Hughes Oh-6 Cayuse / Model 500
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Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor
Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems تحليل اﻹلتواء الديناميكي ﻷنظمة الحركة في المروحية العمودية )Schweizer 300C( by HAITHAM KHAMIS MOHAMMED AL-SAEEDI Dissertation submitted in fulfilment of the requirements for the degree of MSc SYSTEMS ENGINEERING at The British University in Dubai January 2019 DECLARATION I warrant that the content of this research is the direct result of my own work and that any use made in it of published or unpublished copyright material falls within the limits permitted by international copyright conventions. I understand that a copy of my research will be deposited in the University Library for permanent retention. I hereby agree that the material mentioned above for which I am author and copyright holder may be copied and distributed by The British University in Dubai for the purposes of research, private study or education and that The British University in Dubai may recover from purchasers the costs incurred in such copying and distribution, where appropriate. I understand that The British University in Dubai may make a digital copy available in the institutional repository. I understand that I may apply to the University to retain the right to withhold or to restrict access to my thesis for a period which shall not normally exceed four calendar years from the congregation at which the degree is conferred, the length of the period to be specified in the application, together with the precise reasons for making that application. ___________________ Signature of the student COPYRIGHT AND INFORMATION TO USERS The author whose copyright is declared on the title page of the work has granted to the British University in Dubai the right to lend his/her research work to users of its library and to make partial or single copies for educational and research use. -
MD HELICOPTERS DELIVERS NEW MD 600N with ADVANCED, FAA-CERTIFIED ALL-GLASS COCKPIT Authorized Sales Representative Sapura Aero Accepts New, Multi-Mission MD 600N
FOR IMMEDIATE RELEASE MD HELICOPTERS DELIVERS NEW MD 600N WITH ADVANCED, FAA-CERTIFIED ALL-GLASS COCKPIT Authorized Sales Representative Sapura Aero accepts new, multi-mission MD 600N The new MD 600N features an integrated all-glass cockpit; utility/personnel transport & single-patient EMS capability Mesa, Ariz., October 17, 2017 – MD Helicopters, Inc. (MDHI) announces the delivery of a new MD 600N to its Subang, Malaysia- based sales agent, Sapura Aero. Configured with the company’s upgraded FAA type-certified all- glass cockpit, this MD 600N also features single-patient EMS interior from Air Ambulance Technology (AAT). “I am proud to deliver this exquisite aircraft to our partners at Sapura Aero, and am excited about the growth that this delivery will inspire in the region,” said Lynn Tilton, Chief Executive Officer for MD Helicopters. “We have an excellent relationship with the Sapura team built on a shared commitment to operational and organizational excellence. With this delivery complete, I am confident we will move forward with a focus on rapid expansion and excellence in customer experiences.” Type-Certified Glass Cockpit At the 2017 HAI Heli-Expo in Dallas, Texas, MD Helicopters announced their commitment to deliver FAA- certified all-glass cockpits to the company’s full range of single- and twin-engine aircraft. In June of this year the company announced it had completed all FAA certification requirements for the MD 600N cockpit upgrade. On July 26, 2017, the type certification was granted. MDHI’s single-engine all-glass cockpit features: Howell Instruments Electronic Flight Instrument System Garmin G500 (GDU620) PFD/MFD Garmin GTN 650 Touchscreen NAV/COM/GPS L-3 ESI 500 Electronic Standby Instrument Flexible, Multi-Function Cabin Design Renowned for its ergonomic, modular interior design, the MD 600N has the flexibility to support up to six (6) different cabin configurations. -
Helicopter Noise Reduction Technology, Status Report
Helicopter Noise Reduction Technology Status Report 21 April 2015 Contributors: ICCAIA: Snecma, Airbus Helicopters, Sikorsky Aircraft, Bell Helicopter, AgustaWestland, Turbomeca, Marenco Swisshelicopter Research Centers: NASA, DLR, ONERA, JAXA 1 Contents 1 Introduction .................................................................................................................................................. 3 2 Helicopter noise sources and related noise generation mechanisms ............................................................ 4 2.1 Rotor noise ........................................................................................................................................... 4 2.2 Anti-torque noise .................................................................................................................................. 4 2.3 Engine noise ......................................................................................................................................... 5 2.3.1 Turboshaft Engines.......................................................................................................................... 5 2.3.2 Piston Engines ................................................................................................................................. 5 2.4 Contribution of noise sources depending on flight condition .............................................................. 5 3 State-of-the-Art Helicopters ........................................................................................................................ -
