The Reality of Aeronautical Knowledge: the Analysis of Accident Reports Against What Aircrews Are Supposed to Know
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Shipboard Operations
FM 1-564 SHIPBOARD OPERATIONS HEADQUARTERS, DEPARTMENT OF THE ARMY DISTRIBUTION RESTRICTION: Approved for public release; distribution is unlimited. Field Manual *FM1-564 No. 1-564 Headquarters Department of the Army Washington, DC, 29 June 1997 SHIPBOARD OPERATIONS Contents PREFACE CHAPTER 1. PREDEPLOYMENT PLANNING Section 1. Mission Analysis 1-1. Preparation 1-1 1-2. Mission Definition 1-1 1-3. Shipboard Helicopter Training Requirements 1-2 1-4. Service Responsibilities 1-2 1-5. Logistics 1-3 Section 2. Presail Conference 1-6. Coordination 1-7 1-7. Number of Army Aircraft on Board the Ship 1-7 1-8. Checklist 1-7 Section 3. Training Requirements 1-9. Aircrew Requirements for Training 1-9 1-10. Ground School Training 1-11 1-11. Initial Qualification and Currency Requirements 1-11 1-12. Ship Certification and Waiver 1-15 1-13. Detachment Certification 1-15 CHAPTER 2. PREPARATION FOR FLIGHT OPERATIONS Section 1. Chain of Command 2-1. Command Relationship 2-1 2-2. Special Operations 2-2 2-3. Augmentation Support 2-2 Section 2. Personnel Responsibilities 2-4. Flight Quarters Stations 2-3 2-5. Landing Signal Enlisted 2-4 DISTRIBUTION RESTRICTION: Approved for public release; distribution is unlimited. i Section 3. Aircraft Handling 2-6. Fundamentals 2-4 2-7. Helicopter Recovery Tie-Down Procedures 2-5 Section 4. The Air Plan 2-8. Scope 2-5 2-9. Contents 2-6 2-10. Maintenance Test Flights 2-7 2-11. Flight Plan 2-7 2-12. Aqueous Film-Forming Foam System and Mobile Firefighting Equipment 2-7 CHAPTER 3. -
Helicopter Dynamics Concerning Retreating Blade Stall on a Coaxial Helicopter
Helicopter Dynamics Concerning Retreating Blade Stall on a Coaxial Helicopter A project presented to The Faculty of the Department of Aerospace Engineering San José State University In partial fulfillment of the requirements for the degree Master of Science in Aerospace Engineering by Aaron Ford May 2019 approved by Prof. Jeanine Hunter Faculty Advisor © 2019 Aaron Ford ALL RIGHTS RESERVED ABSTRACT Helicopter Dynamics Concerning Retreating Blade Stall on a Coaxial Helicopter by Aaron Ford A model of helicopter blade flapping dynamics is created to determine the occurrence of retreating blade stall on a coaxial helicopter with pusher-propeller in straight and level flight. Equations of motion are developed, and blade element theory is utilized to evaluate the appropriate aerodynamics. Modelling of the blade flapping behavior is verified against benchmark data and then used to determine the angle of attack distribution about the rotor disk for standard helicopter configurations utilizing both hinged and hingeless rotor blades. Modelling of the coaxial configuration with the pusher-prop in straight and level flight is then considered. An approach was taken that minimizes the angle of attack and generation of lift on the advancing side while minimizing them on the retreating side of the rotor disk. The resulting asymmetric lift distribution is compensated for by using both counter-rotating rotor disks to maximize lift on their respective advancing sides and reduce drag on their respective retreating sides. The result is an elimination of retreating blade stall in the coaxial and pusher-propeller configuration. Finally, an assessment of the lift capability of the configuration at both sea level and at “high and hot” conditions were made. -
Adventures in Low Disk Loading VTOL Design
