital Stock Douglas R. Wilburne (as of January 1, 2005) Vice President, Investor Relations Common stock: par value $0.125; 500,000,000 shares authorized; [email protected] 135,373,000 shares outstanding. (401) 457-3606 (401) 457-2220 (fax) $2.08 Cumulative Convertible Preferred stock, Series A: 105,000 shares outstanding. William E. Pitts Director, Investor Relations $1.40 Convertible Preferred Dividend stock, Series B: [email protected] 50,000 shares outstanding. (401) 457-2502 (401) 457-2220 (fax) Transfer Agent and Registrar Wachovia Bank, NA Banks and Rating Agencies Shareholder Services Group – NC1153 Mary F. Lovejoy 1525 West W.T Harris Blvd., 3C3 Vice President and Treasurer Charlotte, NC 28288-1153 [email protected] Phone: (800) 829-8432 (401) 457-6009 Fax: (704) 590-7618 or (704) 590-7614 (401) 457-3533 (fax) E-mail: [email protected] Media Web: www.wachovia.com/firstlink Susan M.
    [Show full text]
  • De L'astronomie À L'entrepreneuriat
    De l’astronomie à l’entrepreneuriat Juin – août 2017 Olivier Ezratty De l’astronomie à l’entrepreneuriat – Olivier Ezratty – Juin-Août 2016 - Page 1 / 255 A propos de l’auteur Olivier Ezratty olivier (at) oezratty.net , http://www.oezratty.net , @olivez consultant et auteur +33 6 67 37 92 41 Olivier Ezratty conseille les entreprises dans l’élaboration de leurs business plans, stratégies produits et marketing, avec une focalisation sur les projets à fort contenu technique et scientifique (objets connectés, intelligence artifi- cielle, medtechs, biotechs, …). Il leur apporte un triple regard : technologique, marketing et management ainsi que la connaissance des écosystèmes dans les industries numériques. Il a réalisé depuis 2005 des missions diverses d’accompagnement stratégique et de conférences ou formations dans différents secteurs tels que la télévision (TF1, RTS-SSR, SES Astra, TDF, Euro Media Group, Netgem), les télécoms (Bouygues Télécom, Orange, SFR, Alcatel-Lucent), les produits grand public (LG Electronics, groupe Seb, L’Oréal, Alt Group), la finance et l’assurance (BPCE, Crédit Agricole, Crédit Mutuel-CIC, Société Géné- rale, Natixis, Groupama). Ces missions couvrent l’assistance à la création de roadmap produit, l’analyse de posi- tionnement et de la concurrence, la définition technologique et marketing de stratégies d’écosystèmes et « d’innovation ouverte », l’assistance à la réalisation de business plans, l’animation de séminaires de brainstor- ming, ainsi que l’intervention dans des conférences et séminaires sur les tendances du marché dans le numérique. Ses contributions s’appuient sur un fort investissement dans l’écosystème de l’innovation et sous différentes cas- quettes, notamment dans l’univers des startups : Expert, membre et l’un des présidents du comité d’agrément de Scientipôle Initiative (Wiplo), une associa- tion membre d’Initiative France qui accélère les startups franciliennes.
    [Show full text]
  • Energiya BURAN the Soviet Space Shuttle.Pdf
    Energiya±Buran The Soviet Space Shuttle Bart Hendrickx and Bert Vis Energiya±Buran The Soviet Space Shuttle Published in association with Praxis Publishing Chichester, UK Mr Bart Hendrickx Mr Bert Vis Russian Space Historian Space¯ight Historian Mortsel Den Haag Belgium The Netherlands SPRINGER±PRAXIS BOOKS IN SPACE EXPLORATION SUBJECT ADVISORY EDITOR: John Mason, M.Sc., B.Sc., Ph.D. ISBN978-0-387-69848-9 Springer Berlin Heidelberg NewYork Springer is part of Springer-Science + Business Media (springer.com) Library of Congress Control Number: 2007929116 Apart from any fair dealing for the purposes of research or private study, or criticism or review, as permitted under the Copyright, Designs and Patents Act 1988, this publication may only be reproduced, stored or transmitted, in any form or by any means, with the prior permission in writing of the publishers, or in the case of reprographic reproduction in accordance with the terms of licences issued by the Copyright Licensing Agency. Enquiries concerning reproduction outside those terms should be sent to the publishers. # Praxis Publishing Ltd, Chichester, UK, 2007 Printed in Germany The use of general descriptive names, registered names, trademarks, etc. in this publication does not imply, even in the absence of a speci®c statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. Cover design: Jim Wilkie Project management: Originator Publishing Services Ltd, Gt Yarmouth, Norfolk, UK Printed on acid-free paper Contents Ooedhpjmbhe ........................................ xiii Foreword (translation of Ooedhpjmbhe)........................ xv Authors' preface ....................................... xvii Acknowledgments ...................................... xix List of ®gures ........................................ xxi 1 The roots of Buran .................................
