Advantageous Autorotation
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Future Battlefield Rotorcraft Capability (FBRC) – Anno 2035 and Beyond
November 2018 Future Battle eld Rotorcraft Capability Anno 2035 and Beyond Joint Air Power Competence Centre Cover picture © Airbus © This work is copyrighted. No part may be reproduced by any process without prior written permission. Inquiries should be made to: The Editor, Joint Air Power Competence Centre (JAPCC), [email protected] Disclaimer This document is a product of the Joint Air Power Competence Centre (JAPCC). It does not represent the opinions or policies of the North Atlantic Treaty Organization (NATO) and is designed to provide an independent overview, analysis and food for thought regarding possible ways ahead on this subject. Comments and queries on this document should be directed to the Air Operations Support Branch, JAPCC, von-Seydlitz-Kaserne, Römerstraße 140, D-47546 Kalkar. Please visit our website www.japcc.org for the latest information on JAPCC, or e-mail us at [email protected]. Author Cdr Maurizio Modesto (ITA Navy) Release This paper is releasable to the Public. Portions of the document may be quoted without permission, provided a standard source credit is included. Published and distributed by The Joint Air Power Competence Centre von-Seydlitz-Kaserne Römerstraße 140 47546 Kalkar Germany Telephone: +49 (0) 2824 90 2201 Facsimile: +49 (0) 2824 90 2208 E-Mail: [email protected] Website: www.japcc.org Denotes images digitally manipulated JAPCC |Future BattlefieldRotorcraft Capability and – AnnoBeyond 2035 | November 2018 Executive Director, JAPCC Director, Executive DEUAF General, Lieutenant Klaus Habersetzer port Branchviae-mail [email protected]. AirOperationsSup contact to theJAPCC’s free feel thisdocument.Please to withregard have you may comments welcome any We thisstudy. -
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27
A B C D E F 1 A012 A03009 125 DOMINIE 1.72 AIRCRAFT 2 A009 A05871 1804 STEAM LOCO 1.32 STEAM ENGINE 3 A013 A02447 1905 ROLLS ROYCE 1.32 CAR 4 A002 A02444 1911 ROLLS ROYCE 1.32 CAR 5 A002 A02443 1912 MODEL T FORD 1.32 CAR 6 A002 A02450 1926 MORRIS COWLEY 1.32 CAR 7 A002 A02446 1930 BENTLEY 1.32 CAR 8 ROB A20440 1930 BENTLEY 1.12 CAR 9 A028 A08440 1932 CHRYSLER IMPERIAL 1.25 CAR 10 A002 A02441 1933 ALFA ROMEO 1.32 CAR 11 A002 A01305 25PDR FIELD GUN & MORRIS QUAD 1.76 VEHICLE 12 ROB A02552 2ND DRAGOON 1815 54MM FIGURE 13 ROB 50 YEARS OF THE GREATEST PLASTIC KITS BOOK 14 A013 A02303 88MM GUN & TRACTOR 1.76 VEHICLE 15 ROB A02303 88MM GUN & TRACTOR (D-DAY) 1.76 VEHICLE 16 A026 A06012 A-10 THUNDERBOLT II 1.72 AIRCRAFT 17 ROB ITALERI 097 A-10 WARTHOG 1.72 AIRCRAFT 18 A026 REVELL 04206 A300-600 ST BELUGA 1144 AIRCRAFT 19 A008 A01028 A6M2 ZERO (VJ DAY) 1.72 AIRCRAFT 20 ROB A50127 A6M2B -21 (2011) 1.72 AIRCRAFT PAINTS IN BOX 21 ROB A01005 A6M2B ZERO 1.72 AIRCRAFT 22 A031 REVELL 4366 A-7A CORSAIR 1.72 AIRCRAFT 23 A007 A04211 ADMIRAL GRAF SPEE 1600 SHIP 24 ROB A01314 AEC MATADOR (D-DAY) 1.76 VEHICLE 25 A026 A04046 AH-1 T SEA COBRA 1.72 HELICOPTER 26 A005 A03077 AH-64 APACHE LONGBOW 1.72 HELICOPTER 27 A014 A07101 AH-64 APACHE LONGBOW 1.48 HELICOPTER 28 A026 A04044 AH-64 APACHE LONGBOW 1.72 HELICOPTER 29 A008 A02014 AICHI D3AI VAL (VJ DAY) 1.72 AIRCRAFT 30 ROB AIRFIX 1972 CATALOUGE BOOK 31 ROB AIRFIX 1974 CATALOUGE BOOK 32 ROB AIRFIX 1983 CATALOUGE BOOK 33 ROB A78183 AIRFIX 2007 CATALOUGE BOOK 34 ROB A78184 AIRFIX 2008 CATALOUGE BOOK 35 ROB AIRFIX CLUB -
Real-Time Helicopter Flight Control: Modelling and Control by Linearization and Neural Networks
Purdue University Purdue e-Pubs Department of Electrical and Computer Department of Electrical and Computer Engineering Technical Reports Engineering August 1991 Real-Time Helicopter Flight Control: Modelling and Control by Linearization and Neural Networks Tobias J. Pallett Purdue University School of Electrical Engineering Shaheen Ahmad Purdue University School of Electrical Engineering Follow this and additional works at: https://docs.lib.purdue.edu/ecetr Pallett, Tobias J. and Ahmad, Shaheen, "Real-Time Helicopter Flight Control: Modelling and Control by Linearization and Neural Networks" (1991). Department of Electrical and Computer Engineering Technical Reports. Paper 317. https://docs.lib.purdue.edu/ecetr/317 This document has been made available through Purdue e-Pubs, a service of the Purdue University Libraries. Please contact [email protected] for additional information. Real-Time Helicopter Flight Control: Modelling and Control by Linearization and Neural Networks Tobias J. Pallett Shaheen Ahmad TR-EE 91-35 August 1991 Real-Time Helicopter Flight Control: Modelling and Control by Lineal-ization and Neural Networks Tobias J. Pallett and Shaheen Ahmad Real-Time Robot Control Laboratory, School of Electrical Engineering, Purdue University West Lafayette, IN 47907 USA ABSTRACT In this report we determine the dynamic model of a miniature helicopter in hovering flight. Identification procedures for the nonlinear terms are also described. The model is then used to design several linearized control laws and a neural network controller. The controllers were then flight tested on a miniature helicopter flight control test bed the details of which are also presented in this report. Experimental performance of the linearized and neural network controllers are discussed. -
