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3-VIEWS - TABLE of CONTENTS to Search: Hold "Ctrl" Key Then Press "F" Key
3-VIEWS - TABLE of CONTENTS To search: Hold "Ctrl" key then press "F" key. Enter manufacturer or model number in search box. Click your back key to return to the search page. It is highly recommended to read Order Instructions and Information pages prior to selection. Aircraft MFGs beginning with letter A ................................................................. 3 B ................................................................. 6 C.................................................................10 D.................................................................14 E ................................................................. 17 F ................................................................. 18 G ................................................................21 H................................................................. 23 I .................................................................. 26 J ................................................................. 26 K ................................................................. 27 L ................................................................. 28 M ................................................................30 N................................................................. 35 O ................................................................37 P ................................................................. 38 Q ................................................................40 R................................................................ -
Cessna 172 in Flight 1964 Cessna 172E 1965 Cessna F172G
Cessna 172 in flight 1964 Cessna 172E 1965 Cessna F172G 1971 Cessna 172 The 1957 model Cessna 172 Skyhawk had no rear window and featured a "square" fin design Airplane Cessna 172 single engine aircraft, flies overhead after becoming airborne. Catalina Island airport, California (KAVX) 1964 Cessna 172E (G- ASSS) at Kemble airfield, Gloucestershire, England. The Cessna 172 Skyhawk is a four-seat, single-engine, high-wing airplane. Probably the most popular flight training aircraft in the world, the first production models were delivered in 1957, and it is still in production in 2005; more than 35,000 have been built. The Skyhawk's main competitors have been the popular Piper Cherokee, the rarer Beechcraft Musketeer (no longer in production), and, more recently, the Cirrus SR22. The Skyhawk is ubiquitous throughout the Americas, Europe and parts of Asia; it is the aircraft most people visualize when they hear the words "small plane." More people probably know the name Piper Cub, but the Skyhawk's shape is far more familiar. The 172 was a direct descendant of the Cessna 170, which used conventional (taildragger) landing gear instead of tricycle gear. Early 172s looked almost identical to the 170, with the same straight aft fuselage and tall gear legs, but later versions incorporated revised landing gear, a lowered rear deck, and an aft window. Cessna advertised this added rear visibility as "Omnivision". The final structural development, in the mid-1960s, was the sweptback tail still used today. The airframe has remained almost unchanged since then, with updates to avionics and engines including (most recently) the Garmin G1000 glass cockpit. -
Unit – I - Elements of Helicopter Aerodynamics – Sae1608
SCHOOL OF MECHANICAL ENGINEERING DEPARTMENT OF AERONAUTICAL ENGINEERING UNIT – I - ELEMENTS OF HELICOPTER AERODYNAMICS – SAE1608 I. INTRODUCTION Principles of Flight A helicopter is a heavier than air flying machine that has a lifting force created by a main rotor according to aerodynamic principles. The basic components of a helicopter are as follows • Main rotor. Put in motion by the power plant (engine). • Fuselage. Intended for accommodation of crew, passengers, equipment and cargo. • Landing gear, that is, arrangement intended for movement over the ground /6 or for parking. • Tail rotor. Provides directional equilibrium and directional control of the helicopter. • Propulsion system which sets in motion the lifting and tail rotors and auxiliary systems. • Transmission