Md 520N Helicopter
TTEECCHHNNIICCAALL DDEESSCCRRIIPPTTIIOONN MMDD 552200NN HHEELLIICCOOPPTTEERR MD Helicopters, Inc. Marketing and Sales 4555 E. McDowell Rd. Mesa, AZ 85215 480-346-6130 www.mdhelicopters.com [email protected] MISSION PROVEN, CHALLENGE READY THIS PAGE INTENTIONALLY LEFT BLANK TECHNICAL DESCRIPTION MD 520N HELICOPTER MD Helicopters, Inc. 4555 E. McDowell Rd Mesa, Arizona CAGE: 1KVX4 DUNS: 054313767 www.mdhelicopters.com This Technical Description includes information and intellectual property that is the property of MD Helicopters, Inc. (MDHI). It provides general information for evaluation of the design, equipment, and performance of the MD 520N helicopter. The information presented in this Technical Description does not constitute an offer and is subject to change without notice. This proprietary information, in its entirety, shall not be duplicated, used, or disclosed—directly or indirectly, in whole or in part—for any purpose other than for evaluation. MD Helicopters, Inc. reserves the right to revise this Technical Description at any time MD 520N Technical Description REPORT NO.: MD14030410-520NTD NO. OF PAGES: 52 Use or disclosure of data in this Technical Description is subject to the restriction on the cover page of this document. ATTACHMENTS: None Revision By Approved Date Pages and/or Paragraphs Affected New BAH 04-Mar-14 All (Initial Issue) MD 520N Technical Description Contents 1. FOREWORD ........................................................................................................ 1 2. KEY ADVANTAGES AND FEATURES -
NASA Aeronautical Engineering Sring Aeronautical Engir Iqineering Aeronautical Engim Engineering Aeronautical E ' Ngineering
Aeronautical NASA SP-7037(150) Engineering July 1982 A Continuing NASA Bibliography with Indexes National Aeronautics and Space Administration (NASA-SP-7037(150» AERONAUTICAL N8^ ENGiNELKING: A CONTINUING BIBLIOGRAPHY allfl J1NUEXES (National Aeronautics and Space Administration) 114 p HC >5.00 CSCL 01A Oncias Aeronautical Engineering sring Aeronautical Engir iqineering Aeronautical Engim Engineering Aeronautical E ' ngineering Aeronaut " Engineering Aerc ing Aeronautical Engir (Sneering Aeronautical bngm il Engineering Aeronautical E lutical Engineering Aeronaut eronautical Engineering Aerc ing Aeronautical Engir ACCESSION NUMBER RANGES ........ Accession numbers efte<i in this Supplement fait within the following ranges, STAR (N-100Q0 Series) N82-2Q139 - N82-22140 IAA (A-10000 Series) A82-25S39 - A82-28538 This bibliography was pmpared by the NASA Scientific and Techracaj Informatioft facility operated for the National Aeronautics and Space Administration by PRO Government Information Systems. NASASP-7037(150) AERONAUTICAL ENGINEERING A CONTINUING BIBLIOGRAPHY WITH INDEXES (Supplement 150) A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information sys- tem and announced in June 1982 in • Scientific and Technical Aerospace Reports (STAR) • International Aerospace Abstracts (IAA). f\ I /\CIZ/\ Scientific and Technical Information Branch 1982 I \l/ lID/ 1 National Aeronautics and Space Administration Washington, DC This supplement is available as NTISUB 141.093 from the National Technical Information Service (NTIS), Springfield, Virginia 22161 at the price of S5.00 domestic; S10.00 foreign. INTRODUCTION Under the terms of an interagency agreement with the Federal Aviation Administration this publication has been prepared by the National Aeronautics and Space Administration for the joint use of both agencies and the scientific and technical community concerned with the field of aeronautical engineering. -
Applications
An invitation to AHS Award Nomination Form Nominations are due by February 26 honor Please nominate online at www.vtol.org/awards-and contests/awards-nomination. innovation and If you are not able to register online, please contact Liz Malleck at (703) 684-6777 x107 excellence for a paper form. in vertical flight technology and its applications The AHS International Awards Program AHS International has a tradition for honoring the vertical flight industry’s most outstanding achievements. Established in 1944, the Society’s Awards Program provides an international showcase for the finest work and research in the industry. Whether it be for a single outstanding contribution or achievement, a major technical innovation, an act of heroism, long and valued service or work that further advances the frontiers of vertical flight technology and its applications, the Society’s awards attract worldwide recognition. Who is eligible for an award? The Society’s Awards recognize achievement at all levels and in all disciplines. Anyone working in the vertical flight industry, anywhere in the world, whether in academia, airframes, engines, systems, the military services, government, research, manufacturing, or in civil and commercial operations or in any other discipline involved in vertical flight is eligible. The Awards Program is structured to recognize individuals at various stages of their careers. Who makes the nominations? he simple answer is you do. You have an important and responsible role to play in identifying those of your colleagues deserving of special T recognition. If there is someone, or a group of persons, you feel is making an outstanding contribution to the world of vertical flight, please read through this brochure, select the appropriate award and make your recommendation. -