Assessment of Navy Heavy-Lift Aircraft Options
THE ARTS This PDF document was made available from www.rand.org as a public CHILD POLICY service of the RAND Corporation. CIVIL JUSTICE EDUCATION Jump down to document ENERGY AND ENVIRONMENT 6 HEALTH AND HEALTH CARE INTERNATIONAL AFFAIRS The RAND Corporation is a nonprofit research NATIONAL SECURITY POPULATION AND AGING organization providing objective analysis and effective PUBLIC SAFETY solutions that address the challenges facing the public SCIENCE AND TECHNOLOGY and private sectors around the world. SUBSTANCE ABUSE TERRORISM AND HOMELAND SECURITY TRANSPORTATION AND INFRASTRUCTURE Support RAND WORKFORCE AND WORKPLACE Purchase this document Browse Books & Publications Make a charitable contribution For More Information Visit RAND at www.rand.org Explore RAND National Defense Research Institute View document details Limited Electronic Distribution Rights This document and trademark(s) contained herein are protected by law as indicated in a notice appearing later in this work. This electronic representation of RAND intellectual property is provided for non- commercial use only. Permission is required from RAND to reproduce, or reuse in another form, any of our research documents for commercial use. This product is part of the RAND Corporation documented briefing series. RAND documented briefings are based on research briefed to a client, sponsor, or targeted au- dience and provide additional information on a specific topic. Although documented briefings have been peer reviewed, they are not expected to be comprehensive and may present preliminary findings. Assessment of Navy Heavy-Lift Aircraft Options John Gordon IV, Peter A. Wilson, Jon Grossman, Dan Deamon, Mark Edwards, Darryl Lenhardt, Dan Norton, William Sollfrey Prepared for the United States Navy Approved for public release; unlimited distribution The research described in this report was prepared for the United States Navy. -
Montgomerie-Bensen B8MR, G-BXDC
Montgomerie-Bensen B8MR, G-BXDC AAIB Bulletin No: 1/2001 Ref: EW/C2000/04/03 - Category: 2.3 Aircraft Type and Registration: Montgomerie-Bensen B8MR, G-BXDC No & Type of Engines: 1 Rotax 582 piston engine Year of Manufacture: 1999 Date & Time (UTC): 16 April 2000 at 1411 hrs Location: Carlisle Airport, Cumbria Type of Flight: Private Persons on Board: Crew - 1 - Passengers - None Injuries: Crew - 1 - Passengers - N/A Nature of Damage: Aircraft destroyed Commander's Licence: Private Pilot's Licence (gyroplanes) Commander's Age: 51 years Commander's Flying Experience: 67 hours (of which 30 were on type) Last 90 days - 44 hours Last 28 days - 43 hours Information Source: AAIB Field Investigation Background information The pilot first showed an active interest in autogyros when in March 1999 he visited Carlisle Airport for a trial lesson. He had not flown before and enjoyed the experience so much that he flew again the same day and agreed to embark on a formal training programme with an instructor who was authorised by the CAA to conduct dual and single seat autogyro training as well as flight examinations. The instructor reported that his student approached all matters to do with his flying 'with a great deal of enthusiasm and a fair degree of ability'. From the start of his course until January 2000 the pilot undertook dual instruction, mainly at weekends, on a two seater VPM M16 autogyro. By March 2000 he was sufficiently experienced to transfer to the 'open frame' single-seat Benson autogyro. He flew this for approximately 20 hours, carrying out mainly short 'hops' along the length of the runway and practising balancing on the main wheels before progressing to flying the aircraft in the visual circuit and carrying out general handling exercises. -
National Rappel Operations Guide