transfers the torque from the power plant to the main and tail rotors. Fig.1 2 • Flight is possible for a flying machine if there is a lifting force counterbalancing its weight. • The lifting force of the helicopter originates at the main rotor. By the rotation of the main rotor in the air a thrust force is developed perpendicular to the plane of rotor rotation. • If the main rotor rotates in the horizontal plane, then its thrust force T is directed vertically upwards (Figure 2), that is, vertical flight is possible. Figure 2: Vertical Flight • The characteristics of the flight depend on the correlation between the thrust force of the main rotor and the weight of the helicopter. • If the thrust force equals the weight of the helicopter, then it will remain motionless in the air. • If, though, the thrust force is greater than the weight, then the helicopter will pass from being motionless into a vertical climb. -
VTOL Hybrids: Tiltrotors Are Gaining Acceptance Nihad E Daidzic,, Ph.D., Sc.D
Minnesota State University, Mankato From the SelectedWorks of Nihad E. Daidzic, Dr.-Ing., D.Sc., ATP, CFII, MEI February, 2017 VTOL hybrids: Tiltrotors are gaining acceptance Nihad E Daidzic,, Ph.D., Sc.D. This work is licensed under a Creative Commons CC_BY-NC-ND International License. Available at: https://works.bepress.com/nihad-daidzic/30/ VTOL HYBRIDS Tiltrotors are gaining acceptance Led by Bell’s XV3 and XV15 and military service-proven Bell-Boeing V22, Leonardo will market the AW609 with other wing & rotor hybrids forthcoming. ry-wing VTOL aircraft that can hov- er, ly vertically up and down, and ly forward, sideways and backward – simply amazing machines. Heli- copters produce thrust as a vector component of the total lift force by effectively tilting the main rotor disc. Gyroplanes, on the other hand, 1st lown in 1923, are hybrids between helicopters and airplanes in which case the lift-producing rotary-wing is in the constant state of autorota- tion (windmilling), while horizontal thrust is normally produced by an internal combustion engine driving conventional propellers. So why do Photo courtesy Leonardo we need yet another airplane-heli- Leonardo AW609, jointly developed by Bell Helicopter and AgustaWestland, holds promise to be copter crossbreed? We need it be- the 1st tiltrotor aircraft certified for civilian operations. Configuration options include corporate, cause helicopters and gyroplanes SAR and EMS. Projected max range is 1100 nm with aux fuel tank, cruise speed of up to 275 kts. are limited by low cruising airspeeds and ranges, while airplanes are not By Nihad Daidzic, PhD, ScD cipal innovations in the published VTOL-capable. -
PROGRAM #Aiaascitech
9–13 JANUARY 2017 GRAPEVINE, TX Addressing Full Spectrum Disruptions Across the Global Aerospace Community PROGRAM www.aiaa-SciTech.org #aiaaSciTech 17-4000 WHAT’S IMPOSSIBLE TODAY WON’T BE TOMORROW. AT LOCKHEED MARTIN, WE’RE ENGINEERING A BETTER TOMORROW. We are partnering with our customers to accelerate manufacturing innovation from the laboratory to production. We push the limits in additive manufacturing, advanced materials, digital manufacturing and next generation electronics. Whether it is solving a global crisis like the need for clean drinking water or travelling even deeper into space, advanced manufacturing is opening the doors to the next great human revolution. Learn more at lockheedmartin.com © 2014 LOCKHEED MARTIN CORPORATION VC377_164 Executive Steering Committee AIAA SciTech Forum Welcome Welcome to the 2017 AIAA Science and Technology Forum and Exposition (AIAA SciTech Forum) – the world’s largest event for aerospace research, development, and technology! Only here will you find the diversity of topics, caliber of speakers, and level of discourse about issues that directly impact your work, your career, and your industry – we are confident you will leave Grapevine prepared to shape the future of aerospace in new and exciting ways. Chuck Gustafson Jill Marlowe By bringing together 11 aerospace science and technology conferences, and by attracting attendees The Aerospace NASA Langley from across academia, industry, and government, AIAA SciTech will give you an unparalleled Corporation Research Center opportunity to hear from industry thought leaders, interact with your peers, and begin the inspired exchange of ideas that so often leads to breakthroughs in our community. Our organizing committee has worked hard over the past year to ensure that our plenary sessions examine some of the most critical issues facing aerospace today, especially the role that disruption plays in our community for better or worse. -
