Libros de Ingeniería aeronáutica y astronáutica, página 2 de 52

Este manual desarrolla los temas incluidos en el Módulo 16 Piston Engines, del programa EASA Parte 66 para técnicos de mantenimiento de aeronaves. Los primeros cinco capítulos están dedicados al estudio de los componentes del motor: cilindro, embolo, biela, cigueñal, valvulas, carter y reductores. Una vez conocidos estos elementos de la arquitectura del motor, es posible abordar con suficiencia los ciclos motores Otto y Diesel, asi como sus rendimientos, contemplados desde la perspectiva del motor de aviacion en los ciclos de cuatro y dos tiempos. El extenso Capitulo 7 trata de la inspeccion, revision, y almacenamiento y preservacion del motor, en atencion a los elementos fundamentales estudiados. Los motores turboalimentados, la carburacion e inyeccion junto al sistema de control electronico FADEC ocupan los capitulos 8 a 13. Preparada, pues, la mezcla aire-gasolina procede a continuacion el estudio del encendido y de puesta en marcha del motor. Los capitulos restantes se dedican al estudio de los sistemas de lubricacion y refrigeracion, en los motores de aviacion de ciclo Otto y Diesel. Cada capitulo se acompaña de gran cantidad de imagenes y esquemas que ayudaran al lector en la comprension de la teoria. El libro finaliza con un completo Indice alfabetico que sera una herramienta muy util de consulta. Por todo lo anterior, Motores de piston para aviones busca, por un lado, ser de ayuda al futuro tecnico para superar con exito los examenes que debe cursar; por otro, introducirle en la tecnologia clasica y avanzada que ha llegado al motor alternativo y que asegura su longevidad en la propulsion de pequeñas aeronaves. Finalmente, la capacidad del motor Diesel de aviacion para usar combustibles para reactores, tipos Jet A o Jet A-1, sin problemas de logistica en cualquier parte del mundo, potencia aun mas esta perspectiva de futuro del motor alternativo. El autor ha trabajado durante muchos años como Ingeniero Inspector de Seguridad en Vuelo, y como profesor para Piloto de Transporte de Linea Aerea (ATPL) y Tecnico de Mantenimiento. Fruto de esa experiencia ha publicado ya otros titulos como Conocimientos del avion, Estructuras de las aeronaves, y Materiales y elementales aeronauticos en esta editorial.

Desde su primera edición, esta obra ha ido experimentando tanto ampliaciones como mejoras en la exposición de los conceptos. El contenido se ha ido adaptando a las exigencias y al aumento del nivel de formacion de los pilotos por parte de las autoridades aeronauticas. En esta decimotercera edicion, corregida y actualizada, se ha cuidado la puesta al dia de algunos temas referentes a la normativa de la FAA y de la JAA (EASA).;Nacido como libro de texto para los pilotos de Iberia, su estudio ha pasado a ser fundamental no solo para los pilotos, tanto militares como civiles, sino tambien para mecanicos de vuelo, tecnicos de operaciones, despachadores de vuelo y controladores de la circulacion aerea.;El contenido de la obra cubre las siguientes materias: caracteristicas de la atmosfera, conceptos elementales de dinamica de fluidos, origen de las fuerzas aerodinamicas, influencia de la forma en planta del ala, dispositivos hipersustentadores, actuaciones de los aviones con motores de embolo, actuaciones de los aviones con motores de reaccion, vuelo a velocidades altas, efectos de la compresibilidad, requisitos, velocidades y distancias en despegues, aterrizajes y en ruta, actuaciones de despegue y aterrizaje, limitaciones estructurales, diagrama de maniobra, generalidades sobre estabilidad estatica y dinamica, estabilidad longitudinal, estabilidad direccional y lateral, ondas de choque y expansion y vuelo supersonico.;Asimismo, incluye dos apendices y un util tesauro de acronimos. El texto, declarado de utilidad aeronautica por el Ejercito del Aire español, se ha distribuido desde la primera edicion tanto en España como en toda Hispanoamerica, y ha sido recomendado por escuelas aeronauticas y organismos oficiales de distintos paises, lo que da fe de la gran calidad de esta obra.;Anibal Isidoro Carmona, doctor ingeniero aeronautico, es especialista en la preparacion de pilotos y tecnicos directamente implicados en las operaciones de vuelo. Cuenta con una dilatada experiencia profesional como instructor en el Centro de Instruccion de Tripulaciones de Iberia, en el Centro de Enseñanza de CASA y como profesor en la Escuela Tecnica Superior de Ingenieros Aeronauticos de Madrid.