NASA/TP—2018–219981 Adventures in Low Disk Loading VTOL Design Mike Scully Ames Research Center Moffett Field, California Click here: Press F1 key (Windows) or Help key (Mac) for help September 2018 This page is required and contains approved text that cannot be changed. NASA STI Program ... in Profile Since its founding, NASA has been dedicated • CONFERENCE PUBLICATION. to the advancement of aeronautics and space Collected papers from scientific and science. The NASA scientific and technical technical conferences, symposia, seminars, information (STI) program plays a key part in or other meetings sponsored or co- helping NASA maintain this important role. sponsored by NASA. The NASA STI program operates under the • SPECIAL PUBLICATION. Scientific, auspices of the Agency Chief Information technical, or historical information from Officer. It collects, organizes, provides for NASA programs, projects, and missions, archiving, and disseminates NASA’s STI. The often concerned with subjects having NASA STI program provides access to the NTRS substantial public interest. Registered and its public interface, the NASA Technical Reports Server, thus providing one of • TECHNICAL TRANSLATION. the largest collections of aeronautical and space English-language translations of foreign science STI in the world. Results are published in scientific and technical material pertinent to both non-NASA channels and by NASA in the NASA’s mission. NASA STI Report Series, which includes the following report types: Specialized services also include organizing and publishing research results, distributing • TECHNICAL PUBLICATION. Reports of specialized research announcements and feeds, completed research or a major significant providing information desk and personal search phase of research that present the results of support, and enabling data exchange services. -
Shipboard Operations
FM 1-564 SHIPBOARD OPERATIONS HEADQUARTERS, DEPARTMENT OF THE ARMY DISTRIBUTION RESTRICTION: Approved for public release; distribution is unlimited. Field Manual *FM1-564 No. 1-564 Headquarters Department of the Army Washington, DC, 29 June 1997 SHIPBOARD OPERATIONS Contents PREFACE CHAPTER 1. PREDEPLOYMENT PLANNING Section 1. Mission Analysis 1-1. Preparation 1-1 1-2. Mission Definition 1-1 1-3. Shipboard Helicopter Training Requirements 1-2 1-4. Service Responsibilities 1-2 1-5. Logistics 1-3 Section 2. Presail Conference 1-6. Coordination 1-7 1-7. Number of Army Aircraft on Board the Ship 1-7 1-8. Checklist 1-7 Section 3. Training Requirements 1-9. Aircrew Requirements for Training 1-9 1-10. Ground School Training 1-11 1-11. Initial Qualification and Currency Requirements 1-11 1-12. Ship Certification and Waiver 1-15 1-13. Detachment Certification 1-15 CHAPTER 2. PREPARATION FOR FLIGHT OPERATIONS Section 1. Chain of Command 2-1. Command Relationship 2-1 2-2. Special Operations 2-2 2-3. Augmentation Support 2-2 Section 2. Personnel Responsibilities 2-4. Flight Quarters Stations 2-3 2-5. Landing Signal Enlisted 2-4 DISTRIBUTION RESTRICTION: Approved for public release; distribution is unlimited. i Section 3. Aircraft Handling 2-6. Fundamentals 2-4 2-7. Helicopter Recovery Tie-Down Procedures 2-5 Section 4. The Air Plan 2-8. Scope 2-5 2-9. Contents 2-6 2-10. Maintenance Test Flights 2-7 2-11. Flight Plan 2-7 2-12. Aqueous Film-Forming Foam System and Mobile Firefighting Equipment 2-7 CHAPTER 3. -
Over Thirty Years After the Wright Brothers
ver thirty years after the Wright Brothers absolutely right in terms of a so-called “pure” helicop- attained powered, heavier-than-air, fixed-wing ter. However, the quest for speed in rotary-wing flight Oflight in the United States, Germany astounded drove designers to consider another option: the com- the world in 1936 with demonstrations of the vertical pound helicopter. flight capabilities of the side-by-side rotor Focke Fw 61, The definition of a “compound helicopter” is open to which eclipsed all previous attempts at controlled verti- debate (see sidebar). Although many contend that aug- cal flight. However, even its overall performance was mented forward propulsion is all that is necessary to modest, particularly with regards to forward speed. Even place a helicopter in the “compound” category, others after Igor Sikorsky perfected the now-classic configura- insist that it need only possess some form of augment- tion of a large