    [Show full text]
  • Bell Helicopter Corporation
    Bell Helicopter Corporation In the early 1930 's, Arthur Young , a brilliant young inventor, built and successfully demonstrated a viable, flyable helicopter model. Larry Bell , a successful entrepreneur and founder of the Bell Aircraft Corporation , was so impressed with Young's efforts that in 1941 he set the youthful inventor up in a small shop in Gardenville, New York At that time Bell was already a manufacturer of conventional aircraft such as the WWII fighter P-39 Airacobra and the P-59, America's first jet-powered airplane. In addition, Bell was to develop the X-1, which was to become the world's first super- sonic plane. By 1951, Bell helicopters were in service around the world, breaking records as fast as they were setting them. And since Bell Aircraft Corporation's reputation for helicopter manufacture began to rival its reputation as a builder of conventional aircraft , the company created a separate helicopter division which was headquartered in Fort Worth, Texas. Today, with Bell helicopters flying in more than 120 different countries , they are logging another ten hours every minute of every day. Our History Bell Aircraft Corporation, the predecessor of Bell Helicopter Textron was founded July 10, 1935 in Buffalo, New York by Lawrence D. Bell, a man referred to as "America's most seasoned dreamer." Bell Aircraft Corporation created a Helicopter Division which moved to Fort Worth, Texas in 1951 and became Bell Helicopter Corporation, a wholly owned subsidiary of Bell Aircraft Corporation. In 1960, Textron of Providence, Rhode Island bought various Bell Aircraft properties including the Helicopter operation.
    [Show full text]
  • Position, Attitude, and Fault-Tolerant Control of Tilting-Rotor Quadcopter
    Position, Attitude, and Fault-Tolerant Control of Tilting-Rotor Quadcopter A thesis submitted to the Graduate School of the University of Cincinnati in partial fulfillment of the requirements of the degree of Master of Science in the Department of Aerospace Engineering and Engineering Mechanics of the College of Engineering and Applied Sciences by Rumit Kumar B. Tech. Maharshi Dayanand University August-2012 Committee Chair: M. Kumar, Ph.D. Copyright 2017, Rumit Kumar This document is copyrighted material. Under copyright law, no parts of this document may be reproduced without the expressed permission of the author. An Abstract of Position, Attitude, and Fault-Tolerant Control of Tilting-Rotor Quadcopter by Rumit Kumar Submitted to the Graduate Faculty as partial fulfillment of the requirements for the Master of Science Degree in Aerospace Engineering University of Cincinnati March 2017 The aim of this thesis is to present algorithms for autonomous control of tilt-rotor quad- copter UAV. In particular, this research work describes position, attitude and fault tolerant con- trol in tilt-rotor quadcopter. Quadcopters are one of the most popular and reliable unmanned aerial systems because of the design simplicity, hovering capabilities and minimal operational cost. Numerous applications for quadcopters have been explored all over the world but very little work has been done to explore design enhancements and address the fault-tolerant capabil- ities of the quadcopters. The tilting rotor quadcopter is a structural advancement of traditional quadcopter and it provides additional actuated controls as the propeller motors are actuated for tilt which can be utilized to improve efficiency of the aerial vehicle during flight.
    [Show full text]
  • Design and Analysis of Delta Wing Tilt Rotor UAV
    S.Ravikanth et al.Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 7, ( Part - 1) July 2015, pp.119-136 RESEARCH ARTICLE OPEN ACCESS Design and Analysis of Delta Wing Tilt Rotor UAV S.Ravikanth 1 , V.V.S.Nikhil Bharadwaj 2 , M.Sai Dheeraj 3 , B.Venkata Sai Anoop4 , Md. Abdul Sami 5 , Sai Apurva .N6, Laskara Farooq7 1 Assistant Professor , Department Of Aeronautical Engineering , MLR Institute Of Technology , Dundigal , Hyderabad.INDIA. 2,4,5.6B.Tech Student , Department Of Aeronautical Engineering , MLR Institute Of Technology , Dundigal ,Hyderabad.INDIA. 3,7 B.Tech Student , Department Of Aeronautical Engineering , MLR Institute Of Technology and Management , Dundigal ,Hyderabad.INDIA. ABSTRACT : A tilt rotor is an aircraft of a special kind, which possesses the characteristics of a helicopter and a fixed-wing airplane. However, there are a great number of important technical problems waiting for settlements. Of them, the flight control system might be a critical one. A tiltrotor aircraft comprising a pair of contra-rotating co-axial tiltable rotors on the longitudinal center line of the aircraft. The rotors may be tiltable sequentially and independently. They may be moveable between a lift position and a flight position in front of or behind the fuselage.In this paper we present a project aimed for the designing of a small scale Unmanned Aerial Vehicle (UAV) with Tiltrotor configuration (that uses two rotating rotors). he current paper describes the adopted design methodology, the mathematical and computational models created to represent the UAV, the physical components that constitute the UAV, and the results obtained so far.