El presente texto describe y explica los principios fundamentales de la Electrónica que debe dominar todo aspirante a Técnico de Mantenimiento Aeromecánico para desempeñar su trabajo correctamente. El libro esta completamente adaptado a los contenidos del Modulo 4 (Fundamentos de Electronica) de la parte 66 del Reglamento (CE) 2042/2003 y del Reglamento (CE) 1149/2011, por lo que resulta ideal para la obtencion de la Licencia de Tecnico de Mantenimiento de Aeronaves LMA B.1, ya que trata cada tema con la profundidad adecuada.;Asimismo, el texto no solo es util para las organizaciones de formacion de mantenimiento parte 147 (centros 147), sino que resulta tambien increiblemente practico para aquellos que deseen prepararse por cuenta propia para aprobar el examen del Modulo 4 (Fundamentos de Electronica) gracias a las variadas cuestiones de autoevaluacion que se incluyen al final de cada unidad y a la bateria final de 200 preguntas de tipo test. Ademas, el libro incorpora un util anexo final.;Por ultimo, la obra esta completamente ilustrada con figuras, imagenes y esquemas que facilitan la comprension de los contenidos y sirven de valioso apoyo para la obtencion de la licencia de Tecnico de Mantenimiento.;El autor, ingeniero aeronautico por la Universidad Politecnica de Madrid, cuenta con mas de diez años de experiencia en la formacion de tecnicos de mantenimiento aeromecanico y ha publicado, tambien en esta editorial, los libros Modulo 2 (Fisica), Modulo 3 (Fundamentos de Electricidad) y Modulo 17 (Helices).

Análisis de fallos en sistemas aeronáuticos es un libro cuya génesis es la investigación del aspecto técnico de la industria aeroespacial, con una perspectiva interdisciplinaria y una visión integral de aporte a la seguridad operacional. Se trata de una obra de utilidad para todos los sectores y especialidades de la actividad aeronautica. Los contenidos y el analisis son de interes en la seguridad operacional tanto de los operadores comerciales como de la aviacion general o las organizaciones militares con medios aereos. A traves de los avances tecnicos y la investigacion de accidentes y sucesos inseguros, la industria ha logrado incrementar los niveles de seguridad; con ese criterio esta estructurada la obra. Desde los primeros contactos del hombre con los fallos de sus rudimentarias herramientas hasta los complejos materiales compuestos que hoy utiliza la industria aeroespacial, esta obra contempla el amplio espectro de materias primas, propiedades intrinsecas, comportamiento tipico y propension a fallos, a traves de una vision y un analisis interdisciplinario y sistemico. El texto esta estructurado de modo que el lector pueda utilizar este libro como lectura tecnica o como manual de consulta sobre temas especificos. La cronologia de los temas se ha desarrollado desde un marco historico evolutivo, partiendo desde las materias primas y las tecnicas de fabricacion, los conceptos de estructuras aeronauticas, la mecanica de fractura, el analisis de fallos (con y sin fractura), la mecanica de fatiga, los protocolos de analisis e investigacion internacionales, los factores humanos y organizacionales en el area tecnica, hasta un compendio de casos tipicos que posibilita la facil comprension de conceptos abstractos. La obra se estructura en 13 capitulos, desarrollados con un enfoque academico teorico, un marco historico referencial y procesos de comprobacion analitica. De igual modo, en todos los casos y capitulos se han utilizado datos, imagenes y graficos obtenidos de investigaciones reales de fallos en servicio en la industria aeronautica. Asimismo, el libro se nutre de gran cantidad de informacion obtenida durante el proceso de investigacion tecnica y deteccion de fallos en accidentes e incidentes de aviacion. Como se indicaba anteriormente, la obra en su conjunto presenta una marcada vision sistemica cuyo objetivo es hallar las causas profundas de los fallos y las condiciones latentes presentes en el sistema que propician los accidentes e incidentes. El autor, investigador tecnico de accidentes de aviacion, lleva mas de 15 años dedicado al estudio de la seguridad operacional desde el ambito tecnico, por lo que ha participado en la investigacion de accidentes de aviacion de transporte, aviacion general y aviacion deportiva. Actualmente desempeña su labor profesional en la autoridad aeronautica de la Republica Argentina como director nacional de investigaciones. Tambien ha sido docente de temas tecnicos especificos de investigacion y es autor de otros trabajos y obras relacionados con este ambito.