single main rotor and a smaller anti- ed lift, or that it must have both. Focusing on what torque tail rotor a few years later, speed was still limited could be called “propulsive compounds,” the following in comparison to that of the helicopter’s fixed-wing pages provide a broad overview of the different helicop- brethren. Although Sikorsky’s basic design withstood ters that have been flown over the years with some sort the test of time and became the dominant helicopter of auxiliary propulsion unit: one or more propellers or configuration worldwide (approximately 95% today), jet engines. This survey also gives a brief look at the all helicopters currently in service suffer from one pri- ways in which different manufacturers have chosen to mary limitation: the inability to achieve forward speeds approach the problem of increased forward speed while much greater than 200 kt (230 mph). -
2017 Top Markets Report Rotorcraft Sector Snapshot
U.S. Department of Commerce International Trade Administration 2017 Top Markets Report Rotorcraft Sector Snapshot Rotorcraft Helicopters, also known as rotorcraft, offer a versatility not Grouping MTOW afforded by automobiles and fixed-wing airplanes. Able to access the inaccessible with significant speed and comfort, a Light single engine <4,000 lbs. rotorcraft is the optimal choice for many enforcement, Intermediate single >4,000 lbs. emergency, and executive endeavors. The industry also engine includes maintenance, repair, and overhaul (MRO) of rotorcraft. Light twin engine <9,000 lbs. Medium twin engine between 9000- The helicopter industry is segmented into six groups, which 15,000 lbs. are dependent on the number of engines and maximum Super-medium twin between 15,000- take-off weight (MTOW), as described in Figure 1 to the right. engine 20,000 lbs. Heavy twin engine >20,000 lbs. The helicopter industry can also be segmented into the Figure 1 following usage categories: • General Aviation (Business/Private/VIP) • Law Enforcement • Emergency Medical Services (EMS)/ Search & Rescue (SAR) • Utility • Oil & Gas/Offshore • Defense Global Industry Landscape The major rotorcraft design and production companies are either North American (U.S. and Canada) or European (France, Italy, and Russia). While the major companies are headquartered in these countries, many production and parts-production facilities are in operation throughout Asia and Latin America. Similarly, the major markets for civil and defense rotorcraft are nations in North America and Europe, which constitute approximately 55 percent of the global market. 2017 ITA Rotorcraft Top M arkets Report 1 This snapshot is part of a larger Top Markets Report. -
Rotor Spring 2018
Departments Features Index of Advertisers Spring 2018 rotor.org Serving the International BY THE INDUSTRY Helicopter Community FOR THE INDUSTRY Grand Canyon Helitack The Best Job in Aviation? What’s In Your Jet Fuel? p 58 Vietnam Pilots and Crew Members Honored p 28 Make the Connection March 4–7, 2019 • Atlanta Georgia World Congress Center Exhibits Open March 5–7 Apply for exhibit space at heliexpo.rotor.org LOTTERY 1* Open to HAI HELI-EXPO 2018 Exhibitors APPLY BY June 22, 2018 WITH PAYMENT LOTTERY 2 Open to All Companies APPLY BY Aug. 10, 2018 WITH PAYMENT heliexpo.rotor.org * For information on how to upgrade within Lottery 1, contact [email protected]. EXHIBIT NOW FALCON CREST AVIATION PROUDLY SUPPLIES & MAINTAINS AVIATION’S BEST SEALED LEAD ACID BATTERY RG-380E/44 RG-355 RG-214 RG-222 RG-390E RG-427 RG-407 RG-206 Bell Long Ranger Bell 212, 412, 412EP Bell 407 RG-222 (17 Ah) or RG-224 (24 Ah) RG-380E/44 (42 Ah) RG-407A1 (27 Ah) Falcon Crest STC No. SR09069RC Falcon Crest STC No. SR09053RC Falcon Crest STC No. SR09359RC Airbus Helicopters Bell 222U Airbus Helicopters AS355 E, F, F1, F2, N RG-380E/44 (42 Ah) BK 117, A-1, A-3, A-4, B-1, B-2, C-1 RG-355 (17 Ah) Falcon Crest STC No. SR09142RC RG-390E (28 Ah) Falcon Crest STC No. SR09186RC Falcon Crest STC No. SR09034RC Sikorsky S-76 A, C, C+ Airbus Helicopters RG-380E/44 (42 Ah) Airbus Helicopters AS350B, B1, B2, BA, C, D, D1 Falcon Crest STC No. -
