DOCSLIB.ORG

Commercial MRO +

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text

Load more

PLEASE CLICK ON THE FOLLOWING LINKS FOR MORE DETAILS Commercial MRO + Aerostructures + Integrated MRO For + Boeing 787 Dreamliner CFM56-3/ CFM56-5b/ CFM56-7b + EcoPower® Engine Wash + Maintenance-By-the-Hour + Engine Accessories, + Components & Parts Repair Landing Gear + Composite Parts + Manufacturing COMMERCIAL MRO COMMERCIAL MRO ST Engineering Aerospace is the world’s largest commercial airframe MRO service provider, who has topped the charts in AIRFRAME eight consecutive Airframe MRO MRO rankings*, achieving 12.5 million manhours in 2016 Lorem ipsum dolorsiw Operating a global network with facilities and Our airframe MRO service offerings span across line, amet, consectetuer affiliates in the Americas, Asia Pacific and Europe, light and heavy maintenance, transit/turnaround our comprehensive suite of capabilities covers servicing and checks, structural repair and airframe, component and engine MRO for a wide modification work, service bulletin/ airworthiness customer base which includes the world’s leading directive compliance and modifications, full-scale airlines and airfreight operators. modernisation, cabin reconfiguration, and green harvesting. We offer customers a high quality, timely and reliable maintenance programme which can be fully With hangar facilities capable of accommodating 42 customised. Since 1990, the Singapore-based MRO wide-body, 26 narrow-body and 16 general aviation has completed over 10,000 commercial aircraft aircraft simultaneously, we provide support on a heavy maintenance and modifications. wide range of customers worldwide. ............. ............. ............. ............. ............. ............. .............* We topped the charts in eight consecutive Airframe MRO rankings, achieving 12.5 million manhours in 2016 (biennial survey .............results published in Aviation Week & Space Technology’s 17 May 2017 edition). ............. ............. ............. ............. ............. ............. ............. ............. ............. .............. COMMERCIAL MRO ST Engineering Aerospace provides repair and overhaul services for more than 25,000 mechanical and avionics component types fitted on various COMPONENT Airbus and Boeing aircraft and helicopters. An MRO appointed service centre for leading OEMs, we provide services for avionics (including flight computers, electrical, radar/communications, instruments and displays) and mechanical components (including heli-dynamics, landing gears, aerostructures, hydraulics, pneumatics and propellers). In addition, we offer customers a wide range of aircraft component management and support services. This includes its in-house trademarked Maintenance-By-the-Hour (MBH™) programme (with which we are supporting a fleet of more than 600 aircraft worldwide), material supply programme support, warehouse and material management, Aircraft-On-Ground spares and service support, aircraft parts trading, aircraft operating lease as well as OEM representation. With facilities in Singapore and China having an Our comprehensive suite of engine capabilities annual capacity of more than 300 engines, includes engine repair and overhaul, engine we offer engine total support with a full spectrum of component and accessory repair, engine fleet ENGINE MRO services in close partnership with the engine OEMs management, on-wing and off-wing maintenance, for a wide range of commercial aircraft engines. asset management, MBH™ programme support, engine wash, engine part-down, as well as engine This includes the CFM56 family, GEnx-1B, GEnx- leasing. 2B, General Electric F110, Honeywell T55, Pratt & Whitney F100, Rolls-Royce / Allison T56 / 501, Our aim is to cover almost every part of the value Turbomeca Makila, as well as the International Aero chain of engine maintenance support that a Engines V2500 engine. customer would look for. COMMERCIAL MRO AEROSTRUCTURES COMMERCIAL MRO AEROSTRUCTURES As part of our Component Total Our aerostructures MRO capabilities are centralised At ST Engineering Aerospace, we understand the Support offering, ST Engineering in our Stockholm-based facility, which is just a importance of letting airlines and aircraft fleet Aerospace provides an extensive stone’s throw from Arlanda International Airport. owners to concentrate on their core business range of maintenance, repair and Our team of aerostructures specialists have through and maximise aircraft availability. Together with overhaul of commercial aircraft dedication, innovation, and experience provided our central maxims and our value system of A330 Trent 700 Thrust Reverser nacelles, primarily thrust reverser, quality MRO services to the aviation community Integrity, Value Creation, Courage, Commitment and undergoing final assembly inlet cowl, fan cowl, exhaust