DOCSLIB.ORG

Flight Manual

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Flight Manual for DCS World Flight Manual AVIODEV INDEX FOREWORD ................................................................................................................................... 7 1. INTRODUCTION ..................................................................................................................... 9 2. AIRCRAFT CHARACTERISTICS ............................................................................................... 15 2.1. AIRCRAFT DIMENSIONS ............................................................................................... 16 o Basic Dimensions ......................................................................................................... 16 2.2. SPECIFICATIONS........................................................................................................... 16 o Wing Specifications ..................................................................................................... 16 o Horizontal Stabilizer Specifications ............................................................................. 16 o Vertical Stabilizer Specification ................................................................................... 16 o Airbrake ....................................................................................................................... 16 2.3. WEIGHTS ..................................................................................................................... 16 3. AIRCRAFT SYSTEMS ............................................................................................................. 19 3.1. FRONT COCKPIT CONTROLS AND INDICATORS ........................................................... 19 Forward Lower Panel .......................................................................................................... 21 Forward Left Panel .............................................................................................................. 21 Forward Right Panel ............................................................................................................ 22 Left Side Panel ..................................................................................................................... 22 Right Side Panel ................................................................................................................... 23 3.2. REAR COCKPIT CONTROLS AND INDICATORS .............................................................. 24 3.3. POWER PLANT ............................................................................................................. 25 Engine Fuel System.............................................................................................................. 27 Anti-Surge Device ................................................................................................................ 27 Engine Anti-Ice System ........................................................................................................ 27 Engine Oil System ................................................................................................................ 27 Engine Starting System ........................................................................................................ 27 Engine Control Panel ........................................................................................................... 27 Engine Controls and Indicators ........................................................................................... 29 Engine Ignition System ........................................................................................................ 32 3.4. AIRCRAFT FUEL SYSTEM .............................................................................................. 33 Transfer System ................................................................................................................... 34 Boost System ....................................................................................................................... 34 Fuel Quantity Indicating System ......................................................................................... 35 2 AVIODEV 3.5. ELECTRICAL SYSTEM .................................................................................................... 38 Starter-Generator ................................................................................................................ 38 Batteries .............................................................................................................................. 38 DC Distribution System ....................................................................................................... 40 AC Distribution System ........................................................................................................ 41 Inverters .............................................................................................................................. 41 Circuit Breaker Panels ......................................................................................................... 43 3.6. HYDRAULIC SYSTEM .................................................................................................... 44 Hydraulic Pressure Indicators.............................................................................................. 44 Hydraulic Pressure Warning Lights ..................................................................................... 45 3.7. FLIGHT CONTROLS ....................................................................................................... 46 Ailerons ............................................................................................................................... 46 Elevators .............................................................................................................................. 46 Aileron and Elevator Trim System ....................................................................................... 47 Control Sticks ....................................................................................................................... 48 Rudder Control .................................................................................................................... 48 Wing Flaps ........................................................................................................................... 49 Speed Brake ......................................................................................................................... 50 3.8. LANDING GEAR SYSTEM .............................................................................................. 52 Landing Gear Levers ............................................................................................................ 52 Landing Gear Position Indicators ........................................................................................ 52 Landing Gear Caution Lights/Audible Signal Buttons .......................................................... 52 Emergency Gear Extension Handles ................................................................................... 52 Emergency Gear Retraction Button (Crash Button) ............................................................ 53 3.9. WHEEL BRAKE SYSTEM ................................................................................................ 53 Anti-Skid System .................................................................................................................. 53 Parking/Emergency Brake System ...................................................................................... 54 Parking/Emergency Brake Handles ..................................................................................... 54 3.10. STALL WARNING SYSTEM ........................................................................................ 54 Stall Caution Light ................................................................................................................ 54 Stall Warning Switches ........................................................................................................ 54 Stall Warning Test Switches ................................................................................................ 54 3.11. PITOT STATIC SYSTEM ............................................................................................. 55 Pitot Heat Switches ............................................................................................................. 55 Pitot Heat Caution Light ...................................................................................................... 55 3 AVIODEV 3.12. INSTRUMENTS ......................................................................................................... 55 Mach/Airspeed Indicators ................................................................................................... 56 Turn and Slip Indicators ....................................................................................................... 56 Vertical Speed Indicator (VSI) .............................................................................................. 57 Standby Artificial Horizons .................................................................................................. 57 Altitude-Encoding Altimeter ............................................................................................... 58 Altimeter ............................................................................................................................