This title's pub date will be changed to Jan.2013 via a database correction form after the submission is accepted and the ISBN is in the system. This handbook for Aviation Maintenance Technicians (AMTs), repair stations, aircraft owners and homebuilders details the standards for acceptable methods, techniques, and practices for the inspection, repair, and alteration of aircraft. It is a combination of the two most important Advisory Circulars (ACs) written by the Federal Aviation Administration (FAA) on this topic--namely, "Acceptable Methods, Techniques, and Practices: Aircraft Inspection and Repair" (AC 43.13-1B) and "Acceptable Methods, Techniques and Practices: Aircraft Alterations" (AC 43.13-2B) -- printed and bound into one volume and called the "AC 43.13-1B/2B." AC 43.13-1B provides details on the materials and practices, health and safety, inspection, repair, and finishes for wood structures, fabric covering, fiberglass and plastics, and metal structures, welding and brazing. It includes chapters dedicated to nondestructive inspection (NDI), corrosion, inspection and protection, aircraft hardware, control cables and turnbuckles, engines, fuel, exhaust, propellers, aircraft systems and components, weight and balance, electrical systems, avionics, and human factors. AC 43.13-2B is a manual filled with details and instructions for the installation of aircraft components and systems, such as communications, navigation, and emergency systems, anticollision and supplementary lights, skis, oxygen systems in nonpressurized aircraft, rotorcraft external-load devices, cargo slings and external racks, glider and banner tow-hitches, aircraft batteries and more, including guidance on adding or relocating instruments. These combined manuals provide this pertinent information where no manufacturer repair or maintenance instructions exist. The details and standards for methods and practices covered are applicable to non-pressurized civil aircraft with a gross weight of 12,500 pounds or less. Illustrated throughout; includes a glossary, and a list of useful acronyms and abbreviations.

The aim of this book is to present quantitative and qualitative aspects of logistics operations supporting recycling and reuse. In individual chapters, the authors address various issues related to reverse network configuration and the organization of collection, transportation, warehousing and reprocessing activities. Moreover a number of best practice examples from different countries and industries are provided. This book will be a valuable resource for both academics and practitioners who want to deepen their knowledge of logistics operations and management for recycling and reuse.

The National Book League was a precursor to the current Booktrust, and was set up in 1924 by the Society of Bookmen in order to promote reading, particularly among the young. To that end, the NBL issued Reader's Guides on a variety of subjects, each written by an author with expertise in that field and containing an annotated bibliography of recommended titles on the subject. Charles Gibbs-Smith was the leading historian of aviation in the 1960s and 1970s, and published several books on the history of flight in Europe and America. This Reader's Guide, first published in 1957, has a detailed bibliography on the histories of a variety of aircraft, as well as a section on aerial battles from World War One onwards.

Results form the German research initiative ComFliTe (Computational Flight Testing)Advanced research in multidisciplinary numerical simulation in flight physics and their applications within the aeronautical industryWritten by leading experts in the fieldThis book reports on the German research initiative ComFliTe (Computational Flight Testing), the main goal of which was to enhance the capabilities of and tools for numerical simulation in flight physics to support future aircraft design and development. The initiative was coordinated by the German Aerospace Center (DLR) and promoted collaboration between the aircraft industry and academia. Activities focused on improving physical modeling for separated flows, developing advanced numerical algorithms for series computations and sensitivity predictions, as well as surrogate and reduced order modeling for aero data production and developing robust fluid-, structure- and flight mechanics coupling procedures. Further topics included more efficient handling of aircraft control surfaces and improving simulation methods for maneuvers, such as gust encounter. The important results of this three-year initiative were presented during the ComFliTe closing symposium, which took place at the DLR in Braunschweig, Germany, on 11-12 June 2012. Computational Flight Testing addresses both students and researchers in the areas of mathematics, numerical simulation and optimization methods, as well as professionals in aircraft design working at the forefront of their field.

