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The Boeing Company 2004 Annual Report the Boeing Company 2004 Annual Report
BC112_Final Cover0302 3/6/05 10:49 PM Page fc1 The Boeing Company The Boeing Company The Boeing Company 2004 Annual Report 100 North Riverside Plaza Chicago, IL 60606-1596 U.S.A. 2004 Annual Report 0707-AR-050707-AR-05 Boeing ifc_ibc_0304 03.04.05 4:06 PM Page ifc1 Vision 2016: People working Shareholder Information The Boeing Company Electronic Proxy Receipt and Voting Duplicate Shareholder Accounts World Headquarters Shareholders have the option of voting their Registered shareholders with duplicate together as a global enterprise The Boeing Company proxies by Internet or telephone, instead of accounts may contact EquiServe for 100 North Riverside Plaza returning their proxy cards through the mail. instructions regarding the consolidation of Chicago, IL 60606-1596 Instructions are in the proxy statement and those accounts. The Company recom- for aerospace leadership. U.S.A. attached to the proxy card for the annual mends that registered shareholders always 312-544-2000 meeting. use the same form of their names in all Registered shareholders can go to stock transactions to be handled in the Strategies Values Transfer Agent, Registrar, Dividend www.econsent.com/ba to sign up to same account. Registered shareholders Run healthy core businesses Leadership Paying Agent and Plan Administrator receive their annual report and proxy state- may also ask EquiServe to eliminate excess The transfer agent is responsible for ment in an electronic format in the future. mailings of annual reports going to share- Leverage strengths into new products and services Integrity shareholder records, issuance of stock, Beneficial owners may contact the brokers holders in the same household. -
Electrically Heated Composite Leading Edges for Aircraft Anti-Icing Applications”
UNIVERSITY OF NAPLES “FEDERICO II” PhD course in Aerospace, Naval and Quality Engineering PhD Thesis in Aerospace Engineering “ELECTRICALLY HEATED COMPOSITE LEADING EDGES FOR AIRCRAFT ANTI-ICING APPLICATIONS” by Francesco De Rosa 2010 To my girlfriend Tiziana for her patience and understanding precious and rare human virtues University of Naples Federico II Department of Aerospace Engineering DIAS PhD Thesis in Aerospace Engineering Author: F. De Rosa Tutor: Prof. G.P. Russo PhD course in Aerospace, Naval and Quality Engineering XXIII PhD course in Aerospace Engineering, 2008-2010 PhD course coordinator: Prof. A. Moccia ___________________________________________________________________________ Francesco De Rosa - Electrically Heated Composite Leading Edges for Aircraft Anti-Icing Applications 2 Abstract An investigation was conducted in the Aerospace Engineering Department (DIAS) at Federico II University of Naples aiming to evaluate the feasibility and the performance of an electrically heated composite leading edge for anti-icing and de-icing applications. A 283 [mm] chord NACA0012 airfoil prototype was designed, manufactured and equipped with an High Temperature composite leading edge with embedded Ni-Cr heating element. The heating element was fed by a DC power supply unit and the average power densities supplied to the leading edge were ranging 1.0 to 30.0 [kW m-2]. The present investigation focused on thermal tests experimentally performed under fixed icing conditions with zero AOA, Mach=0.2, total temperature of -20 [°C], liquid water content LWC=0.6 [g m-3] and average mean volume droplet diameter MVD=35 [µm]. These fixed conditions represented the top icing performance of the Icing Flow Facility (IFF) available at DIAS and therefore it has represented the “sizing design case” for the tested prototype. -
Fly-By-Wire - Wikipedia, the Free Encyclopedia 11-8-20 下午5:33 Fly-By-Wire from Wikipedia, the Free Encyclopedia
Fly-by-wire - Wikipedia, the free encyclopedia 11-8-20 下午5:33 Fly-by-wire From Wikipedia, the free encyclopedia Fly-by-wire (FBW) is a system that replaces the Fly-by-wire conventional manual flight controls of an aircraft with an electronic interface. The movements of flight controls are converted to electronic signals transmitted by wires (hence the fly-by-wire term), and flight control computers determine how to move the actuators at each control surface to provide the ordered response. The fly-by-wire system also allows automatic signals sent by the aircraft's computers to perform functions without the pilot's input, as in systems that automatically help stabilize the aircraft.[1] Contents Green colored flight control wiring of a test aircraft 1 Development 1.1 Basic operation 1.1.1 Command 1.1.2 Automatic Stability Systems 1.2 Safety and redundancy 1.3 Weight saving 1.4 History 2 Analog systems 3 Digital systems 3.1 Applications 3.2 Legislation 3.3 Redundancy 3.4 Airbus/Boeing 4 Engine digital control 5 Further developments 5.1 Fly-by-optics 5.2 Power-by-wire 5.3 Fly-by-wireless 5.4 Intelligent Flight Control System 6 See also 7 References 8 External links Development http://en.wikipedia.org/wiki/Fly-by-wire Page 1 of 9 Fly-by-wire - Wikipedia, the free encyclopedia 11-8-20 下午5:33 Mechanical and hydro-mechanical flight control systems are relatively heavy and require careful routing of flight control cables through the aircraft by systems of pulleys, cranks, tension cables and hydraulic pipes. -