Government of India Office of Director General of Civil Aviation
GOVERNMENT OF INDIA OFFICE OF DIRECTOR GENERAL OF CIVIL AVIATION TECHNICAL CENTRE, OPPOSITE SAFDARJUNG AIRPORT, NEW DELHI CIVIL AVIATION REQUIREMENTS DRAFT SECTION 2 – AIRWORTHINESS SERIES 'O', PART VI F No.11-690/CAR/O-VI/2006/AI (2) ISSUE II DATED __________APRIL 2016 EFFECTIVE: FORTHWITH Subject Manufacture, Registration and Operation of Powered Hang Gliders 1 INTRODUCTION This part of the Civil Airworthiness Requirements specifies requirements relating to, manufacture, registration, maintenance operation and security of powered hang gliders. 1.1 For the purpose of this CAR, a powered hang glider is a vehicle that is used or intended to be used for manual operation in the air by a single occupant/ double 1.1.1 occupant. is used or intended to be used for recreation, sport, or any other purpose approved by 1.1.2 DGCA in writing. 1.1.3 has the maximum AUW less than 275 kgs for a single seater. 1.1.4 has the maximum AUW less than 375 kgs for a double seater. 1.1.5 is not capable of more than 70 knots calibrated air speed at full power in level flight, and 1.1.6 has a power-off stall speed which does not exceed 30 knots calibrated air speed. 2 DEFINITION 2.1 "Acrobatic flight" means manoeuvres intentionally performed by an aircraft involving an abrupt change in its attitude, an abnormal attitude or abnormal variation in speed. 2.2 "Air Traffic Control Clearance" means authorisation by an Air Traffic Control unit for an aircraft to proceed within controlled airspace under specified conditions. 2.3 "Controlled Airport” means an airport at which an Air Traffic Control unit is provided. -
Air-Britain (Trading) Ltd Unit 1A, Munday Works 58-66 Morley Road Tonbridge TN9 1RA +44 (0)1732 363815 [email protected]
SUMMER 2018 SALES DEPARTMENT Air-Britain (Trading) Ltd Unit 1A, Munday Works 58-66 Morley Road Tonbridge TN9 1RA www.air-britain.co.uk +44 (0)1732 363815 [email protected] NEW BOOKS PAGES 2 & 3 This booklist shows the latest books & CDs available from Air-Britain. Full details of additional Air-Britain books and more detailed descriptions are shown online AUSTER – the Company and the Aircraft Tom Wenham, Rod Simpson & Malcolm Fillmore NEW Auster Aircraft has a long and distinguished history, starting with its formation as British Taylorcraft in 1938 and end - ing with its absorption into Beagle Aircraft in 1960.The Auster was not, strictly, a new design since it had its origins in the American Taylorcraft two seater. However, World War II gave it a welcome momentum which led to more than 1,600 artillery spotter Austers being built for the British and other air forces. The Rearsby factory was at maximum production during the war - but, as with all other aircraft manufacturing plants, it found a sudden collapse in military orders when peace came. However, there were returning flyers keen to keep their skills alive and the Autocrat and its successors were successful, not only in the UK but also across the world. Using the same basic airframe, the Auster constantly changed its shape and the 180hp Husky of 1960 was a very different animal from the original 55hp Taylorcraft Model C. Austers were sold all over the world and were used for many tasks including crop spraying, aerial advertising and joyriding. The company also developed new models including the very successful AOP.9, and the less successful Agricola, Atlantic and Avis. -
HELICOPTERS (Air-Cushion Vehicles B60V)