This book provides a description of the modeling, design, and calculation of the aeronautical qualities of airplanes and drones. Divided into several parts, this book first summarizes all the necessary theoretical developments about the equations of motions and trajectory calculations of the machine. It then goes on to describe practical building processes and considers piloting methods. The last part makes a comparison between theoretical calculations and measured recorded data of the real flying machine.

Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered. The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to "what if" questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimization Provides an overview of advanced technologies for propulsion and reducing aerodynamic drag Offers insight into the derivation of design sensitivity information Emphasizes design based on first principles Considers pros and cons of innovative configurations Reconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts.

"Compressibility, Turbulence and High Speed Flow" introduces the reader to the field of compressible turbulence and compressible turbulent flows across a broad speed range, through a unique complimentary treatment of both the theoretical foundations and the measurement and analysis tools currently used. The book provides the reader with the necessary background and current trends in the theoretical and experimental aspects of compressible turbulent flows and compressible turbulence. Detailed derivations of the pertinent equations describing the motion of such turbulent flows is provided and an extensive discussion of the various approaches used in predicting both free shear and wall bounded flows is presented. Experimental measurement techniques common to the compressible flow regime are introduced with particular emphasis on the unique challenges presented by high speed flows. Both experimental and numerical simulation work is supplied throughout to provide the reader with an overall perspective of current trends. It features an introduction to current techniques in compressible turbulent flow analysis; an approach that enables engineers to identify and solve complex compressible flow challenges; prediction methodologies, including the Reynolds-averaged Navier Stokes (RANS) method, scale filtered methods and direct numerical simulation (DNS); and current strategies focusing on compressible flow control.

"Providing an early introduction to STEM education, this book uses simple text and labeled photographs to examine a wide range of exciting machines used at the airport, revealing how each machine solves a particular problem. Machines covered include jet airplanes, staircases on wheels, scanners, conveyor belts, radars, and more!"

Master's Thesis from the year 2008 in the subject Engineering - Aerospace Technology, grade: A, University of Southampton, course: Computational Aerodynamics, language: English, abstract: Wing-in-ground effect (WIG) vehicles offer an exciting capability to fill the enormous void between speed of an aircraft and the payload capacity of a ship. WIG vehicles would be able to move cargo and passengers faster than a ship and more economical than an aircraft. Ground effect is a phenomenon that occurs on all wings flying close to the ground or a surface. The aim of this project is to investigate the behavior of wings (NACA/DHMTU series) in ground effect (on a fixed/variable terrain) using Fluent CFD package. The NACA 0012 and DHMTU series used in this project are designed specifically to fly in close proximity to the ground. The performance of the NACA/ DHMTU airfoils is examined for the lift and the drag coefficients at different altitudes with varying angle of attack. The results are compared to experimental data that is available to assess the accuracy of the CFD simulation.

Proven techniques for deriving the basic aerodynamic properties of axisymmetric-shaped bodies with the minimum amount of time and effort Aerodynamics of Missiles and Rockets describes the basic aerodynamics model used in the widespread Analytical Initial Missile Synthesis (AIMS) computer code for symmetric missile and rocket sizing and design. It is a collection of empirical, semi-empirical and theoretical aerodynamics engineering methods for a component build-up approach to aerodynamics prediction. This book serves as an on-the-job application manual and desk reference for the prediction of basic aerodynamics. It can also be used for courses in applied aerodynamics in Mechanical and Aerospace Engineering programs and for short courses in industry and government. This practical guide provides an alternative approach to utilizing numerous, complex, stand-alone computer codes, but is also a good complement to these codes. The book offers insight into the methods and techniques used to derive answers and correct magnitudes generated by code, giving confidence in final results. Features a Microsoft Excel file that automates calculations and provides complete tabulated output for missile and rocket geometry and design, and design and for rapid assessments of aerodynamic properties based on changes in geometry or flight conditions On-the-job application manual and desk reference for the prediction of basic aerodynamics Combination of long-standing, empirical and semi-empirical techniques with classical aerodynamic theory A component build-up approach utilized, with body and wing/tail surface aerodynamics determined separately and then combined for total configuration zero-lift drag, lift, center of pressure location, and pitching moment