Aircraft Winglet Design
DEGREE PROJECT IN VEHICLE ENGINEERING, SECOND CYCLE, 15 CREDITS STOCKHOLM, SWEDEN 2020 Aircraft Winglet Design Increasing the aerodynamic efficiency of a wing HANLIN GONGZHANG ERIC AXTELIUS KTH ROYAL INSTITUTE OF TECHNOLOGY SCHOOL OF ENGINEERING SCIENCES 1 Abstract Aerodynamic drag can be decreased with respect to a wing’s geometry, and wingtip devices, so called winglets, play a vital role in wing design. The focus has been laid on studying the lift and drag forces generated by merging various winglet designs with a constrained aircraft wing. By using computational fluid dynamic (CFD) simulations alongside wind tunnel testing of scaled down 3D-printed models, one can evaluate such forces and determine each respective winglet’s contribution to the total lift and drag forces of the wing. At last, the efficiency of the wing was furtherly determined by evaluating its lift-to-drag ratios with the obtained lift and drag forces. The result from this study showed that the overall efficiency of the wing varied depending on the winglet design, with some designs noticeable more efficient than others according to the CFD-simulations. The shark fin-alike winglet was overall the most efficient design, followed shortly by the famous blended design found in many mid-sized airliners. The worst performing designs were surprisingly the fenced and spiroid designs, which had efficiencies on par with the wing without winglet. 2 Content Abstract 2 Introduction 4 Background 4 1.2 Purpose and structure of the thesis 4 1.3 Literature review 4 Method 9 2.1 Modelling -
The Boeing Company 2002 Annual Report
The Boeing Company 200220022002 AnnualAnnualAnnual ReportReportReport Vision 2016: People working together as a global enterprise for aerospace leadership. Strategies Core Competencies Values Run healthy core businesses Detailed customer knowledge Leadership Leverage strengths into new and focus Integrity products and services Large-scale system integration Quality Open new frontiers Lean enterprise Customer satisfaction People working together A diverse and involved team Good corporate citizenship Enhancing shareholder value The Boeing Company Table of Contents Founded in 1916, Boeing evokes vivid images of the amazing products 1 Operational Highlights and services that define aerospace. Each day, more than three million 2 Message to Shareholders passengers board 42,300 flights on Boeing jetliners, more than 345 8 Corporate Essay satellites put into orbit by Boeing launch vehicles pass overhead, and 16 Corporate Governance 6,000 Boeing military aircraft stand guard with air forces of 23 countries 18 Commercial Airplanes and every branch of the U.S. armed forces. 20 Integrated Defense Systems We are the leading aerospace company in the world and a top U.S. 22 Boeing Capital Corporation exporter. We hold more than 6,000 patents, and our capabilities and 24 Air Traffic Management related services include formulation of system-of-systems solutions, 26 Phantom Works advanced information and communications systems, financial services, 28 Connexion by BoeingSM homeland security, defense systems, missiles, rocket engines, launch 30 Shared Services Group systems and satellites. 32 Financials But Boeing is about much more than statistics or products, no matter 88 Selected Products, how awe-inspiring. It’s also about the enterprising spirit of our people Programs and Services working together to provide customers the best solutions possible. -
Guide to Methods & Tools for Airline Flight Safety Analysis, Issue 2
PAGE LEFT BLANK Guide to METHODS & TOOLS FOR AIRLINE FLIGHT SAFETY ANALYSIS Prepared by: GAIN Working Group B, Analytical Methods and Tools Second Edition – June 2003 THIS PAGE LEFT BLANK GAIN Guide to Methods & Tools for Airline Flight Safety Analysis Table of Contents Page Foreword...................................................................................................................................v Acknowledgements .................................................................................................................vi 1.0 Introduction.......................................................................................................................1 1.1 Purpose of Guide .........................................................................................................1 1.2 GAIN Overview ..........................................................................................................1 1.3 Working Group B: Analytical Methods and Tools .....................................................1 1.4 Scope ...........................................................................................................................2 1.5 Definitions ...................................................................................................................2 1.6 Review of Methods and Tools.....................................................................................2 1.7 Organization of this Guide ..........................................................................................3 1.8 Changes -