CPC - B64C - 2020.02 B64C AEROPLANES; HELICOPTERS (air-cushion vehicles B60V) Special rules of classification The use of the available Indexing Codes under B64C 1/00- B64C 2230/00 is mandatory for classifying additional information. B64C 1/00 Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like (aerodynamical features common to fuselages, wings, stabilising surfaces, and the like B64C 23/00; flight-deck installations B64D) Definition statement This place covers: • Overall fuselage shapes and concepts (only documents relating thereto are attributed the symbol B64C 1/00, when the emphasis is on aerodynamic aspects the symbol B64C 1/0009 is attributed). • Structural features (including frames, stringers, longerons, bulkheads, skin panels and interior liners). • Windows and doors (including hatch covers, access panels, drain masts, canopies and windscreens). • Fuselage structures adapted for mounting power plants, floors, integral loading means (such as steps). • Attachment of wing or tail units or stabilising surfaces to the fuselage; • Relatively movable fuselage parts (for improving pilot's view or for reducing size for storage). • Severable/jettisonable parts for facilitating emergency escape. • Inflatable fuselage components. • Fuselage adaptations for receiving aerials or radomes. • Passive cooling of fuselage structures and sound/heat insulation (including isolation mats, and clips for mounting such mats and components such as pipes or cables). References Limiting references This place does not cover: Structural features and concepts are attributed the relevant symbol(s) in B64C 1/06 - B64C 1/12 Aerodynamical features common to fuselages, wings, stabilising B64C 23/00 surfaces, and the like Flight-deck installations B64D Special rules of classification Structures and components for helicopters falling within this main group and/or appended subgroups are additionally attributed the symbol B64C 27/04. -
FAA Regulations of Ultralight Vehicles Sudie Thompson
Journal of Air Law and Commerce Volume 49 | Issue 3 Article 4 1984 FAA Regulations of Ultralight Vehicles Sudie Thompson Follow this and additional works at: https://scholar.smu.edu/jalc Recommended Citation Sudie Thompson, FAA Regulations of Ultralight Vehicles, 49 J. Air L. & Com. 591 (1984) https://scholar.smu.edu/jalc/vol49/iss3/4 This Comment is brought to you for free and open access by the Law Journals at SMU Scholar. It has been accepted for inclusion in Journal of Air Law and Commerce by an authorized administrator of SMU Scholar. For more information, please visit http://digitalrepository.smu.edu. Comments FAA REGULATION OF ULTRALIGHT VEHICLES SUDIE THOMPSON A RELATIVELY NEW form of sport and recreational avi- ation has swept the aviation industry - ultralights. Ul- tralights are the first airplanes to have been developed and marketed as "air recreational vehicle[s]." ' Powered ul- tralights are featherweight planes which cost between $2,800 and $7,000.2 Unpowered ultralights are most frequently called hang gliders.' It is estimated that the worldwide total of powered and unpowered ultralights of all types is 25,000,' and one source predicts that the world total of 20,000, pow- ered ultralights will soon double.5 An October, 1981, article places the Federal Aviation Administration's (FAA) estimate of the number of powered ultralights flying in the United States alone at about 2,500.6 Less than one year later the Experimental Aircraft Association (EAA) and the FAA in- creased their estimates of the number of operational powered and unpowered ultralights (excluding true hang gliders) to 7 10,000. -
An Introduction and Brief History
KITES An Introduction and Brief History SKY WIND WORLD.ORG FLYING A ROKAKKU - FLYING BUFFALO PROJECT HISTORY From China kites spread to neighboring countries and across the seas to the Pacific region. At the same time they spread across Burma, India and arriving in North Africa about 1500 years ago. They did not arrive in Europe or America until much later probably via the trade routes Kites are thought to have originated in China about 3000 years ago. One story is that a fisherman was out on a windy day and his hat blew away and got caught on his fishing line which was then when these areas developed. blown up in to the air. Bamboo was a ready source of straight sticks for spars and silk fabric was available to make a light covering, then in the 2nd century AD paper was invented and is still used to this day. PHYSICS Kites fly when thrust, lift, drag and gravity are balanced. The flying line and bridle hold the kite at an angle to the wind so that the air flows faster across the top than the bottom producing the lift. THE PARTS OF A KITE 1 THE SAIL • This can be made of any material such as paper, fabric or plastic. • It is used to trap the air. The air must have somewhere to escape otherwise it spills over the front edge and makes the kite wobble. This can be done by using porous fabric or making it bend backwards to allow the air to slip smoothly over the side. -