Load more

Recommended publications
  • (12) United States Patent (10) Patent No.: US 8,869,504 B1 Schwarz Et Al
    USOO88695 04B1 (12) United States Patent (10) Patent No.: US 8,869,504 B1 Schwarz et al. (45) Date of Patent: Oct. 28, 2014 (54) GEAREDTURBOFAN ENGINE GEARBOX 5.431,539 A 7/1995 Carvalho ARRANGEMENT 5,443,365 A * 8/1995 Ingling et al. ............. 416, 193A 5,778,659 A 7/1998 Duesler et al. 6,464,401 B1 10/2002 Allard (71) Applicant: United Technologies Corporation, 7,144.221 B2 * 12/2006 Giffin ............................ 416,189 Hartford, CT (US) 8,137,070 B2 * 3/2012 Van Houten ... 416,189 2006.0024162 A1* 2, 2006 Giffin .......... ... 415,208.3 (72) Inventors: Frederick M. Schwarz, Glastonbury, 2007/015.1258 A1* 7/2007 Gaines et al. ................... 60,792 CT (US); William G. Sheridan, 2008/00987.17 A1* 5, 2008 Orlando et al. .... ... 60,226.1 Southington, CT (US) 2010/0218478 A1* 9/2010 Merry et al. .................... 60,205 glon, 2011/0056208 A1 3/2011 Norris et al. .................... 6Of772 2011/O123326 A1 5/2011 DiBenedetto et al. (73) Assignee: United Technologies Corporation, 2012/0110979 A1* 5, 2012 Rosenkrans et al. ......... 60,226.1 Hartford, CT (US) 2012fO251306 A1* 10/2012 Reinhardt et al. ......... 415, 1821 2012fO263579 A1* 10, 2012 Otto et al. .......... ... 415,124.2 (*) Notice: Subject to any disclaimer, the term of this 2012/0291449 A1* 11/2012 Adams et al. ................... 60,793 2012/03 15130 A1 12/2012 Hasel et al. patent is extended or adjusted under 35 2013, OO25257 A1 1/2013 Suciu et all U.S.C. 154(b) by 0 days. 2013/0025258 A1* 1/2013 Merry et al.
    [Show full text]
  • Anteproyecto De Una Aeronave
    CENTRO UNIVERSITARIO DE LA DEFENSA ACADEMIA GENERAL DEL AIRE ANTEPROYECTO DE UNA AERONAVE AERONAVE DE ENTRENAMIENTO AVANZADO Trabajo Fin de Grado Autor: A. A. D. Rafael Ángel Reyes Rodríguez (LXVI – CGEA-EOF) Director: José Serna Serrano Co-director: Francisco Javier Sánchez Velasco Grado en Ingeniería en Organización industrial Curso: 2014/2015 – convocatoria: junio Tribunal nombrado por la dirección del Centro Universitario de la Defensa de San Javier, el día ____ de ____________ de 20____. Presidente: Dr. D. Manuel Caravaca Garratón Secretario: Dr. D. Alejandro López Belchí Vocal: Col. Dr. Andrés Dolón Payán Realizado el acto de defensa del Trabajo Fin de Grado, el día____ de _________ de 20____, en el Centro Universitario de la Defensa de San Javier. Calificación: __________________________. EL PRESIDENTE EL SECRETARIO EL VOCAL ANTEPROYECTO DE UNA AERONAVE AERONAVE DE ENTRENAMIENTO AVANZADO RESUMEN: Este trabajo trata de plasmar en su desarrollo el anteproyecto de una hipotética aeronave de entrenamiento avanzado. En él se busca encontrar una solución de compromiso al estado del arte actual, a partir del cálculo de los parámetros definitorios básicos de dicha aeronave, incluida la polar del avión. Para ello se acude a las referencias señaladas en busca de las herramientas necesarias para el establecimiento de los valores aerodinámicos y motrices deseados. Como producto final se obtiene un compendio de constantes que nos permite evaluar las características diferenciadoras de la aeronave con las ya existentes. ABSTRACT: This work tries to develop a conceptual advanced jet trainer design for a hypothetical aircraft. It seeks to find a compromise solution to the current state of the art, from the calculation of the basic parameters defining the aircraft, including polar aircraft.