PDF Download
October 2006 Volume V, Issue VI www.boeing.com/frontiers LOOKING AHEAD Meet the Advanced Systems organization A SKILLED BUILD 16 of IDS, where Boeing employees are Determinant assembly helps 777 line developing new-technology solutions to support its defense, security, space and THAT FEELS BETTER 28 new market customers A look at Boeing’s wellness resources A QUALITY DECISION 34 Streamlined process aids Boeing, suppliers October 2006 Volume V, Issue VI ON THE COVER: The A160 Hummingbird. Photo by Bob Ferguson O T O BOB FERGUSON PH COVER STORY MOVING AHEAD 12 Employees in the Advanced Systems organization of Integrated Defense Systems—such as those working on the Orbital Express ASTRO demonstration satellite in Huntington Beach, Calif. (above)—are developing future capabilities to support defense, security and other customers. What’s in your wellness toolkit? Boeing offers employees wellness FEELING 28 “tools” from information to services to fitness opportunities. These re- FEATURE sources allow employees to focus on the wellness of themselves and their fam- BETTER ily members. That helps employees be more productive at work and at home. STORY BOEING FRONTIERS October 2006 3 October 2006 Volume V, Issue VI O T O The new 777 Accurate Floor Grid–Determinant T PH Assembly Process gives mechanics easier access R during assembly. It also requires significantly less CKHA 16 O space than the previous three-story tooling struc- L N ture used to build up 777 floor grids. IA R MA COMMERCIAL AIRPLANES INTEGRATED DEFENSE SYSTEMS Parts of a tool What’s the big idea Members of the Manufacturing Engineering team Boeing is developing a high-capacity miniature 16 in Everett, Wash., came up with an idea to improve 20 satellite. -
FLYHT 2019 July Investor Presentation
July 2019 FLYHT Aerospace Solutions Ltd. TSX.V: FLY OTCQX: FLYLF 1 TSX.V: FLY OTCQX: FLYLF Disclaimer www.flyht.com Forward Looking Statements This discussion includes certain statements that may be deemed “forward-looking statements” that are subject to risks and uncertainty. All statements, other than statements of historical facts included in this discussion, including, without limitation, those regarding the Company’s financial position, business strategy, projected costs, future plans, projected revenues, objectives of management for future operations, the Company’s ability to meet any repayment obligations, the use of non-GAAP financial measures, trends in the airline industry, the global financial outlook, expanding markets, research and development of next generation products and any government assistance in financing such developments, foreign exchange rate outlooks, new revenue streams and sales projections, cost increases as related to marketing, research and development (including AFIRS 228), administration expenses, and litigation matters, may be or include forward-looking statements. Although the Company believes the expectations expressed in such forward-looking statements are based on a number of reasonable assumptions regarding the Canadian, U.S., and global economic environments, local and foreign government policies/regulations and actions and assumptions made based upon discussions to date with the Company’s customers and advisers, such statements are not guarantees of future performance and actual results or developments may differ materially from those in the forward- looking statements. Factors that could cause actual results to differ materially from those in the forward-looking statements include production rates, timing for product deliveries and installations, Canadian, U.S., and foreign government activities, volatility of the aviation market for the Company’s products and services, factors that result in significant and prolonged disruption of air travel worldwide, U.S. -
The Deadline for Airlines to Comply with the GADSS Mandate Is 1St of January 2021
23 I AIRLINE & AIRCRAFT OPERATIONS The deadline for airlines to comply with the GADSS mandate is 1st of January 2021. The mandate requires aircraft operators to automate aircraft tracking capabilities. The hardware options available for operators are reviewed here. The avionic options to comply with GADSS he impetus for the International aircraft designs submitted after the updated to include new documents and Civil Aviation Organization’s introduction of the GADSS mandate must amendments pertaining to how data is (ICAO’s) Global Aeronautical be capable of timely FDR data recovery stored in distributed server networks, TDistress and Safety Systems in addition to having the standard flight such as a data-cloud and accessed and (GADSS) standards came from two high- recorders. used in an accident investigation. profile aircraft accidents. These were the The mandatory GADSS requirements Current Annex 13 legislation is based loss of Air France (AF) 447 in 2009 and will be effective from 1 January 2021. around flight data information, including the disappearance of Malaysian Airways its location during the post-flight location MH370 in 2014. and recovery (PFLR) phase. Despite flying in surveyed airspace at ICAO GADSS is defined as a performance- the time it went missing, AF447 was only A special multidisciplinary meeting on based approach, meaning the system is found about two years later. global flight tracking (MMGFT) was graded on functionality rather than In 2014 MH370 was lost in the convened in May 2014 to propose mandating a specific solution. Indian Ocean, which is very deep in recommendations for future actions. One parts. Usual methods of accurately of the main decisions taken was the need locating the wreckage have so far been for operators to pursue aircraft flight- Background unsuccessful. -
Analytical Fuselage and Wing Weight Estimation of Transport Aircraft
NASA Technical Memorandum 110392 Analytical Fuselage and Wing Weight Estimation of Transport Aircraft Mark D. Ardema, Mark C. Chambers, Anthony P. Patron, Andrew S. Hahn, Hirokazu Miura, and Mark D. Moore May 1996 National Aeronautics and Space Administration Ames Research Center Moffett Field, California 94035-1000 NASA Technical Memorandum 110392 Analytical Fuselage and Wing Weight Estimation of Transport Aircraft Mark D. Ardema, Mark C. Chambers, and Anthony P. Patron, Santa Clara University, Santa Clara, California Andrew S. Hahn, Hirokazu Miura, and Mark D. Moore, Ames Research Center, Moffett Field, California May 1996 National Aeronautics and Space Administration Ames Research Center Moffett Field, California 94035-1000 2 Nomenclature KF1 frame stiffness coefficient, IAFF/ A fuselage cross-sectional area Kmg shell minimum gage factor AB fuselage surface area KP shell geometry factor for hoop stress AF frame cross-sectional area KS constant for shear stress in wing (AR) aspect ratio of wing Kth sandwich thickness parameter b wingspan; intercept of regression line lB fuselage length bs stiffener spacing lLE length from leading edge to structural box at theoretical root chord bS wing structural semispan, measured along quarter chord from fuselage lMG length from nose to fuselage mounted main gear bw stiffener depth lNG length from nose to nose gear CF Shanley’s constant lTE length from trailing edge to structural box at CP center of pressure theoretical root chord C root chord of wing at fuselage intersection R l1 length of nose -
Instrument and Equipment
PCAR PART 7 Republic of the Philippines CIVIL AVIATION REGULATIONS (CAR) PART 7 INSTRUMENT AND EQUIPMENT July 2021 Edition i U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 INTENTIONALLY LEFT BLANK PAGE July 2021 Edition ii U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 July 2021 Edition iii U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 July 2021 Edition iv U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 July 2021 Edition v U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 RECORD OF AMENDMENTS Amendment No. Date Subject Incorporated By Original Issue 23 June 2008 Ruben F. Ciron First Amendment 21 March 2011 1. 7.2.9 Navigation Equipment Ramon S. Gutierrez Second Amendment 01 August 2013 Inserted vertical bars on the LT GEN William K previous amendments Hotchkiss III AFP (Ret) Third Amendment 31 October 2013 1. -
Aircraft Accident Report: American Airlines, Inc., Mcdonnell Douglas
Explosive decompression, American Airlines, Inc., McDonnell Douglas DC-10-10, N103AA, Near Windsor, Ontario, Canada, June 12, 1972 Micro-summary: On climb, this McDonnell Douglas DC-10-10 experienced an opening of a cargo door, explosive decompression, and a main cabin floor collapse, disrupting the flight control system. Event Date: 1972-06-12 at 1925 EST Investigative Body: National Transportation Safety Board (NTSB), USA Investigative Body's Web Site: http://www.ntsb.gov/ Cautions: 1. Accident reports can be and sometimes are revised. Be sure to consult the investigative agency for the latest version before basing anything significant on content (e.g., thesis, research, etc). 2. Readers are advised that each report is a glimpse of events at specific points in time. While broad themes permeate the causal events leading up to crashes, and we can learn from those, the specific regulatory and technological environments can and do change. Your company's flight operations manual is the final authority as to the safe operation of your aircraft! 3. Reports may or may not represent reality. Many many non-scientific factors go into an investigation, including the magnitude of the event, the experience of the investigator, the political climate, relationship with the regulatory authority, technological and recovery capabilities, etc. It is recommended that the reader review all reports analytically. Even a "bad" report can be a very useful launching point for learning. 4. Contact us before reproducing or redistributing a report from this anthology. Individual countries have very differing views on copyright! We can advise you on the steps to follow.