National Rappel Operations Guide 2019 NATIONAL RAPPEL OPERATIONS GUIDE USDA FOREST SERVICE National Rappel Operations Guide i Page Intentionally Left Blank National Rappel Operations Guide ii Table of Contents Table of Contents ..........................................................................................................................ii USDA Forest Service - National Rappel Operations Guide Approval .............................................. iv USDA Forest Service - National Rappel Operations Guide Overview ............................................... vi USDA Forest Service Helicopter Rappel Mission Statement ........................................................ viii NROG Revision Summary ............................................................................................................... x Introduction ...................................................................................................... 1—1 Administration .................................................................................................. 2—1 Rappel Position Standards ................................................................................. 2—6 Rappel and Cargo Letdown Equipment .............................................................. 4—1 Rappel and Cargo Letdown Operations .............................................................. 5—1 Rappel and Cargo Operations Emergency Procedures ........................................ 6—1 Documentation ................................................................................................ -
Book Reviews the SYCAMORE SEEDS
Afterburner Book Reviews THE SYCAMORE SEEDS Early British Helicopter only to be smashed the following night in a gale. The book then covers the Cierva story in some detail, the Development chapter including, out of context, two paragraphs on By C E MacKay the Brennan propeller-driven rotor driven helicopter [helicogyro] fl own in 1924 at Farnborough but Distributed by A MacKay, 87 Knightscliffe Avenue, aborted by the Air Ministry the next year, stating that Netherton, Glasgow G13 2RX, UK (E charlese87@ there was no future for the helicopter and backing btinternet.com). 2014. 218pp. Illustrated. £12.95. Cierva’s autogyro programme contracting Avro to build ISBN 978-0-9573443-3-4. the fi rst British machines. Good coverage is given to the range of Cierva autogyros culminating in the Avro Given the paucity of coverage of British helicopter C30 Rota and its service use by the RAF. development I approached this slim (218 A5 pp) The heart of the book begins with a quotation: publication with interest. While autogyros have been “Morris, I want you to make me blades, helicopter well documented, Charnov and Ord-Hume giving blades,” with which William Weir, the fi rst Air Minister, exhaustive and well documented treatments of the founder of the RAF and supporter of Cierva, brought helicopter’s predecessor, the transition to the directly furniture maker H Morris & Co into the history of driven rotor of the helicopter is somewhat lacking. rotorcraft pulling in designers Bennett, Watson, Unfortunately MacKay’s book only contributes a Nisbet and Pullin with test pilots Marsh and Brie fi nal and short chapter to the ‘British Helicopter’ to form his team. -
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. -
Helicopter Physics by Harm Frederik Althuisius López
Helicopter Physics By Harm Frederik Althuisius López Lift Happens Lift Formula Torque % & Lift is a mechanical aerodynamic force produced by the Lift is calculated using the following formula: 2 = *4 '56 Torque is a measure of how much a force acting on an motion of an aircraft through the air, it generally opposes & object causes that object to rotate. As the blades of a Where * is the air density, 4 is the velocity, '5 is the lift coefficient and 6 is gravity as a means to fly. Lift is generated mainly by the the surface area of the wing. Even though most of these components are helicopter rotate against the air, the air pushes back on the rd wings due to their shape. An Airfoil is a cross-section of a relatively easy to measure, the lift coefficient is highly dependable on the blades following Newtons 3 Law of Motion: “To every wing, it is a streamlined shape that is capable of generating shape of the airfoil. Therefore it is usually calculated through the angle of action there is an equal and opposite reaction”. This significantly more lift than drag. Drag is the air resistance attack of a specific airfoil as portrayed in charts much like the following: reaction force is translated into the fuselage of the acting as a force opposing the motion of the aircraft. helicopter via torque, and can be measured for individual % & -/ 0 blades as follows: ! = #$ = '()*+ ∫ # 1# , where $ is the & -. Drag Force. As a result the fuselage tends to rotate in the Example of a Lift opposite direction of its main rotor spin. -
National Advisory Committee for Aeronautics