    [Show full text]
  • Usafalmanac ■ Gallery of USAF Weapons
    USAFAlmanac ■ Gallery of USAF Weapons By Susan H.H. Young The B-1B’s conventional capability is being significantly enhanced by the ongoing Conventional Mission Upgrade Program (CMUP). This gives the B-1B greater lethality and survivability through the integration of precision and standoff weapons and a robust ECM suite. CMUP will include GPS receivers, a MIL-STD-1760 weapon interface, secure radios, and improved computers to support precision weapons, initially the JDAM, followed by the Joint Standoff Weapon (JSOW) and the Joint Air to Surface Standoff Missile (JASSM). The Defensive System Upgrade Program will improve aircrew situational awareness and jamming capability. B-2 Spirit Brief: Stealthy, long-range, multirole bomber that can deliver conventional and nuclear munitions anywhere on the globe by flying through previously impenetrable defenses. Function: Long-range heavy bomber. Operator: ACC. First Flight: July 17, 1989. Delivered: Dec. 17, 1993–present. B-1B Lancer (Ted Carlson) IOC: April 1997, Whiteman AFB, Mo. Production: 21 planned. Inventory: 21. Unit Location: Whiteman AFB, Mo. Contractor: Northrop Grumman, with Boeing, LTV, and General Electric as principal subcontractors. Bombers Power Plant: four General Electric F118-GE-100 turbo fans, each 17,300 lb thrust. B-1 Lancer Accommodation: two, mission commander and pilot, Brief: A long-range multirole bomber capable of flying on zero/zero ejection seats. missions over intercontinental range without refueling, Dimensions: span 172 ft, length 69 ft, height 17 ft. then penetrating enemy defenses with a heavy load Weight: empty 150,000–160,000 lb, gross 350,000 lb. of ordnance. Ceiling: 50,000 ft. Function: Long-range conventional bomber.
    [Show full text]
  • Aerodynamic Performance Analysis of a Low-Speed Acrobatic Airplane by Numerical Simulation
    0HFiQLFD&RPSXWDFLRQDO9RO;;, SS± 65,GHOVRKQ 9(6RQ]RJQLDQG$&DUGRQD!(GV" 6DQWD)H±3DUDQi $UJHQWLQD 2FWREHU AERODYNAMIC PERFORMANCE ANALYSIS OF A LOW-SPEED ACROBATIC AIRPLANE BY NUMERICAL SIMULATION Andres D. Ortiz*, Luis E. Quiroz*, Rodolfo A. Köck† *University of Concepción Department of Mechanical Engineering Edmundo Larenas 234, Barrio Universitario, Concepción, Chile Casilla 160-C, correo 3 Concepción e-mail: [email protected] , [email protected] , http://www.dim.udec.cl †Cadetech S.A. Fluid-Dynamics Division Serrano 551 of. 208, Concepción, Chile e-mail: [email protected] , http://www.cadetech.cl Keywords: numerical, simulation, acrobatic airplane, aerodynamic, performance, analysis, FLUENT® code. Abstract. The goal of this work is to simulate and to analyze, by means of the CFD commercial code FLUENT®, the flow around a low-speed acrobatic airplane, the ENAER T- 35 PILLAN, with similar characteristics to the most light civil airplanes, widely used anywhere in the world. Specifically, the aerodynamic loads on the structure are required, specifying the critical conditions of flight and the consequent load distributions on the airplane according to the application of norm FAR-23. Finally, the worst flight conditions happen at the cruise speed (Mach 0.25) and maximum load factor. In this condition the lift and drag forces, bending and torsion moments at the main spar of the wing are maximum, even greater than for the highest speed of flight (Mach 0.37). Finally, a series of graphs were made to considering the maximum loads on the wing as function of the speed of flight and the angle of attack. ***************************************************************** $'2UWL] /(4XLUR]DQG5$.|FN 1 NOMENCLATURE 1.1 General symbols AR Aspect Ratio, dimensionless.