nozzle across the globe. We aim to deliver durable and Compassion, our work processes are focused on and other secondary structures, reliable repair solutions performed to a high meeting your requirements and creating value by as well as repair and overhaul of standard of quality at a competitive price. enhancing operational excellence. flight control surfaces and other aerostructures components We perform both minor and major structural repairs for airframe, nacelle and aerostructure components. Complete aircraft set Boeing 767 PW4000 Complete aircraft set Boeing 737NG CFM56-7B thrust reversers ready for delivery after ready for delivery after overhaul service overhaul service COMMERCIAL MRO AEROSTRUCTURES NACELLE CAPABILITIES THURST REVERSER INLET COWL EXHAUST NOZZLE FAN COWL Aircraft Type Engine Aircraft Type Engine Aircraft Type Engine Aircraft Type Engine A300 PW4000 A320 V2500-A5 A330 Trent 700 A330 Trent 700 A310 PW4000 A330 Trent 700 A340 CFM56-5C 737NG CFM56-7B A330 Trent 700 A340 CFM56-5C 737NG CFM56-7B 787 GEnx 737NG CFM56-7B 737NG CFM56-7B 787 GEnx 787 Trent 1000 747 PW4000 747 PW4000 787 Trent 1000 767 PW4000 767 PW4000 787 GEnx 787 GEnx 787 Trent 1000 787 Trent 1000 BOEING 787 DREAMLINER GLOBAL • Access to suite of proprietary repairs, processes, SUPPORT ON FULL NACELLE SYSTEM instructions and materials. COMPONENTS • Production based tooling to support deep ST Engineering Aerospace signed a long term level repairs and replacement of major nacelle agreement with UTC Aerospace Systems in July structural elements/sub-structure components 2013, to provide MRO services on the Boeing 787 utilising proprietary production tooling Dreamliner nacelle systems for both the Rolls Royce • Expanded access to stay out zones with Trent 1000 and General Electric GEnx engines. proprietary aerostructures 350° materials • Out of manual repair schemes, acoustic area As a licensed UTC Aerospace Systems Boeing repairs, large area repairs 787 nacelles MRO provider, we offer operators a • Sytems test and fault isolation comprenesive range of repair Solutions and services • Large stock of assets (both Nacelle platforms) Full nacelle MRO services; including but not limited to: to support operators needs thrust reversers, inlet cowls, fan cowls, exhaust nozzles, centerbody • Maintenance-By-the-Hour, service level and all sub-assemblies agreements, ad-hoc repairs, technical assistance and scheduled overhaul offerings COMMERCIAL MRO AEROSTRUCTURES FLIGHT CONTROLS AND OTHER AEROSTRUCTURES COMPONENT CAPABILITIES AT ST Engineering Aerospace, we Capabilities including but not limited to: provide overhaul and repair services for Ailerons, doors, elevators, flaps, panels, stabilisers, a wide range of flight control and other slats, tabs, vanes, spoilers, radom, rudder, wing tip, A330 Trent 700 Boeing 737NG CFM56-7B Boeing 767 PW4000 aerostructures related components. Our winglets and more. Thrust Reverser Thrust Reverser Thrust Reverser extensive knowledge and experience in metal and composite bonding is a key ADDED VALUE SERVICES element in our product portfolio LOAN & EXCHANGE SERVICES We maintain a large pool of rotable assets, consisting of nacelle and aerostructures component, such as thrust reverser, inlet cowl, fan cowl, exhaust A330 Trent 700 A330 Trent 700 A340 CFM56-5C Inlet Cowl Exhaust Nozzle Inlet Cowl nozzle and others for a wide range of aircraft types. Boeing 737NG slat, wedge Metal-bonding with repair doubler Post repair assembly worn out of limit due to surface treated in anodising line per chafting in operations Boeing specification BAC555 COMMERCIAL MRO AEROSTRUCTURES ENGINEERING SERVICES FIELD-SERVICE At ST Engineering Aerospace, we help our customers Whether it’s a complex composite repair, structural establish pro-active maintenance programmes repair, special Inspection or fleet sampling overview, which improve customer fleet reliability, and reduce our dynamic team of experienced craftsmen A300 PW4000 Thrust unplanned maintenance events and removals. can provide a tailor made solution to meet your Reverser rigging and trouble shooting training Through pro-active maintenance, we help customers requirements. Airworthiness certificates for on-site at customer conduct removal plans and recommend Service inspections, modifications or repairs performed on location Bulletin incorporations. site can be provided as applicable. • Maintaining fleet reliability ON-SITE SUPPORT • Achieving product design life service goals It’s cost cutting initiatives or product familiarisation • Avoiding unplanned maintenanance events we can support you on site with training and • Avoiding unscheduled removals information modules aimed at improving • Reducing risk of exposure to exchange/loan fees performance and optimising resources. •
Recommended publications
  • Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory figures As of Sept

    Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory figures As of Sept

    Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2014. By Aaron M. U. Church, Associate Editor I 2015 USAF Almanac BOMBER AIRCRAFT flight controls actuate trailing edge surfaces that combine aileron, elevator, and rudder functions. New EHF satcom and high-speed computer upgrade B-1 Lancer recently entered full production. Both are part of the Defensive Management Brief: A long-range bomber capable of penetrating enemy defenses and System-Modernization (DMS-M). Efforts are underway to develop a new VLF delivering the largest weapon load of any aircraft in the inventory. receiver for alternative comms. Weapons integration includes the improved COMMENTARY GBU-57 Massive Ordnance Penetrator and JASSM-ER and future weapons The B-1A was initially proposed as replacement for the B-52, and four pro- such as GBU-53 SDB II, GBU-56 Laser JDAM, JDAM-5000, and LRSO. Flex- totypes were developed and tested in 1970s before program cancellation in ible Strike Package mods will feed GPS data to the weapons bays to allow 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft weapons to be guided before release, to thwart jamming. It also will move added 74,000 lb of usable payload, improved radar, and reduced radar cross stores management to a new integrated processor. Phase 2 will allow nuclear section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in and conventional weapons to be carried simultaneously to increase flexibility. Iraq during Desert Fox in December 1998.
  • Lockheed Martin F-35 Lightning II Incorporates Many Significant Technological Enhancements Derived from Predecessor Development Programs

    Lockheed Martin F-35 Lightning II Incorporates Many Significant Technological Enhancements Derived from Predecessor Development Programs

    AIAA AVIATION Forum 10.2514/6.2018-3368 June 25-29, 2018, Atlanta, Georgia 2018 Aviation Technology, Integration, and Operations Conference F-35 Air Vehicle Technology Overview Chris Wiegand,1 Bruce A. Bullick,2 Jeffrey A. Catt,3 Jeffrey W. Hamstra,4 Greg P. Walker,5 and Steve Wurth6 Lockheed Martin Aeronautics Company, Fort Worth, TX, 76109, United States of America The Lockheed Martin F-35 Lightning II incorporates many significant technological enhancements derived from predecessor development programs. The X-35 concept demonstrator program incorporated some that were deemed critical to establish the technical credibility and readiness to enter the System Development and Demonstration (SDD) program. Key among them were the elements of the F-35B short takeoff and vertical landing propulsion system using the revolutionary shaft-driven LiftFan® system. However, due to X- 35 schedule constraints and technical risks, the incorporation of some technologies was deferred to the SDD program. This paper provides insight into several of the key air vehicle and propulsion systems technologies selected for incorporation into the F-35. It describes the transition from several highly successful technology development projects to their incorporation into the production aircraft. I. Introduction HE F-35 Lightning II is a true 5th Generation trivariant, multiservice air system. It provides outstanding fighter T class aerodynamic performance, supersonic speed, all-aspect stealth with weapons, and highly integrated and networked avionics. The F-35 aircraft
  • Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept

    Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept

    Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber.
  • Download This File Now!