Historical Perspective Boeing Frontiers / September 2010 11
e was eccentric and controversial, and wealthy almost beyond measure, a “ I want to be maverick businessman and Hollywood movie producer who in his later years The need for Hbecame a recluse. remembered for But Howard Hughes Jr. also was passionate about aviation, an aerospace pioneer and record-setting pilot who left a legacy of companies and accomplishments that only one thing— shaped the future of Boeing, and of airplanes that advanced aircraft design and flight and are a part of aviation history. my contribution This month marks the 75th anniversary of a record-breaking performance by one of those airplanes, the H-1 Racer. On Sept. 13, 1935, Hughes piloted the H-1 at 352 mph to aviation.” (566 kph) over a measured speed course near Santa Ana, Calif., shattering the existing – Howard Hughes international record of 314 mph (505 kph). It was the H-1 that gave birth to Hughes Aircraft Co., which was established that speed same year. Boeing’s satellite business in El Segundo, Calif., and its helicopter business in Mesa, Ariz., have their roots in the aviation company Hughes founded. But the connection between Boeing and Howard Hughes goes back even further. Hughes was born in Houston in 1905, the son of a wealthy oil industrialist. By 1931, the young Hughes was already a well-known motion picture producer and an emerging pilot with a passion for speed and an eye for accuracy and detail. He admired Charles Lindbergh and had started to make a name for himself as an aviator with a Boeing airplane, the 100A. -
Technical Description
TTEECCHHNNIICCAALL DDEESSCCRRIIPPTTIIOONN MMDD 990022 EEXXPPLLOORREERR MD Helicopters, Inc. Sales and Marketing 4555 E. McDowell Rd. Mesa, AZ 85215 PH: 480.346.6474 FAX: 480.346.6339 www.mdhelicopters.com [email protected] MISSION PROVEN, CHALLENGE READY THIS PAGE INTENTIONALLY LEFT BLANK TECHNICAL DESCRIPTION MD 902 EXPLORER MD Helicopters, Inc. 4555 E. McDowell Rd Mesa, Arizona CAGE: 1KVX4 DUNS: 054313767 www.mdhelicopters.com This Technical Description includes information and intellectual property that is the property of MD Helicopters, Inc. (MDHI). It provides general information for evaluation of the design, equipment, and performance of the MD 902 helicopter. The information presented in this Technical Description does not constitute an offer and is subject to change without notice. This proprietary information, in its entirety, shall not be duplicated, used, or disclosed—directly or indirectly, in whole or in part—for any purpose other than for evaluation. MD Helicopters, Inc. reserves the right to revise this Technical Description at any time MD 902 Explorer Technical Description REPORT NO.: MD14021407-902TD NO. OF PAGES: 74 Use or disclosure of data in this Technical Description is subject to the restriction on the cover page of this document. ATTACHMENTS: None Revision By Approved Date Pages and/or Paragraphs Affected New RCP 14-Feb-14 All (Initial Issue) MD 902 Explorer Technical Description Contents 1. FOREWORD ........................................................................................................ 1 -
AH-64E Apache How to Innovate Over a Long Term: the Boeing AH-64 Apache the Aerospace & Defense Forum History to the Apache
The Aerospace & Defense Forum Arizona Chapter August 12, 2014 Apache Overview Boeing Military Aircraft | Vertical Lift AH-64E Apache How to Innovate over a Long Term: The Boeing AH-64 Apache The Aerospace & Defense Forum Cash Striplin Apache Business Development Mesa, Arizona Plant The Boeing Company August 12, 2014 Copyright 2014 - The Boeing Company Unpublished Work – All Rights Reserved Third Party Disclosure Requires Written Approval | 1 Apache Overview Boeing Military Aircraft | Vertical Lift History to the Apache Family 1948 – Howard Hughes launches first helicopter program, the XH-17 flying crane. 1963 – Hughes OH-6A, forerunner of MD 500 Series, makes first flight. 1975 – First AH-64 Apache prototype makes first flight. 1982 – Hughes Helicopters, Inc. opens Mesa, Arizona, facility 1984 – McDonnell Douglas Corporation purchases Hughes Helicopters, Inc. 1986 – McDonnell Douglas moves helicopter headquarters from Culver City, California to Mesa. 1993 – McDonnell Douglas Helicopter Company becomes McDonnell Douglas Helicopter Systems. 1997 – McDonnell Douglas merges with The Boeing Company. Rotorcraft operations are in Philadelphia & Mesa. Copyright 2014 - The Boeing Company Unpublished Work – All Rights Reserved Third Party Disclosure Requires Written Approval | 2 1 The Aerospace & Defense Forum Arizona Chapter August 12, 2014 Apache Overview Boeing Military Aircraft | Vertical Lift Quote from my Dad: Boy Scout Troop 427 - 1961: A plan that is not written down is just a day dream | 3 Apache Overview Boeing Military Aircraft | Vertical -