    [Show full text]
  • Combat Aircraft Team; the US Air Force Air Power Yearbook Is the Ultimate Guide to the World’S Most Powerful Air Arm
    Advanced jet TRAINING ALENIA AERMACCHI M-346 • ISRAELI SKYHAWK RETIREMENT • PACER CLASSIC T-38 TALONS • GREEK BUCKEYES AND TEXAN IIS Volume 17 • Number 3 AMERICA’S BESTSELLING MILITARY AVIATION MAGAZINE combataircraft.net EAGLE FROM THE COCKPIT Pilot stories from the mighty F-15C ‘Desert Storm’ 25 years ON F-15C victories IN THE NEWS: USAF Saves the a-10 SIKORSKY CH-53K C-5 SUPER GALAXY KING STALLION AT DOVER AFB S-3 Vikings BOW OUT OF UK £4.50 SERVICE WITH VX-30 CHINESE FIGHTER BOMBER REVIEW MARCH 2016 SPECIAL united states air force air power YEARBOOK 2016 Produced by the Combat Aircraft team; the US Air Force Air Power Yearbook is the ultimate guide to the world’s most powerful air arm. Packed with features on latest aircraft capabilities, famous squadrons and the personnel that fly and maintain the various types, plus a detailed unit and aircraft air power review. This 100-page publication is a must-have for USAF aviation fans. FEATURING: F-22 on the front line A review of the Raptor’s combat debut over Syria and recent deployment to Europe. 40 Years of exercise’ Red Flag’ A review and tribute to the world’s most famous exercise. Bayou Militia A unit review of the F-15Cs of the 122nd Fighter Squadron Louisiana ANG F-35 training Behind the scenes at Eglin and Luke AFB as the F-35 training squadrons get up to full speed. B-1 today Exclusive interviews with B-1 senior officers as we detail recent combat operations and latest JUST upgrades for the B-1 Lancer.
    [Show full text]
  • F-16 Barak Strike 17
    N O 1 9 Y EY EA RA 1 0 A P R I L 2 0 1 8 STRIKE 17 CROATIAN AIR THE LARGEST FORCE TO RECEIVE EXERCISE OF F-16 BARAK 2017 FIGHTER AIRCRAFT interview VICE ADMIRAL COLIN J. KILRAIN NATO SPECIAL OPERATIONS CYBER HEADQUARTERS SHIELD 2018 THE READINESS IMPERATIVE Cover by Tomislav Brandt IN THIS ISSUE croatian air force Edited by: Vesna PINTARIĆ, Photo: Tomislav BRANDT croatian military magazine The Republic of Croatia has faced one of its most impor- tant and complex strategic decisions involving its defence sector since the 1991-95 Homeland War. It had to choose between retaining the capability to monitor and protect its sovereign air space, or losing that control and thus renouncing the nation’s full sovereignty. Drawing upon its experiences from the Homeland War, in which air force USAF/WikimediaFoto: Commons played a decisive role, the only logical conclusion was that investing in fighter aircraft today meant investing in the future and security of Croatia, and a pre-condition of its stability and future economic development. AT ITS SESSION OF 29 MARCH 2018, THE GOVERNMENT OF THE REPUBLIC OF CROATIA ADOPTED THE DECISION ON THE PROCUREMENT OF A MULTI-ROLE FIGHTER AIRCRAFT, OPTING FOR THE LOCKHEED-MARTIN F-16C/D BLOCK 30 BARAK FROM THE STATE OF ISRAEL. IT REPRESENTS A HISTORIC DECISION FOR THE CROATIAN AIR FORCE... CROATIAN AIR FIGHTER FORCE TO RECEIVE F-16 BARAK AIRCRAFT 4 CROATIAN AIR FORCE 4 APRIL 2018 CROMIL CROMIL APRIL 2018 5 CROATIAN AIR FORCE TO RECEIVE F-16 BARAK FIGHTER AIRCRAFT 04-13_F-16_Barak.indd 4-5 PAGE27/04/2018 13:084 14 INTERVIEW VICE ADMIRAL COLIN J.