    Download This File Now!

    INTRODUCTION................................................................................................................. 4 1. AERODYNAMIC SECTION........................................................................................... 8 1.1 Introduction ............................................................................................................................................................ 8 1.2 The Pitch limiters ................................................................................................................................................. 10 1.2 The Lift and Drag ( Cl / Cd )............................................................................................................................... 12 1.3 The Rudder ( CY )................................................................................................................................................ 19 1.4 The Drag Index (DI)............................................................................................................................................. 20 2 ENGINES SECTION................................................................................................ 22 2.1 The Pratt & Whitney engines ............................................................................................................................. 22 2.2 The General Electric Engines ............................................................................................................................. 28 3 A BIT OF HISTORY.............................................................................................
  • Issue No. 4, Oct-Dec

    Issue No. 4, Oct-Dec

    VOL. 6, NO. 4, OCTOBER - DECEMBER 1979 t l"i ~ ; •• , - --;j..,,,,,,1:: ~ '<• I '5t--A SERVt(;E P\JBLICATtON Of: t.OCKH EE:O-G EORGlA COt.'PAfllV A 01Vt$10,.. or t.OCKHEEOCOAf'ORATION A SERVICE PUBLICATION OF LOCKHEED-GEORGIA COMPANY The C-130 and Special Projects Engineering A DIVISION OF Division is pleased to welcome you to a LOCKHEED CORPORATION special “Meet the Hercules” edition of Service News magazine. This issue is de- Editor voted entirely to a description of the sys- Don H. Hungate tems and features of the current production models of the Hercules aircraft, the Ad- Associate Editors Charles 1. Gale vanced C-130H, and the L-100-30. Our James A. Loftin primary purpose is to better acquaint you with these two most recently updated Arch McCleskey members of Lockheed’s distinguished family Patricia A. Thomas of Hercules airlifters, but first we’d like to say a few words about the engineering or- Art Direction & Production ganization that stands behind them. Anne G. Anderson We in the Project Design organization have the responsibility for the configuration and Vol. 6, No. 4, October-December 1979 systems operation of all new or modified CONTENTS C-130 or L-100 aircraft. During the past 26 years, we have been intimately involved with all facets of Hercules design and maintenance. Our goal 2 Focal Point is to keep the Lockheed Hercules the most efficient and versatile cargo aircraft in the world. We 0. C. Brockington, C-130 encourage our customers to communicate their field experiences and recommendations to us so that Engineering Program Manager we can pass along information which will be useful to all operators, and act on those items that would benefit from engineeringattention.
  • The Market for Aviation Turbofan Engines

    The Market for Aviation Turbofan Engines

    The Market for Aviation Turbofan Engines Product Code #F640 A Special Focused Market Segment Analysis by: Aviation Gas Turbine Forecast Analysis 1 The Market for Aviation Turbofan Engines 2010-2019 Table of Contents Executive Summary .................................................................................................................................................2 Introduction................................................................................................................................................................2 Trends..........................................................................................................................................................................3 Market Focus .............................................................................................................................................................3 Competitive Environment.......................................................................................................................................4 Figure 1 - The Market for Aviation Turbofan Engines Unit Production 2010 - 2019 (Bar Graph) .................................................................................6 Figure 2 - The Market for Aviation Turbofan Engines Value of Production 2010 - 2019 (Bar Graph)...........................................................................6 Manufacturers Review.............................................................................................................................................7
  • Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept

    Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept

    Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2015. By Aaron M. U. Church, Senior Editor ■ 2016 USAF Almanac BOMBER AIRCRAFT B-1 Lancer Brief: Long-range bomber capable of penetrating enemy defenses and de- livering the largest weapon load of any aircraft in the inventory. COMMENTARY The B-1A was initially proposed as replacement for the B-52, and four proto- types were developed and tested before program cancellation in 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft added 74,000 lb of usable payload, improved radar, and reduced radar cross section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in Iraq during Desert Fox in December 1998. Its three internal weapons bays accommodate a substantial payload of weapons, including a mix of different weapons in each bay. Lancer production totaled 100 aircraft. The bomber’s blended wing/ body configuration, variable-geometry design, and turbofan engines provide long range and loiter time. The B-1B has been upgraded with GPS, smart weapons, and mission systems. Offensive avionics include SAR for tracking, B-2A Spirit (SSgt. Jeremy M. Wilson) targeting, and engaging moving vehicles and terrain following. GPS-aided INS lets aircrews autonomously navigate without ground-based navigation aids Dimensions: Span 137 ft (spread forward) to 79 ft (swept aft), length 146 and precisely engage targets. Sniper pod was added in 2008. The ongoing ft, height 34 ft. integrated battle station modifications is the most comprehensive refresh in Weight: Max T-O 477,000 lb.
  • Gallery of Weapons

    Gallery of Weapons

    Gallery of Weapons By Aaron M. U. Church 2017 USAF Almanac B-1 Lancer TSgt. Richard Ebensberger/USAF BOMBER AIRCRAFT 2016. FY17 funds support development of higher ■■ B-2 SPIRIT powered Military Code (M-Code) jam-resistant Brief: Stealthy, long-range nuclear and con- ■■ B-1 LANCER GPS interface. B-1s resumed Pacific presence ventional strike bomber. Brief: Long-range penetrating bomber capable rotations to Guam in 2016. of delivering the largest weapon load of any COMMENTARY aircraft in the Air Force inventory. EXTANT VARIANT(S) The B-2 is a flying wing that combines LO • B-1B. Upgraded production version of the stealth design with high aerodynamic efficiency. COMMENTARY canceled B-1A. Spirit entered combat against Serb targets The B-1A was initially proposed as a replace- Function: Long-range conventional bomber. during Allied Force on March 24, 1999. B-2 ment for the B-52, and four prototypes were Operator: AFGSC, AFMC. production was completed in three successive developed and tested before program cancella- First Flight: Dec. 23, 1974 (B-1A); Oct. 18, blocks and all aircraft were upgraded to Block tion in 1977. The program was revived in 1981 1984 (B-1B). 30 standards with AESA radar. AESA paves the as the B-1B. The vastly upgraded aircraft added Delivered: June 1985-May 1988. way for future advanced weapons integration 74,000 lb of usable payload, improved radar, and IOC: Oct. 1, 1986, Dyess AFB, Texas (B-1B). including Long-Range Standoff (LRSO) mis- reduced radar cross section, but cut speed to Production: 104. sile and B61-12 bomb.
  • AC-130 GUNSHIP and ITS VARIANTS Research from 10/2010 AC-130

