Module 1: Introduction to Flight
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Feuling® Reaper® Series Camshafts for Milwaukee Eight Grinds: 405, 465, 508, 521
FEULING® REAPER® SERIES CAMSHAFTS FOR MILWAUKEE EIGHT GRINDS: 405, 465, 508, 521, 592 • FEULING® REAPER® camshafts have wide lobe separations producing very wide power bands • Smooth camshaft lobe ramps are easier on valve-train components eliminating excessive valve-train noise and wear. • Better Throttle Response - Increased MPG - Easy Starting - Unique Idle Sound • Made in U.S.A. 405 CAM - A workhorse, producing a wide powerband increasing torque and HP throughout the entire RPM range when compared to stock. Direct bolt in replacement for Milwaukee Eight engines, can be used with stock valve springs, pushrods, lifters and exhaust. Will respond well with slip-on mufflers and or complete exhaust system and a high flow air cleaner. Note Feuling recommends using mufflers with smaller cores for best lower RPM power and pull. Part # 1340 Valve Lift Open Close Duration @ 50" lift @ TDC Lobe Centerline Intake .395 4 ATDC 24 ABDC 200 .068 103 Exhaust .405 36 BBDC 11 BTDC 205 .049 108 RPM range: 1,700 - 5,700 Grind: 405 Overlap: 7 465 CAM - The 465 Reaper is an accelerator, producing solid bottom end performance with substantial gains above 2,800 RPM when compared to stock. This direct bolt in replacement for Milwaukee Eight engines can be used with stock valve springs, pushrods, lifters and exhaust. Will respond well with slip-on mufflers and or performance exhaust system and air cleaner. Use of performance valve-springs is not required but may result in a quieter, smoother running valve-train See Feuling #1107. This cam will also respond well with increased bore and or compression Part #1343 Valve Lift Open Close Duration @ 50" lift @ TDC Lobe Centerline Intake .445 4 BTDC 23 ABDC 207 .100 99.5 Exhaust .465 50 BBDC 6 ATDC 236 .100 112 RPM range: 1,850 - 5,950 Grind: 465 Overlap: 10 521 CAM - Aggressive pulling power with a "nasty" sound, the REAPER 521 grind will shine in 114" and larger cubic inch engines with added compression ratio. -
Download Video Products and Analyze Mission Results from Reapers Or Any Other Intelligence, Surveillance, and Reconnaissance Aircraft Supported by a Distributed Crew
Disclaimer The views expressed in this article are those of the author and do not reflect the official policy or position of the United States Air Force, Department of Defense, or the US Government. 2 The MQ-9 Reaper Remotely Piloted Aircraft: Humans and Machines in Action by Timothy M. Cullen Submitted to the Engineering Systems Division on August 12, 2011 in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy in Engineering Systems: Technology, Management, and Policy Abstract Remotely piloted aircraft and the people that control them are changing how the US military operates aircraft and those who fly, yet few know what “drone” operators actually do, why they do what they do, or how they shape and reflect remote air warfare and human-machine relationships. What do the remote operators and intelligence personnel know during missions to “protect and avenge” coalition forces in Iraq and Afghanistan and how do they go about knowing what they know? In an ethnographic and historical analysis of the Air Force’s preeminent weapon system for the counterinsurgencies in the two countries, this study describes how social, technical, and cognitive factors mutually constitute remote air operations in war. Armed with perspectives and methods developed in the fields of the history of technology, sociology of technology, and cognitive anthropology, the author, an Air Force fighter pilot, describes how distributed crews represent, transform, and propagate information to find and kill targets and traces the observed human and machine interactions to policy assumptions, professional identities, employment concepts, and technical tools. In doing so, he shows how the people, practices, and machines associated with remotely piloted aircraft have been oriented to and conditioned by trust in automation, experience, skill, and social interactions and how they have influenced and reflected the evolving operational environment, encompassing organizations, and communities of practice. -
Tethered Fixed-Wing Aircraft to Lift Payloads…