    [Show full text]
  • Taking Flight
    FROM THE COCKPIT IN THIS ISSUE >>> 03 BEHIND THE SCREENS : Alpha 3.5 Flight Model Update RSI MUSEUM : 13 The Past, Present & Future of Flight Controls GALACTAPEDIA : 27 Leyland’s Tortoise LORE FEATURE: 29 MaxOx ISSUE: 07 04 Editor: Ben Lesnick Copy Editor: Martin Driver Layout: Michael Alder FROM THE COCKPIT GREETINGS, CITIZENS! You might as well call this one “the flight issue!” was kind enough to give us a whole load of detail on Instead of focusing on the development of a particular the work that went into this one. Enjoy! ship, this time we’re looking at the development of flight itself. That’s because Alpha 3.5, now available We’ve been bouncing around ideas on how to to the community at large, introduces a major revamp relaunch the RSI Museum in Jump Point and hit on of Star Citizen’s complex flight model. The immortal an idea that seemed like it could be an interesting one: Townes Van Zandt sang that “to live is to fly,” and that a look at both the real-world history of something and couldn’t be more literal in the case of Star Citizen. To how important it is to the makeup of the ‘verse. So, this say that there’s been plenty of debate about the flight month’s Museum looks at the history of the HOTAS model since it first went public with Arena Commander through its real-world development in the 1950s for back in 2014 would be an understatement. While jet fighters, its adoption as the high-end flight setup the community has regularly provided invaluable of choice for gamers in the 90s, and then its use in feedback and the developers have continued to refine Human starships of the 30th century.
    [Show full text]
  • Mp-Msg-045-05
    Modeling & Simulation for Experimentation, Test & Evaluation and Training: Alenia Aeronautica Experiences and Perspectives Mrs. Marcella Guido Alenia Aeronautica Simulation & System’s Operability C.so Marche 41, 10146 Torino Italy [email protected] Mr. Cristiano Montrucchio Alenia Aeronautica Simulation & System’s Operability Manager C.so Marche, 41, 10146 Torino Italy [email protected] ABSTRACT The use of Modeling & Simulation to support aircraft development is nowadays common practice within any modern aeronautical industry, and a long term key capability of Alenia Aeronautica. Starting from such crucial role, M&S utilization has progressively expanded to effectively support the aeronautical system’s early stages – feasibility and definition, and later stages – in service support and pilots training, becoming an essential element during the entire system’s life cycle. The main tool to implement and sustain such capability is the Synthetic Environment, which relies on the following elements: • Flight Simulators with engineering and training potential • Simulators networking at both LAN and WAN (Local and Wide Area Network) levels • Tactical scenarios • Image generation • Virtual reality The paper will focus on the latest major experiences of Alenia Aeronautica with the AMX ACOL, Eurofighter, C-27J and Sky-X UAV Programs, from systems concept, through development and experimentation, to pilots training and mission rehearsal. Moreover, Alenia Aeronautica’s approach and perspectives in the field of the simulation of Network Centric Operations will be described: the Network Centric Simulation Environment 1.0 INTRODUCTION The use of Modeling & Simulation (M&S) in aerospace engineering is nowadays common practice within any modern aeronautical firm and a long term key capability of Alenia Aeronautica.