Military Helicopter Modernization: Background and Issues for Congress
Order Code RL32447 CRS Report for Congress Received through the CRS Web Military Helicopter Modernization: Background and Issues for Congress June 24, 2004 Christian F. M. Liles Research Associate Foreign Affairs, Defense and Trade Division Christopher Bolkcom Specialist in National Defense Foreign Affairs, Defense and Trade Division Congressional Research Service ˜ The Library of Congress Military Helicopter Modernization: Background and Issues for Congress Summary Recent military operations, particularly those in Afghanistan and Iraq, have brought to the fore a number of outstanding questions concerning helicopters in the U.S. armed forces, including deployability, safety, survivability, affordability, and operational effectiveness. These concerns are especially relevant, and made more complicated, in an age of “military transformation,” the “global war on terrorism,” and increasing pressure to rein in funding for the military, all of which provide contradictory pressures with regard to DOD’s large, and often complicated, military helicopter modernization efforts. Despite these questions, the military use of helicopters is likely to hold even, if not grow. This report includes a discussion of the evolving role of helicopters in military transformation. The Department of Defense (DOD) fields 10 different types of helicopters, which are largely of 1960s and 1970s design. This inventory numbers approximately 5,500 rotary-wing aircraft, not including an additional 144 belonging to the Coast Guard, and ranges from simple “utility” platforms such as the ubiquitous UH-1 “Huey” to highly-advanced, “multi-mission” platforms such as the Air Force’s MH- 53J “Pave Low” special operations helicopter and the still-developmental MV-22B “Osprey” tilt-rotor aircraft. Three general approaches can be taken to modernize DOD’s helicopter forces: upgrading current platforms, rebuilding current helicopter models (often called recapitalization), or procuring new models. -
Modeling the OH-6A Using FLIGHTLAB and Helicopter Simulator Considerations
Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection 2002-03 Modeling the OH-6A using FLIGHTLAB and helicopter simulator considerations Ouellette, Gregory A. Monterey, California. Naval Postgraduate School http://hdl.handle.net/10945/6038 NAVAL POSTGRADUATE SCHOOL Monterey, California THESIS MODELING THE OH-6A USING FLIGHTLAB AND HELICOPTER SIMULATOR CONSIDERATIONS by Gregory A. Ouellette March 2002 Thesis Advisor: E. Roberts Wood Second Reader: Russ W. Duren Approved for public release; distribution is unlimited. THIS PAGE INTENTIONALLY LEFT BLANK REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project (0704-0188) Washington DC 20503. 1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED March 2002 Master’s Thesis 4. TITLE AND SUBTITLE: Title (Mix case letters) 5. FUNDING NUMBERS Modeling The OH-6A Using FLIGHTLAB And Helicopter Simulator Considerations 6. AUTHOR(S) Gregory A. Ouellette 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION Naval Postgraduate School REPORT NUMBER Monterey, CA 93943-5000 9. SPONSORING / MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10. -
Boeing History Chronology Boeing Red Barn
Boeing History Chronology Boeing Red Barn PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 Boeing History Chronology PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 PRE -1910 1910 Los Angeles International Air Meet Museum of Flight Collection HOME PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 1881 Oct. 1 William Edward Boeing is born in Detroit, Michigan. 1892 April 6 Donald Wills Douglas is born in Brooklyn, New York. 1895 May 8 James Howard “Dutch” Kindelberger is born in Wheeling, West Virginia. 1898 Oct. 26 Lloyd Carlton Stearman is born in Wellsford, Kansas. 1899 April 9 James Smith McDonnell is born in Denver, Colorado. 1903 Dec. 17 Wilbur and Orville Wright make the first successful powered, manned flight in Kitty Hawk, North Carolina. 1905 Dec. 24 Howard Robard Hughes Jr. is born in Houston, Texas. 1907 Jan. 28 Elrey Borge Jeppesen is born in Lake Charles, Louisiana. HOME PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 1910 s Boeing Model 1 B & W seaplane HOME PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 1910 January Timber baron William E. Boeing attends the first Los Angeles International Air Meet and develops a passion for aviation. March 10 William Boeing buys yacht customer Edward Heath’s shipyard on the Duwamish River in Seattle. The facility will later become his first airplane factory. 1914 May Donald W. Douglas obtains his Bachelor of Science degree from the Massachusetts Institute of Technology (MIT), finishing the four-year course in only two years.