Tethered Fixed-Wing Aircraft to Lift Payloads: A Concept Enabled by Electric Propulsion David Rancourt Etienne Demers Bouchard Université de Sherbrooke Georgia Institute of Technology 3000 boul. Université – Pavillon P2 275 Ferst Drive NW Sherbrooke, QC Atlanta, GA CANADA USA [email protected] [email protected] Keywords: Electric propulsion, novel aircraft concept, VTOL, hybrid-electric powertrain ABSTRACT Helicopters have been essential to the military as they have been one of the only solutions for air-transporting substantial payloads with no need for complex mile-long runway infrastructures. However, they are fundamentally limited with high fuel consumption and reduced range. A disruptive concept to vertical lift uses tethered fixed-wing aircraft to lift a payload, where multiple aircraft collaborate and fly along a near circular flight path in hover. The Electric-Powered Reconfigurable Rotor concept (EPR2) leverages the recent progress in electric propulsion and modern controls to enable efficient load lifting using fixed-wing aircraft. The novel idea is to replace tethered manned aircraft (with onboard energy, fuel) with electric-powered fixed-wing aircraft with remote energy source to enable efficient collaborative load lifting. This paper presents the conceptual design of a heavy-lifting aircraft concept using electric-powered tethered fixed-wing aircraft for a ~30 metric ton lifting capability. A physics-based multidisciplinary design and simulation environment is used to predict the performance and optimize the aircraft flight path. It is demonstrated that this concept could hover with only 3.01 MW of power yet be able to translate to over 80 kts with minimal power increase by leveraging the benefits of complex non-circular flight paths. -
Sculptor Nina Slobodinskaya (1898-1984)
1 de 2 SCULPTOR NINA SLOBODINSKAYA (1898-1984). LIFE AND SEARCH OF CREATIVE BOUNDARIES IN THE SOVIET EPOCH Anastasia GNEZDILOVA Dipòsit legal: Gi. 2081-2016 http://hdl.handle.net/10803/334701 http://creativecommons.org/licenses/by/4.0/deed.ca Aquesta obra està subjecta a una llicència Creative Commons Reconeixement Esta obra está bajo una licencia Creative Commons Reconocimiento This work is licensed under a Creative Commons Attribution licence TESI DOCTORAL Sculptor Nina Slobodinskaya (1898 -1984) Life and Search of Creative Boundaries in the Soviet Epoch Anastasia Gnezdilova 2015 TESI DOCTORAL Sculptor Nina Slobodinskaya (1898-1984) Life and Search of Creative Boundaries in the Soviet Epoch Anastasia Gnezdilova 2015 Programa de doctorat: Ciències humanes I de la cultura Dirigida per: Dra. Maria-Josep Balsach i Peig Memòria presentada per optar al títol de doctora per la Universitat de Girona 1 2 Acknowledgments First of all I would like to thank my scientific tutor Maria-Josep Balsach I Peig, who inspired and encouraged me to work on subject which truly interested me, but I did not dare considering to work on it, although it was most actual, despite all seeming difficulties. Her invaluable support and wise and unfailing guiadance throughthout all work periods were crucial as returned hope and belief in proper forces in moments of despair and finally to bring my study to a conclusion. My research would not be realized without constant sacrifices, enormous patience, encouragement and understanding, moral support, good advices, and faith in me of all my family: my husband Daniel, my parents Andrey and Tamara, my ount Liubov, my children Iaroslav and Maria, my parents-in-law Francesc and Maria –Antonia, and my sister-in-law Silvia. -
Producing a Past: Cyrus Mccormick's Reaper from Heritage to History
Loyola University Chicago Loyola eCommons Dissertations Theses and Dissertations 2014 Producing a Past: Cyrus Mccormick's Reaper from Heritage to History Daniel Peter Ott Loyola University Chicago Follow this and additional works at: https://ecommons.luc.edu/luc_diss Part of the United States History Commons Recommended Citation Ott, Daniel Peter, "Producing a Past: Cyrus Mccormick's Reaper from Heritage to History" (2014). Dissertations. 