Evaluation of V-22 Tiltrotor Handling Qualities in the Instrument Meteorological Environment
University of Tennessee, Knoxville TRACE: Tennessee Research and Creative Exchange Masters Theses Graduate School 5-2006 Evaluation of V-22 Tiltrotor Handling Qualities in the Instrument Meteorological Environment Scott Bennett Trail University of Tennessee - Knoxville Follow this and additional works at: https://trace.tennessee.edu/utk_gradthes Part of the Aerospace Engineering Commons Recommended Citation Trail, Scott Bennett, "Evaluation of V-22 Tiltrotor Handling Qualities in the Instrument Meteorological Environment. " Master's Thesis, University of Tennessee, 2006. https://trace.tennessee.edu/utk_gradthes/1816 This Thesis is brought to you for free and open access by the Graduate School at TRACE: Tennessee Research and Creative Exchange. It has been accepted for inclusion in Masters Theses by an authorized administrator of TRACE: Tennessee Research and Creative Exchange. For more information, please contact [email protected]. To the Graduate Council: I am submitting herewith a thesis written by Scott Bennett Trail entitled "Evaluation of V-22 Tiltrotor Handling Qualities in the Instrument Meteorological Environment." I have examined the final electronic copy of this thesis for form and content and recommend that it be accepted in partial fulfillment of the equirr ements for the degree of Master of Science, with a major in Aviation Systems. Robert B. Richards, Major Professor We have read this thesis and recommend its acceptance: Rodney Allison, Frank Collins Accepted for the Council: Carolyn R. Hodges Vice Provost and Dean of the Graduate School (Original signatures are on file with official studentecor r ds.) To the Graduate Council: I am submitting herewith a thesis written by Scott Bennett Trail entitled “Evaluation of V-22 Tiltrotor Handling Qualities in the Instrument Meteorological Environment”. -
Future of Vertical Flight
www.vtol.org Kenneth Swartz, Regional Director – Americas The Vertical Flight Society www.vtol.org | [email protected] Kitty Hawk Cora © Vertical Flight Society: CC-BY-SA 4.0 © Vertical Flight Society: CC-BY-SA 4.0 Released March 2018 1 www.vtol.org . Founded as “The American Helicopter Society, Inc.” 75 years ago in Connecticut on Feb. 25, 1943 – “For the purpose of collecting, compiling and disseminating information concerning the helicopter” – Sikorsky Aircraft received its order for the first American helicopters on January 5, 1943 (28 XR-4 helicopters) . The first and longest-serving helicopter non-profit Sikorsky XR-4 helicopter – Founding members Igor Sikorsky, Arthur Young, Frank Piasecki, Courtesy of Sikorsky Aircraft Corp. Stanley Hiller, Reggie Brie, A.A. Griffiths, etc. – Included engineers, pilots, operators and presidents from industry, academia and government in Allied countries . Now 6,000 individual and 95 corporate members . Advancing vertical flight worldwide First Annual AHS Awards Banquet Born with the American Helicopter Industry Oct. 7, 1944 © Vertical Flight Society: CC-BY-SA 4.0 2 www.vtol.org © Vertical Flight Society: CC-BY-SA 4.0 3 www.vtol.org . The international professional society for those working to advance vertical flight – Founded in 1943 as the American Helicopter Society – Everything from VTOL MAVs/UAS to helicopters and eVTOL to STOVL (everything vertical except rockets) CFD of Joby S4, Aug 2015 . Expands knowledge about vertical flight technology and promotes its application around the world . Advances safety and acceptability . Advocates for vertical flight R&D funding . Helps educate and support today’s and tomorrow’s vertical flight engineers and leaders VFF Scholarship Winners at AHS Forum 71, May 2015 © Vertical Flight Society: CC-BY-SA 4.0 4 www.vtol.org .