The Aircraft Designers: A Grumman Historical Perspective tells the behind-the-scenes story of the designers and engineers who conceived and built Grumman aircraft from the founding of the company in 1929 until its 1994 acquisition by Northrop. While Grumman aircraft have been previously documented, The Aircraft Designers focuses instead on the people, disciplines, processes, and anecdotes behind the creation of such past icons as the F6F Wildcat and TBF Avenger and modern-day weapon systems like the F-14 Tomcat, E-2 Hawkeye, EA-6B Prowler, and Joint STARS. Michael Ciminera has identified key team members who contributed to the creation and development of each new design, creating an unparalleled historical record of the aeronautical achievements of the Grumman Corporation. He has also chronicled the evolution from the aircraft design of the past, which bore the earmark of the chief engineer/designer, to today's complex aircraft systems, which require a significant team effort involving such disciplines as aerodynamics, structures, propulsion, avionics, systems analysis, software, simulation, testing, and much more. The Aircraft Designers provides a unique insight into the leadership traits, technical skills, and lasting contributions of Grumman's designers. It will stand as the definitive historical account of the people who made Grumman aircraft a reality.

The development of clean, sustainable energy systems is one of the pre-eminent issues of our time. Most projections indicate that combustion-based energy conversion systems will continue to be the predominant approach for the majority of our energy usage, and gas turbines will continue to be important combustion-based energy conversion devices for many decades to come, used for aircraft propulsion, ground-based power generation, and mechanical-drive applications. This book compiles the key scientific and technological knowledge associated with gas turbine emissions into a single authoritative source. The book has three sections: the first section reviews major issues with gas turbine combustion, including design approaches and constraints, within the context of emissions. The second section addresses fundamental issues associated with pollutant formation, modeling, and prediction. The third section features case studies from manufacturers and technology developers, emphasizing the system-level and practical issues that must be addressed in developing different types of gas turbines that emit pollutants at acceptable levels.

Aviation fuel hydrant systems at airports are the penultimate step in the delivery chain of aviation fuel into aircraft. It is therefore imperative to ensure that the quality and cleanliness of the jet fuel in the hydrant is maintained at all times. This publication has been developed to assist in the optimisation of hydrant system operations. It provides recommended practices for operational checks, inspections and maintenance procedures to ensure aviation fuel quality assurance and cleanliness standards are met. It also provides recommendations for associated equipment, from pump sets to hydrant pit valves and for those undertaking routine checks and inspections of such equipment. This publication is applicable to owners, operators and users of aviation fuel hydrant systems at airports worldwide. It will also be of interest to procurement managers of equipment and materials for hydrant system inspection, maintenance and checking purposes, including service providers. Hydrant system designers will also find this publication useful as background information on the expectations of hydrant system owners and operators. This publication includes a free A3 annual planner pull-out/separate downloadable pdf.

This volume contains an investigation of remotely piloted research vehicle (RPRV) and unmanned aircraft system (UAS) mishaps and will examine their causes, consequences, resultant corrective actions, and lessons learned. Most undesired outcomes usually do not occur because of a single event, but rather from a series of events and actions involving equipment malfunctions and/or human factors. This book comprises a series of case studies focusing mostly on accidents and incidents involving experimental aircraft. The information provided should be of use to flight-test organizations, aircraft operators, educators, and students, among others. These lessons are not unique to the UAS environment and are also applicable to human aviation and space flight activities. Common elements include crew resource management, training, mission planning issues, management and programmatic pressures (e.g., schedule, budget, resources), cockpit/control station design, and other factors. (Contains copyright material)

Civil Avionics Systems, Second Edition is an updated and in-depth practical guide to integrated avionic systems as applied to civil aircraft. This new edition has been expanded to include the latest developments in modern avionics. It describes avionic systems and potential developments in the field to help educate students and practitioners in the process of designing, building, and operating modern aircraft in the contemporary aviation system. Integration is a predominant theme of the book, since even as aircraft systems are becoming more integrated and complex, so are the economic, political, and technical environments in which they operate. Key features: content that is based on many years of practical industrial experience by the authors on a range of civil and military projects; focus on the integration and interconnectedness of systems in modern complex aircraft; updated contents in light of latest applications; and, substantial new material on avionics technology, software, and system safety. The authors are all recognized experts, and between them have over 140 years of experience in the aircraft industry. Their direct and accessible style ensures that Civil Avionics Systems, Second Edition is a must-have guide to integrated avionic systems in modern aircraft for aerospace students and practitioners.