    [Show full text]
  • Helmet-Mounted Display Design Guide I Contract NAS2-14151
    Helmet-Mounted Display Design Guide Richard L. Newman and Kevin W. Greeley TR-97-11 3 November 1997 Crew Systems Post Office Box 963 San Marcos, Texas (512)-754-7733 REPORT DOCUMENTATION PAGE Form Approved OMB NO. 0704-0188 I -- Pu~licreporting burden for thls collection of lnformatlon IS estimated to average 1 hour per response~nclud~n~the tlme for reviewing instructions, searching exlstlna data sources 1 gather~noand malntalilnc? the data needed and Completlno and revlewlng the collection of informatlon Send comments reqardlnq thls burden estlmate or any othei aspect of this collect8on of informat~on.~nciud~n- suagestions for reducing tiiir burden to Washington Headquarters Services, Directorate Tor lnf6rmation Operations and Remns, 1215 Jefferson 1 Davis Hlohway, Su~te1204. Arlinat&, \j& 22202.43132, and to tn.0 Off~ceof Manaaem-nt and Budae?. Paoerwork Reduction Proiect. (0704-0188).. Washlnaton. DC 20503 1 1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3. REPORT TYPE AND DAT S COVERED 3 November 1997 Eontractor Report 1I 1I 14. TITLE AND SUBTITLE 5. FUNDING NUMBERS I Helmet-Mounted Display Design Guide I Contract NAS2-14151 Richard L. Newman and Kevin W. Greeley I I I 7. PERFORMING ORGANIZATION NAMEIS) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION REPORT NUMBER 1 Crew Systems Post Office Box 963 San Marcos, Texas 78667 I 9. SPONSORINGIMONlTORlMG AGENCY NAME(S) AND ADDRESS(E5) 10. SPONSORING IMONIJORING AGENCY REPORT NUMBER Aeroflightdynamics Directorate I Ames Research Center Moffett Field, California 94035 11. SUPPLEMENTARY NOTES 12a. DISTRIBUTION I AVAILABILITY STATEMENT 12b. DISTRIBUTION CODE Unclassified-Unlimited I 13. AESTRACT (Maximum 200 words) 1 Helmet-mounted d~splays(HMDs) present flight, navigation, and weapon information in the pilot's line of sight.
    [Show full text]
  • The Pratt & Whitney Purepower® Geared Turbofan™ Engine Overview
    9/27/2015 The Pratt & Whitney PurePower® Geared Turbofan™ Engine Alan Epstein VP, Technology and Environment Pratt & Whitney Academie de l’Air et de l’Espace Paris, September 2015 © 2015 United Technologies Corporation This document has been publicly released 1 Overview The Development of the Geared TurbofanTM Engine • Some historical perspective • A recurrent theme - conventional wisdom vs. reality • The roles of architecture, design, and technology • Speculation on the future © 2015 United Technologies Corporation This document has been publicly released 2 1 9/27/2015 PurePower® Geared Turbofan™ Engine © 2015 United Technologies Corporation This document has been publicly released 3 Why History? “There is nothing new in the world except the history you do not know.” Harry S. Truman © 2015 United Technologies Corporation This document has been publicly released 4 2 9/27/2015 Pratt & Whitney – Dependable Engines Wasp Pic Wasp Engine Turbofan Engine 1925 2015 © 2015 United Technologies Corporation This document has been publicly released 5 Eras of Engine Architecture Single Spool Dual Spool Turbojet High Bypass Turbofan Ultra-High Bypass (1937) (1951) (1969) Geared Turbofan (2015) >10% STEPS IN EFFICIENCY OVERALL EFFICIENCY EFFICIENCY OVERALL 1940 1960 1980 2000 2020 © 2015 United Technologies Corporation This document has been publicly released 6 3 9/27/2015 Geared Turbofan Technology Demonstrators Over 50 years of interest Hamilton Standard General Electric Lycoming ALF502 4 5 Pratt & Whitney PW304, 1957 Q-Fan, 19722 QCSEE, 1977 1980