    AC-130 GUNSHIP and ITS VARIANTS Research from 10/2010 AC-130

    THE AC-130 GUNSHIP AND ITS VARIANTS Research from 10/2010 AC-130 The AC-130 gun ship’s primary missions are close air support, air interdiction and armed reconnaissance. Other missions include perimeter and point defense, escort, landing, drop and extraction zone support, forward air control, limited command and control, and combat search and rescue. These heavily armed aircraft incorporate side-firing weapons integrated with sophisticated sensor, navigation and fire control systems to provide surgical firepower or area saturation during extended periods, at night and in adverse weather. The AC-130 has been used effectively for over thirty years to take out ground defenses and targets. One drawback to using the AC-130 is that it is typically only used in night assaults because of its poor maneuverability and limited orientations relative to the target during attack. During Vietnam, gun ships destroyed more than 10,000 trucks and were credited with many life-saving close air support missions. AC-130s suppressed enemy air defense systems and attacked ground forces during Operation Urgent Fury in Grenada. This enabled the successful assault of Point Saline’s airfield via airdrop and air land of friendly forces. The gunships had a primary role during Operation Just Cause in Panama by destroying Panamanian Defense Force Headquarters and numerous command and control facilities by surgical employment of ordnance in an urban environment. As the only close air support platform in the theater, Spectres were credited with saving the lives of many friendly personnel. Both the H-models and A-models played key roles. The fighting was opened by a gunship attack on the military headquarters of the dictator of Panama and the outcome was never in doubt.
  • A Parametric Analysis of a Turbofan Engine with an Auxiliary Bypass Combustion Chamber – the Turboaux Engine

    A Parametric Analysis of a Turbofan Engine with an Auxiliary Bypass Combustion Chamber – the Turboaux Engine

    Old Dominion University ODU Digital Commons Mechanical & Aerospace Engineering Theses & Dissertations Mechanical & Aerospace Engineering Fall 12-2020 A Parametric Analysis of a Turbofan Engine with an Auxiliary Bypass Combustion Chamber – The TurboAux Engine Kaleab Fetahi Old Dominion University, [email protected] Follow this and additional works at: https://digitalcommons.odu.edu/mae_etds Part of the Mechanical Engineering Commons, Thermodynamics Commons, and the Transportation Commons Recommended Citation Fetahi, Kaleab. "A Parametric Analysis of a Turbofan Engine with an Auxiliary Bypass Combustion Chamber – The TurboAux Engine" (2020). Master of Science (MS), Thesis, Mechanical & Aerospace Engineering, Old Dominion University, DOI: 10.25777/55dp-vd74 https://digitalcommons.odu.edu/mae_etds/330 This Thesis is brought to you for free and open access by the Mechanical & Aerospace Engineering at ODU Digital Commons. It has been accepted for inclusion in Mechanical & Aerospace Engineering Theses & Dissertations by an authorized administrator of ODU Digital Commons. For more information, please contact [email protected]. A PARAMETRIC ANALYSIS OF A TURBOFAN ENGINE WITH AN AUXILIARY BYPASS COMBUSTION CHAMBER – THE TURBOAUX ENGINE by Kaleab Fetahi B.S. May 2019, Old Dominion University M.S. December 2020, Old Dominion University A Thesis Submitted to the Faculty of Old Dominion University in Partial Fulfillment of the Requirements for the Degree of MASTER OF SCIENCE MECHANICAL ENGINEERING OLD DOMINION UNIVERSITY December 2020 Approved by: Sharan Asundi (Director) Arthur C. Taylor (Co-Director) Adem Ibrahim (Member) ii ABSTRACT A PARAMETRIC ANALYSIS OF A TURBOFAN ENGINE WITH AN AUXILIARY BYPASS COMBUSTION CHAMBER – THE TURBOAUX ENGINE Kaleab Fetahi Old Dominion University, 2020 Director: Dr. Sharan Asundi A parametric study of a novel turbofan engine with an auxiliary combustion chamber, nicknamed the TurboAux engine is presented.
  • Modern Combat Aircraft (1945 – 2010)

    Modern Combat Aircraft (1945 – 2010)