1486. https://ecommons.luc.edu/luc_diss/1486 This Dissertation is brought to you for free and open access by the Theses and Dissertations at Loyola eCommons. It has been accepted for inclusion in Dissertations by an authorized administrator of Loyola eCommons. For more information, please contact [email protected]. This work is licensed under a Creative Commons Attribution-Noncommercial-No Derivative Works 3.0 License. Copyright © 2014 Daniel Peter Ott LOYOLA UNIVERSITY CHICAGO PRODUCING A PAST: CYRUS MCCORMICK’S REAPER FROM HERITAGE TO HISTORY A DISSERTATION SUBMITTED TO THE FACULTY OF THE GRADUATE SCHOOL IN CANDIDACY FOR THE DEGREE OF DOCTOR OF PHILOSOPHY JOINT PROGRAM IN AMERICAN HISTORY / PUBLIC HISTORY BY DANIEL PETER OTT CHICAGO, ILLINOIS MAY 2015 Copyright by Daniel Ott, 2015 All rights reserved. ACKNOWLEDGMENTS This dissertation is the result of four years of work as a graduate student at Loyola University Chicago, but is the scholarly culmination of my love of history which began more than a decade before I moved to Chicago. At no point was I ever alone on this journey, always inspired and supported by a large cast of teachers, professors, colleagues, co-workers, friends and family. I am indebted to them all for making this dissertation possible, and for supporting my personal and scholarly growth. -
History of Solar Flight July 2008
History of Solar Flight July 2008 solar airplane aircraft continuous sustainable flight solar-powered solar cells mppt helios Sky-Sailor sun-powered HALE platform solaire avion vol continu dévelopement durable énergie solaire cellules plateforme History of Solar flight André Noth, [email protected] Autonomous Systems Lab, Swiss Federal Institute of Technology Zürich 1. The conjunction of two pioneer fields, electric flight and solar cells The use of electric power for flight vehicles propulsion is not new. The first one was the hydrogen- filled dirigible France in year 1884 that won a 10 km race around Villacoulbay and Medon. At this time, the electric system was superior to its only rival, the steam engine but then with the arrival of gasoline engines, work on electrical propulsion for air vehicles was abandoned and the field lay dormant for almost a century [2]. On the 30th June 1957, Colonel H. J. Taplin of the United Kingdom made the first officially recorded electric powered radio controlled flight with his model “Radio Queen”, which used a permanent-magnet motor and a silver-zinc battery. Unfortunately, he didn’t carry on these experiments. Further developments in the field came from the great German pioneer, Fred Militky, who first achieved a successful flight with a Radio Queen, 1957 free flight model in October 1957. Since this premises, electric flight continuously evolved with constant improvements in the fields of motors and batteries [12]. Three years before Taplin and Militky’s experiments, in 1954, photovoltaic technology was born at Bell Telephone Laboratories. Daryl Chapin, Calvin Fuller, and Gerald Pearson developed the first silicon photovoltaic cell capable of converting enough of the sun’s energy into power to run everyday electrical Gerald Pearson, Daryl Chapin equipment. -
Simone Weil Durante Il Soggiorno a New York, Tra Luglio E Ottobre Del 1942 - Ec Cetto Le Annotazioni Raccolte in Un Taccui No a Londra Negli Ultimi Mesi Di Vita
I testi che compongono questo quarto e ul timo volume dei Quaderni furono scritti da Simone Weil durante il soggiorno a New York, tra luglio e ottobre del 1942 - ec cetto le annotazioni raccolte in un taccui no a Londra negli ultimi mesi di vita. Pub blicati nel 1950 da Gallimard con il titolo La connaissance surnaturelle, vengono ora ri proposti per la prima volta in una sequenza rigorosa e completa. Dato il carattere la cunoso dell’edizione francese, nella quale fra l’altro non ci si è preoccupati di segna re il passaggio da un quaderno all’altro, né di rispettarne la successione cronologica, si è infatti preferito fondare la traduzione su un accurato studio dei manoscritti. Questi testi si presentano, anche formal mente, come la continuazione dei quaderni di Marsiglia. Ma ora la riflessione tende a concentrarsi progressivamente intorno ad alcuni nuclei tematici spesso svolti in an notazioni piuttosto lunghe, con un proce dimento di scrittura più prossimo a un’ar ticolazione per brevi capitoli che non al l’andamento frammentato dei precedenti quaderni. In particolare, mai come in que sto periodo il pensiero della Weil si appun ta sul significato della favola e dei miti, esercitandosi su testi delle più svariate tra dizioni — e proprio in questa zona si in contreranno alcune intuizioni folgoranti, per esempio sulla simbolica zodiacale. Il volume si chiude con un completo ap parato di indici relativi all’intera compa gine dei Quaderni: degli autori e opere cita ti e commentati; dei personaggi storici e leggendari, luoghi, popoli, entità, esseri di vini; delle figure, immagini, parole. -