Helicopter Safety July-August 1991
F L I G H T S A F E T Y F O U N D A T I O N HELICOPTER SAFETY Vol. 17 No. 4 For Everyone Concerned with the Safety of Flight July/August 1991 The Philosophy and Realities of Autorotations Like the power-off glide in a fixed-wing aircraft, the autorotation in a helicopter must be used properly if it is to be a successful safety maneuver. by Michael K. Hynes Aviation Consultant In all helicopter flying, there is no single event that has a In the early years of airplane flight, the fear of engine greater impact on safety than the autorotation maneuver. failure, or that the airplane might have structural prob- The mere mention of the word “autorotation” at any lems during flight, was very strong. If either of these gathering of helicopter pilots, especially flight instruc- events took place, the pilot’s ability to get the airplane tors, will guarantee a long and lively discussion. safely on the ground quickly was important. The time it took to get the airplane on the ground was directly in There are many misconceptions about autorotations and proportion to the altitude at which the airplane was being they contribute to the accident rate when an autorotation flown. It is therefore logical that all early flights were precedes a helicopter landing accident. One approach to flown at low altitudes, often at less than 500 feet above a discussion of autorotations is to look at the subject the ground (agl). from three views: first, the philosophy of the subject; second, the reality of the circumstances that require au- At these low altitudes, the pilot did not always have the torotations; and third, the execution of the maneuver. -
DYNAMIC MODELING of AUTOROTATION for SIMULTANEOUS LIFT and WIND ENERGY EXTRACTION by SADAF MACKERTICH B.S. Rochester Institute O
DYNAMIC MODELING OF AUTOROTATION FOR SIMULTANEOUS LIFT AND WIND ENERGY EXTRACTION by SADAF MACKERTICH B.S. Rochester Institute of Technology, 2012 A thesis submitted in partial fulfilment of the requirements for the degree of Master of Science in the Department of Mechanical and Aerospace Engineering in the College of Engineering and Computer Science at the University of Central Florida Orlando, Florida Spring Term 2016 Major Professor: Tuhin Das c 2016 Sadaf Mackertich ii ABSTRACT The goal of this thesis is to develop a multi-body dynamics model of autorotation with the objective of studying its application in energy harvesting. A rotor undergoing autorotation is termed an Autogyro. In the autorotation mode, the rotor is unpowered and its interaction with the wind causes an upward thrust force. The theory of an autorotating rotorcraft was originally studied for achieving safe flight at low speeds and later used for safe descent of helicopters under engine failure. The concept can potentially be used as a means to collect high-altitude wind energy. Autorotation is inherently a dynamic process and requires detailed models for characterization. Existing models of autorotation assume steady operating conditions with constant angu- lar velocity of the rotor. The models provide spatially averaged aerodynamic forces and torques. While these steady-autorotation models are used to create a basis for the dynamic model developed in this thesis, the latter uses a Lagrangian formulation to determine the equations of motion. The aerodynamic effects on the blades that produce thrust forces, in- plane torques, and out-of-plane torques, are modeled as non-conservative forces within the Lagrangian framework. -
FY 06 Aviation Accident Review