    I MODERN COMBAT AIRCRAFT (1945 – 2010) Modern Combat Aircraft (1945-2010) is a brief overview of the most famous military aircraft developed by the end of World War II until now. Fixed-wing airplanes and helicopters are presented by the role fulfilled, by the nation of origin (manufacturer), and year of first flight. For each aircraft is available a photo, a brief introduction, and information about its development, design and operational life. The work is made using English Wikipedia, but also other Web sites. FIGHTER-MULTIROLE UNITED STATES UNITED STATES No. Aircraft 1° fly Pg. No. Aircraft 1° fly Pg. Lockheed General Dynamics 001 1944 3 011 1964 27 P-80 Shooting Star F-111 Aardvark Republic Grumman 002 1946 5 012 1970 29 F-84 Thunderjet F-14 Tomcat North American Northrop 003 1947 7 013 1972 33 F-86 Sabre F-5E/F Tiger II North American McDonnell Douglas 004 1953 9 014 1972 35 F-100 Super Sabre F-15 Eagle Convair General Dynamics 005 1953 11 015 1974 39 F-102 Delta Dagger F-16 Fighting Falcon Lockheed McDonnell Douglas 006 1954 13 016 1978 43 F-104 Starfighter F/A-18 Hornet Republic Boeing 007 1955 17 017 1995 45 F-105 Thunderchief F/A-18E/F Super Hornet Vought Lockheed Martin 008 1955 19 018 1997 47 F-8 Crusader F-22 Raptor Convair Lockheed Martin 009 1956 21 019 2006 51 F-106 Delta Dart F-35 Lightning II McDonnell Douglas 010 1958 23 F-4 Phantom II SOVIET UNION SOVIET UNION No.
  • Introductory Study of the Chemical Behavior of Jet Emissions in Photochemical Smog.[Computerized Simulation]

    Introductory Study of the Chemical Behavior of Jet Emissions in Photochemical Smog.[Computerized Simulation]

    N O T I C E THIS DOCUMENT HAS BEEN REPRODUCED FROM MICROFICHE. ALTHOUGH IT IS RECOGNIZED THAT CERTAIN PORTIONS ARE ILLEGIBLE, IT IS BEING RELEASED IN THE INTEREST OF MAKING AVAILABLE AS MUCH INFORMATION AS POSSIBLE ^_tsa (NASA-CR-152345) INTRUll[1C'IuRY STUDY OF THL Nd0-[1d y 1 ^ CHE"IICAL LF.tiaV1U[1 OF JE'i EtI551UNS IN (^ PHUTOc:HE^y 1CAL SMOG :• i^al [ieEort (Systems Applications, lnc.) i 15 I^ NC A^)6/MF AJ L'nclas '' ='! ^^^^ R {. ^^ 1 .. ^ N ^ ^^^1 PREPARED BY SY^ITEMB APPLICATIONS. INC. t^ NT f-, . - ^^! - t 5 ^.3S^ Final Report fc INTRODUCTORY STUDY OF THE CHEMICAL BENAVIOR OF JE7 EMISSIONS IN PHOTOCHEMICAL SMOG Contract No. NAS2-882.1 EF76-04R May 1976 by Gary Z. Whitten Henry Hogo Systems Applications, Incorporated 950 Northgate Drive San Rafael, California 94903 C Prepared for - Ames Research Center = National Aeronautics and Space Administration Moffett Field, California 94035 ' and Federal Aviation Administration Washington, D. C. _ C^ _ T=^ -- ^.^ - -^— i ii CONTENTS L `^ f OF ILLUSTRATIONS vi LIST OF TABLES ix I INTRODUCTION . 1 II EXHAUST EMISSIONS IN THE VICINITY OF AN AIRPORT 3 A. The LTO Cycle . 3 6. Kydrocarbon Composition of Aircraft Emissions 6 C. Aircraft Emissions of Nitrogen Oxides . 11 D. Hydrocarbon/NOx Ratios from Aircraft Emissions and Automobile Emissions 18 1. I'^^drocarbonjNOx Ratios from Aircraft Emissions 18 2. Hydrocarbon/NOx Ratios from Automobile Exhaust Emissions 25 III COMPUTER SIMULATIONS OF PHOTOCHEMICAL SMOG 27 A. The Generalized Kinetic Mechanism . 27 B. Results of the Computer Simulations 32 G. Computer Simulations with Automobile Emissions 49 IV SENSITIVITY RUNS AND EVALUATION OF THE KINETIC MECHANISM 53 ` A.