Air-Breathing Engine Precooler Achieves Record-Breaking Mach 5 Performance 23 October 2019
Air-breathing engine precooler achieves record-breaking Mach 5 performance 23 October 2019 The Synergetic Air-Breathing Rocket Engine (SABRE) is uniquely designed to scoop up atmospheric air during the initial part of its ascent to space at up to five times the speed of sound. At about 25 km it would then switch to pure rocket mode for its final climb to orbit. In future SABRE could serve as the basis of a reusable launch vehicle that operates like an aircraft. Because the initial flight to Mach 5 uses the atmospheric air as one propellant it would carry much less heavy liquid oxygen on board. Such a system could deliver the same payload to orbit with a vehicle half the mass of current launchers, potentially offering a large reduction in cost and a higher launch rate. Reaction Engines' specially constructed facility at the Colorado Air and Space Port in the US, used for testing the innovative precooler of its air-breathing SABRE engine. Credit: Reaction Engines Ltd UK company Reaction Engines has tested its innovative precooler at airflow temperature conditions equivalent to Mach 5, or five times the speed of sound. This achievement marks a significant milestone in its ESA-supported Airflow through the precooler test item in the HTX heat exchanger test programme. UK company Reaction development of the air-breathing SABRE engine, Engines has tested its innovative precooler at airflow paving the way for a revolution in space access temperature conditions equivalent to Mach 5, or five and hypersonic flight. times the speed of sound. This achievement marks a significant milestone in the ESA-supported development The precooler heat exchanger is an essential of its air-breathing SABRE engine, paving the way for a SABRE element that cools the hot airstream revolution in hypersonic flight and space access. -
Design of a Micro-Aircraft Glider
Design of A Micro-Aircraft Glider Major Qualifying Project Report Submitted to the faculty of WORCESTER POLYTECHNIC INSTITUTE In partial fulfillment of the requirements for The Degree of Bachelor of Science Submitted by: ______________________ ______________________ Zaki Akhtar Ryan Fredette ___________________ ___________________ Phil O’Sullivan Daniel Rosado Approved by: ______________________ _____________________ Professor David Olinger Professor Simon Evans 2 Certain materials are included under the fair use exemption of the U.S. Copyright Law and have been prepared according to the fair use guidelines and are restricted from further use. 3 Abstract The goal of this project was to design an aircraft to compete in the micro-class of the 2013 SAE Aero Design West competition. The competition scores are based on empty weight and payload fraction. The team chose to construct a glider, which reduces empty weight by not employing a propulsion system. Thus, a launching system was designed to launch the micro- aircraft to a sufficient height to allow the aircraft to complete the required flight by gliding. The rules state that all parts of the aircraft and launcher must be contained in a 24” x 18” x 8” box. This glider concept was unique because the team implemented fabric wings to save substantial weight and integrated the launcher into the box to allow as much space as possible for the aircraft components. The empty weight of the aircraft is 0.35 lb, while also carrying a payload weight of about 0.35 lb. Ultimately, the aircraft was not able to complete the required flight because the team achieved 50% of its desired altitude during tests. -
Actuator Saturation Analysis of a Fly-By-Wire Control System for a Delta-Canard Aircraft
DEGREE PROJECT IN VEHICLE ENGINEERING, SECOND CYCLE, 30 CREDITS STOCKHOLM, SWEDEN 2020 Actuator Saturation Analysis of a Fly-By-Wire Control System for a Delta-Canard Aircraft ERIK LJUDÉN KTH ROYAL INSTITUTE OF TECHNOLOGY SCHOOL OF ENGINEERING SCIENCES Author Erik Ljudén <[email protected]> School of Engineering Sciences KTH Royal Institute of Technology Place Linköping, Sweden Saab Examiner Ulf Ringertz Stockholm KTH Royal Institute of Technology Supervisor Peter Jason Linköping Saab Abstract Actuator saturation is a well studied subject regarding control theory. However, little research exist regarding aircraft behavior during actuator saturation. This paper aims to identify flight mechanical