    [Show full text]
  • Helmet-Mounted Display Design Guide I Contract NAS2-14151
    https://ntrs.nasa.gov/search.jsp?R=19980018292 2020-06-16T01:04:29+00:00Z Helmet-Mounted Display Design Guide Richard L. Newman and Kevin W. Greeley TR-97-11 3 November 1997 Crew Systems Post Office Box 963 San Marcos, Texas (512)-754-7733 REPORT DOCUMENTATION PAGE Form Approved OMB NO. 0704-0188 I -- Pu~licreporting burden for thls collection of lnformatlon IS estimated to average 1 hour per response~nclud~n~the tlme for reviewing instructions, searching exlstlna data sources 1 gather~noand malntalilnc? the data needed and Completlno and revlewlng the collection of informatlon Send comments reqardlnq thls burden estlmate or any othei aspect of this collect8on of informat~on.~nciud~n- suagestions for reducing tiiir burden to Washington Headquarters Services, Directorate Tor lnf6rmation Operations and Remns, 1215 Jefferson 1 Davis Hlohway, Su~te1204. Arlinat&, \j& 22202.43132, and to tn.0 Off~ceof Manaaem-nt and Budae?. Paoerwork Reduction Proiect. (0704-0188).. Washlnaton. DC 20503 1 1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3. REPORT TYPE AND DAT S COVERED 3 November 1997 Eontractor Report 1I 1I 14. TITLE AND SUBTITLE 5. FUNDING NUMBERS I Helmet-Mounted Display Design Guide I Contract NAS2-14151 Richard L. Newman and Kevin W. Greeley I I I 7. PERFORMING ORGANIZATION NAMEIS) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION REPORT NUMBER 1 Crew Systems Post Office Box 963 San Marcos, Texas 78667 I 9. SPONSORINGIMONlTORlMG AGENCY NAME(S) AND ADDRESS(E5) 10. SPONSORING IMONIJORING AGENCY REPORT NUMBER Aeroflightdynamics Directorate I Ames Research Center Moffett Field, California 94035 11. SUPPLEMENTARY NOTES 12a.
    [Show full text]
  • (12) United States Patent (10) Patent N0.2 US 8,402,742 B2 Roberge Et Al
    US008402742B2 (12) United States Patent (10) Patent N0.2 US 8,402,742 B2 Roberge et al. (45) Date of Patent: Mar. 26, 2013 (54) GAS TURBINE ENGINE SYSTEMS 4,005,575 A 2/1977 Scott et a1. INVOLVING TIP FANS 4,021,142 A 5/1977 Violette 4,043,121 A 8/1977 Thomas et al. (75) Inventors: Gary D. Roberge, Tolland, CT (US); i E2358 Gabriel L- 5119i“, Glastonbury, CT (Us) 4,964,844 A 10/1990 Bagnall 5,010,729 A 4/1991 Adamson et al. (73) Assignee: United Technologies Corporation, 5,182,905 A 2/1993 Stransky et 81. Hartford CT (Us) 5,388,964 A * 2/1995 Ciokajlo et al. ........... .. 60/226.1 ’ 5,404,713 A 4/1995 Johnson ( * ) Notice: Subject' to any disclaimer,~ the term of this 2 223L135? al' patent 1s extended or adjusted under 35 6,209,311 B1 4/2001 11011 et a1, U.S.C. 154(b) by 0 days. 6,223,616 B1 5/2001 Sheridan 6,339,927 B1 1/2002 DiPietro, Jr. 6,381,948 B1 5/2002 Klingels (21) Appl' NO" 13/452368 H2032 H * 7/2002 DiPietro, Jr. ............. .. 60/39.162 . _ 6,471,482 B2 10/2002 Montgomery et al. (22) F1169 APr- 201 2012 6,901,739 B2 6/2005 Christopherson 7,185,484 B2 3/2007 Grif?n, III et al. (65) Prior Publication Data 7,246,484 B2 7/2007 Gif?n, III et a1. 7,591,754 B2 9/2009 Duong et al. US 2013/0028712 A1 Jan 31, 2013 7,824,305 B2 11/2010 Duong et al.
    [Show full text]