DOIDOI FYFY 0606 AviationAviation MishapsMishaps 44 AircraftAircraft AccidentsAccidents TheThe lossloss ofof oneone lifelife OneOne serious,serious, andand threethree minorminor injuriesinjuries 1212 IncidentsIncidents withwith PotentialPotential DOIDOI FYFY 0606 AviationAviation MishapsMishaps NTSB 831.13 Flow and dissemination of accident or incident information. (b) … Parties to the investigation may relay to their respective organizations information necessary for purposes of prevention or remedial action. … However, no (release of) information… without prior consultation and approval of the NTSB. ThisThis informationinformation isis providedprovided forfor accidentaccident preventionprevention purposespurposes onlyonly Fairbanks,Fairbanks, AKAK OctoberOctober 6,6, 20052005 Husky A-1B Mission Resource Clinic Training Damage Substantial Injuries None Procurement Fleet NTSB ID ANC06TA002 Fairbanks,Fairbanks, AKAK OctoberOctober 6,6, 20052005 Issues Mission briefing Cockpit communications Distraction Crew Selection Training standards and program objectives NTSBNTSB ProbableProbable CauseCause Fairbanks,Fairbanks, AK,AK, October October 6,6, 20052005 The National Probable Cause Transportation Safety Board determined that “The flight instructor's the probable cause of inadequate supervision of the dual this accident was … student during the landing roll, which resulted in the dual student applying the brakes excessively, and the airplane nosing over. A factor associated with the accident was the excessive braking by the dual student.” FAI -
(12) United States Patent (10) Patent No.: US 8,991,744 B1 Khan (45) Date of Patent: Mar
USOO899.174.4B1 (12) United States Patent (10) Patent No.: US 8,991,744 B1 Khan (45) Date of Patent: Mar. 31, 2015 (54) ROTOR-MAST-TILTINGAPPARATUS AND 4,099,671 A 7, 1978 Leibach METHOD FOR OPTIMIZED CROSSING OF 35856 A : 3. Wi NATURAL FREQUENCIES 5,850,6154. W-1 A 12/1998 OSderSO ea. 6,099.254. A * 8/2000 Blaas et al. ................... 416,114 (75) Inventor: Jehan Zeb Khan, Savoy, IL (US) 6,231,005 B1* 5/2001 Costes ....................... 244f1725 6,280,141 B1 8/2001 Rampal et al. (73) Assignee: Groen Brothers Aviation, Inc., Salt 6,352,220 B1 3/2002 Banks et al. Lake City, UT (US) 6,885,917 B2 4/2005 Osder et al. s 7,137,591 B2 11/2006 Carter et al. (*) Notice: Subject to any disclaimer, the term of this 16. R 1239 sign patent is extended or adjusted under 35 2004/0232280 A1* 11/2004 Carter et al. ............... 244f1725 U.S.C. 154(b) by 494 days. OTHER PUBLICATIONS (21) Appl. No.: 13/373,412 John Ballard etal. An Investigation of a Stoppable Helicopter Rotor (22) Filed: Nov. 14, 2011 with Circulation Control NASA, Aug. 1980. Related U.S. Application Data (Continued) (60) Provisional application No. 61/575,196, filed on Aug. hR". application No. 61/575,204, Primary Examiner — Joseph W. Sanderson • Y-s (74) Attorney, Agent, or Firm — Pate Baird, PLLC (51) Int. Cl. B64C 27/52 (2006.01) B64C 27/02 (2006.01) (57) ABSTRACT ;Sp 1% 3:08: A method and apparatus for optimized crossing of natural (52) U.S. -
Development of a Helicopter Vortex Ring State Warning System Through a Moving Map Display Computer
Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection 1999-09 Development of a helicopter vortex ring state warning system through a moving map display computer Varnes, David J. Monterey, California. Naval Postgraduate School http://hdl.handle.net/10945/26475 DUDLEY KNOX LIBRARY NAVAL POSTGRADUATE SCHOOL MONTEREY CA 93943-5101 NAVAL POSTGRADUATE SCHOOL Monterey, California THESIS DEVELOPMENT OF A HELICOPTER VORTEX RING STATE WARNING SYSTEM THROUGH A MOVING MAP DISPLAY COMPUTER by David J. Varnes September 1999 Thesis Advisor: Russell W. Duren Approved for public release; distribution is unlimited. 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. REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED 1. agency use only (Leave blank) September 1999 Master's Thesis 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS DEVELOPMENT OF A HELICOPTER VORTEX RING STATE WARNING SYSTEM THROUGH A MOVING MAP DISPLAY COMPUTER 6. AUTHOR(S) Varnes, David, J. 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) PERFORMING ORGANIZATION Naval Postgraduate School REPORT NUMBER Monterey, CA 93943-5000 10.