parameters that can be useful when analyzing actuator saturation. The studied aircraft is an unstable delta-canard aircraft. By varying the aircraft’s center-of- gravity and applying a square wave input in pitch, saturated actuators have been found and investigated closer using moment coefficients as well as other flight mechanical parameters. The studied flight mechanical parameters has proven to be highly relevant when analyzing actuator saturation, and a simple connection between saturated actuators and moment coefficients has been found. One can for example look for sudden changes in the moment coefficients during saturated actuators in order to find potentially dangerous flight cases. In addition, the studied parameters can be used for robustness analysis, but needs to be further investigated. Lastly, the studied pitch square wave input shows no risk of aircraft departure with saturated elevons during flight, provided non-saturated canards, and that the free-stream velocity is high enough to be flyable. i Sammanfattning Styrdonsmättning är ett välstuderat ämne inom kontrollteorin. -
The Design and Development of a Human-Powered
THE DESIGN AND DEVELOPMENT OF A HUMAN-POWERED AIRPLANE A THESIS Presented to the Faculty of the Graduate Division "by James Marion McAvoy^ Jr. In Partial Fulfillment of the Requirements for the Degree Master of Science in Aerospace Engineering Georgia Institute of Technology June _, 1963 A/ :o TEE DESIGN AND DETERMENT OF A HUMAN-POWERED AIRPLANE Approved: Pate Approved "by Chairman: M(Ly Z7. /q£3 In presenting the dissertation as a partial fulfillment of the requirements for an advanced degree from the Georgia Institute of Technology, I agree that the Library of the Institution shall make it available for inspection and circulation in accordance with its regulations governing materials of this type. I agree that permission to copy from, or to publish from, this dissertation may he granted by the professor under whose direction it was written, or, in his absence, by the dean of the Graduate Division when such copying or publication is solely for scholarly purposes and does not involve potential financial gain. It is under stood that any copying from, or publication of, this disser tation which involves potential financial gain will not be allowed without written permission. i "J-lW* 11 ACKNOWLEDGMENTS The author wishes to express his most sincere appreciation to Pro fessor John J, Harper for acting as thesis advisor, and for his ready ad vice at all times. Thanks are due also to Doctor Rohin B. Gray and Doctor Thomas W. Jackson for serving on the reading committee and for their help and ad vice . Gratitude is also extended to,all those people who aided in the construction of the MPA and to those who provided moral and physical sup port for the project. -
Stabilizer PLUS 7-Channel Receiver Essential Instructions
Lemon RX Stabilizer PLUS Receiver – Essential Instructions v1.1 Lemon RX Stabilizer PLUS 7-Channel Receiver Essential Instructions Contents Introducing the Lemon StabPLUS ............................................................................................................ 2 Functions ........................................................................................................................................................ 2 Transmitter Requirements .............................................................................................................................. 2 Servos and Power Sources .............................................................................................................................. 3 Setting up the StabPLUS ......................................................................................................................... 4 Installation ...................................................................................................................................................... 4 Binding ............................................................................................................................................................ 5 Setting Failsafe ................................................................................................................................................ 5 Test Flying .............................................................................................................................................. 6 Preparing