    [Show full text]
  • Gas Turbines Specs.V2 C C M Y K OUTLOOK/SPECIFICATIONS GAS TURBINE ENGINES GENERAL DATA ARRANGEMENT PERFORMANCE DIMENSIONS & WTS
    OUTLOOK/SPECIFICATIONS GAS TURBINE ENGINES GENERAL DATA ARRANGEMENT PERFORMANCE DIMENSIONS & WTS. - . P R R H E R M S - . E E U * P W E * S ) G H W . O R E / N A P O P ) . P U T T E . E O E H P B . S Y S P A APPLICATIONS / P C L P S N . S T MODEL OR X I H ) / / r O TYPE* S E R O L R . ) X B A / o L . L S E R T E R B O REMARKS . A . E R E E N S L N U M DESIGNATION P O P S L I R ( W L V U F L ) V A M T U S ( . ( T L E . H T F O N S E E N R - C T L T A . N V E I H E P S P F F R U F I H A A E I F ( T E . W . B B P I T O O O L R P L I - . G G X C N X X . E L / M M Y T E I A A A A N . A A O B I O O V A R O O T E P I E A B L M D O ( N N C S C M S S T L R M L D T ACCURATE AUTOMATION CORP., Chattanooga, TN, USA AT-1500 C-J 1 1 An 150 lb. t. 1.35 3.8 8.8 14.5 18 Decoys, targets, UAVs.
    [Show full text]
  • The History of the XV-15 Tilt Rotor Research Aircraft
    * cover (Final) 2/18/04 2:27 PM Page 1 The History of The XV-15 Tilt Rotor Research Aircraft From Concept to Flight The History of the XV-15 Tilt Rotor Research Aircraft:FromConcepttoFlight Research Rotor Tilt The HistoryoftheXV-15 Monograph 17NASASP-2000-4517 National Aeronautics and Space Administration Martin D. Maisel • Demo J. Giulianetti • Daniel C. Dugan NASA SP-2000-4517 The History of the XV-15 Tilt Rotor Research Aircraft: From Concept to Flight Martin D. Maisel Demo J. Giulianetti and Daniel C. Dugan Monographs in Aerospace History #17 The NASA History Series National Aeronautics and Space Administration Office of Policy and Plans NASA History Division Washington, D.C. 2000 Contents Prologue . iii Dedication . v Acknowledgments . vii Forewords . ix List of Figures . xiii List of Acronyms . xix Introduction . 1 Early Efforts. 4 XV-3 Program . 12 NASA-Army Cooperation . 19 Building the Technology Base. 20 Tilt Rotor Research Aircraft Project Office. 28 Aircraft Development . 42 Navy Participation . 59 Flight Envelope Expansion . 61 Flight Research . 65 Incidents. 83 Paris Air Show . 88 Evaluations and Demonstrations . 91 Crash . 98 The End of an Era . 100 XV-15 Project Summary . 103 Epilogue . 105 Appendix A Aircraft Descriptions . 115 Appendix B Key Personnel . 133 Appendix C Chronology . 140 Appendix D Awards and Records . 154 Appendix E Photo Gallery. 157 Appendix F Bibliography of Tilt Rotor Related Publications. 164 About the Authors . 185 Index . 187 i Prologue This monograph is a testament to the efforts of many people overcoming multi- ple technical challenges encountered while developing the XV-15 tilt rotor research aircraft.
    [Show full text]
  • The History Of
    * cover (Final) 2/18/04 2:27 PM Page 1 The History of The XV-15 Tilt Rotor Research Aircraft From Concept to Flight The History of the XV-15 Tilt Rotor Research Aircraft:FromConcepttoFlight Research Rotor Tilt The HistoryoftheXV-15 Monograph 17NASASP-2000-4517 National Aeronautics and Space Administration Martin D. Maisel • Demo J. Giulianetti • Daniel C. Dugan NASA SP-2000-4517 The History of the XV-15 Tilt Rotor Research Aircraft: From Concept to Flight Martin D. Maisel Demo J. Giulianetti and Daniel C. Dugan Monographs in Aerospace History #17 The NASA History Series National Aeronautics and Space Administration Office of Policy and Plans NASA History Division Washington, D.C. 2000 Contents Prologue . iii Dedication . v Acknowledgments . vii Forewords . ix List of Figures . xiii List of Acronyms . xix Introduction . 1 Early Efforts. 4 XV-3 Program . 12 NASA-Army Cooperation . 19 Building the Technology Base. 20 Tilt Rotor Research Aircraft Project Office. 28 Aircraft Development . 42 Navy Participation . 59 Flight Envelope Expansion . 61 Flight Research . 65 Incidents. 83 Paris Air Show . 88 Evaluations and Demonstrations . 91 Crash . 98 The End of an Era . 100 XV-15 Project Summary . 103 Epilogue . 105 Appendix A Aircraft Descriptions . 115 Appendix B Key Personnel . 133 Appendix C Chronology . 140 Appendix D Awards and Records . 154 Appendix E Photo Gallery. 157 Appendix F Bibliography of Tilt Rotor Related Publications. 164 About the Authors . 185 Index . 187 i Prologue This monograph is a testament to the efforts of many people overcoming multi- ple technical challenges encountered while developing the XV-15 tilt rotor research aircraft.
    [Show full text]