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS TECHNICAL NOTE 2154 AN ANALYSIS OF TIlE AUTOROTATIVE PERFORMANCE OF A BELICOPTER POWERED BY ROTOR-TIP JET UN[TS By Alfred Gessow Langley Aeronautical Laboratory Langley Air Force Base, Va. Washington July 1950 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS TECHNICAL NOTE 2l AN ANALYSIS OF THE AUTOROTATIVE PERFORMANCE OF A HELICOPTER POWERED BY ROTOR-TIP JET UNITS By Alfred Gessow SUMMARY The autorotative performance of an assumed helicopter was studied to determine the effect of inoperative jet units located at the rotor- blade tip on the helicopter rate of descent. For a representative ram- jet design, the effect of the jet drag is to increase the minimum rate of descent of the helicopter from about l,OO feet per minute to 3,700 feet per minute when the rotor is operating at a tip speed of approximately 600 feet per second. The effect is less if the rotor operates at lower tip speeds, but the rotor kinetic energy and the stall margin available for the landing maneuver are then reduced. Power-off rates of descent of pulse-jet helicopters would be expected to be less than those of ram- jet.helicopters because pulse jets of current design appear to have greater ratios of net power-on thrust to power-off, drag than currently designed rain jets. Iii order to obtain greater accuracy in studies of autorotative per- forimance, calculations in'volving high power-off rates of descent should include the weight-supporting effect of the fuselage parasite-drag force and the fact that the rotor thrust does not equal the weight of the helicopter. -
Helicopter Flying Handbook (FAA-H-8083-21B) Chapter 8
Chapter 8 Ground Procedures and Flight Preparations Introduction Once a pilot takes off, it is up to him or her to make sound, safe decisions throughout the flight. It is equally important for the pilot to use the same diligence when conducting a preflight inspection, making maintenance decisions, refueling, and conducting ground operations. This chapter discusses the responsibility of the pilot regarding ground safety in and around the helicopter and when preparing to fly. 8-1 Preflight There are two primary methods of deferring maintenance on rotorcraft operating under part 91. They are the deferral Before any flight, ensure the helicopter is airworthy by provision of 14 CFR part 91, section 91.213(d) and an FAA- inspecting it according to the rotorcraft flight manual (RFM), approved MEL. pilot’s operating handbook (POH), or other information supplied either by the operator or the manufacturer. The deferral provision of 14 CFR section 91.213(d) is Remember that it is the responsibility of the pilot in command widely used by most pilot/operators. Its popularity is due (PIC) to ensure the aircraft is in an airworthy condition. to simplicity and minimal paperwork. When inoperative equipment is found during preflight or prior to departure, the In preparation for flight, the use of a checklist is important decision should be to cancel the flight, obtain maintenance so that no item is overlooked. [Figure 8-1] Follow the prior to flight, determine if the flight can be made under the manufacturer’s suggested outline for both the inside and limitations imposed by the defective equipment, or to defer outside inspection. -
Paper Helicopters Preparation
Paper Helicopters Preparation CLASS LEVEL First – sixth class OBJECTIVES Content Strand and Strand Unit Energy & forces, Forces Through investigation the child should be enabled to come to appreciate that gravity is a force, SESE: Science Curriculum page 87. In this activity children explore how some things fall and how varying the size of the rotor blades, the shape of the rotor blades and the weight of a paper helicopter affect the way a helicopter spins. Skill development Through completing the strand units of the science curriculum the child should be enabled to design, plan and carry out simple experiments, having regard to one or two variables and the need to sequence tasks and tests, SESE: Science Curriculum page 79. This activity helps them understand fair testing by changing only one variable (i.e. shape only or length only) at a time. Investigating; experimenting; observing; analysing; measuring/timing; recording and communicating. CURRICULUM LINKS Mathematics Data / representing and interpreting data SESE: History Continuity and change over time/ technological and scientific developments over long periods BACKGROUND A previous activity on how things fall (i.e. the weight of the object is not a factor – Galileo and the Leaning Tower of Pisa) would help understanding of this activity, but not essential. MATERIALS/EQUIPMENT Paper, Ruler, Paper Clips, Scissors Templates of different sizes PREPARATION Test out a few thicknesses of paper/cardboard first to see that some of them spin. BACKGROUND The shape of the helicopter rotor blades make it spin INFORMATION when dropped from a height. Gravity pulls the helicopter down. The air resists the movement and pushes up each rotor separately, causing the helicopter to spin.