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Metodi E Modelli Di Pianificazione E Progettazione Eliportuale Per Servizi Di Trasporto Civile
Metodi e modelli di pianificazione e progettazione eliportuale per servizi di trasporto civile Luigi Maritano Corso di Dottorato in Tecnica ed Economia dei Trasporti XXIV Ciclo Tutor: Prof. Ing. Salvatore Amoroso Coordinatore: Prof. Ing. Marco Migliore UNIVERSITÀ DEGLI STUDI DI PALERMO FACOLTA’ DI INGEGNERIA Dipartimento di Ingegneria Civile, Ambientale, Aerospaziale, dei Materiali (D.I.C.A.M.) In copertina: Artist Rendering of the Air Pegasus Metro Heliplex heliport http://ironboundnewark.com/we-fly-high-newark-heliportheliplex UNIVERSITÀ DEGLI STUDI DI PALERMO FACOLTÀ DI INGEGNERIA Dipartimento di Ingegneria Civile, Ambientale, Aerospaziale, dei Materiali Corso di Dottorato di Ricerca in Tecnica ed Economia dei Trasporti – XXIV Ciclo S.S.D. ICAR/05 Metodi e modelli di pianificazione e progettazione eliportuale per servizi di trasporto civile Tesi di dottorato di: Tutor: Luigi Maritano Prof. Ing. Salvatore Amoroso Coordinatore del Corso: Prof. Ing. Marco Migliore INDICE GENERALE INDICE GENERALE ................................................................................................. pagina I INDICE DELLE FIGURE E DELLE TABELLE ................................................................ V INTRODUZIONE ................................................................................................................. 1 CAPITOLO 1 - L’impiego civile dell’elicottero: considerazioni di carattere generale e analisi del contesto nazionale ed internazionale Premessa ........................................................................................................................... -
Decision 2005/07/R
DECISION No 2005/07/R OF THE EXECUTIVE DIRECTOR OF THE AGENCY of 19-12-2005 amending Decision No 2003/19/RM of 28 November 2003 on acceptable means of compliance and guidance material to Commission Regulation (EC) No 2042/2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to Regulation (EC) No 1592/2002 of 15 July 2002 on common rules in the field of civil aviation (hereinafter referred to as the Basic Regulation) and establishing a European Aviation Safety Agency1 (hereinafter referred to as the “Agency”), and in particular Articles 13 and 14 thereof. Having regard to the Commission Regulation (EC) No 2042/2003 of 28 November 2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks.2 Whereas: (1) Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence (hereinafter referred to as Part-66 AMC Appendix I) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered as a permanent rulemaking task for the Agency. This decision represents the first update according to an accelerated procedure accepted by AGNA and SSCC. -
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). -
Iran and the Gulf Military Balance - I
IRAN AND THE GULF MILITARY BALANCE - I The Conventional and Asymmetric Dimensions FIFTH WORKING DRAFT By Anthony H. Cordesman and Alexander Wilner Revised July 11, 2012 Anthony H. Cordesman Arleigh A. Burke Chair in Strategy [email protected] Cordesman/Wilner: Iran & The Gulf Military Balance, Rev 5 7/11/12 2 Acknowledgements This analysis was made possible by a grant from the Smith Richardson Foundation. It draws on the work of Dr. Abdullah Toukan and a series of reports on Iran by Adam Seitz, a Senior Research Associate and Instructor, Middle East Studies, Marine Corps University. 2 Cordesman/Wilner: Iran & The Gulf Military Balance, Rev 5 7/11/12 3 INTRODUCTION ............................................................................................................................................. 5 THE HISTORICAL BACKGROUND ....................................................................................................................... 6 Figure III.1: Summary Chronology of US-Iranian Military Competition: 2000-2011 ............................... 8 CURRENT PATTERNS IN THE STRUCTURE OF US AND IRANIAN MILITARY COMPETITION ........................................... 13 DIFFERING NATIONAL PERSPECTIVES .............................................................................................................. 17 US Perceptions .................................................................................................................................... 17 Iranian Perceptions............................................................................................................................ -
Helicopters 2015 Flightglobal’S Helicopter Data
DATA INSIGHT HELICOPTERS 2015 FLIGHTGLOBAL’S HELICOPTER DATA This report features helicopter data capabilities with information extracted from Flightglobal’s Fleets Analyzer database. The report is divided in two sections: civil (page 3 to 7) and military (page 8 to 11). CONTENTS CIVil helicopters 3 Fleet share by region 3 Top 10 countries 4 Top 10 types 5 Q1&Q2 Deliveries 2014 vs 2015 6 Fleet growth & deliveries 7 MilitarY helicopters 8 Fleet share by region 8 Top 10 countries and types 9 Q1&Q2 Deliveries 2014 vs 2015 10 Fleet growth & deliveries 11 2 | Flightglobal CIVIL HELICOPTERS: FLEET SHARE BY REGION EUROPE NORTH AMERICA 27% 35% Turbine: 6,770 MIDDLE EAST Piston: 2,608 Turbine: 8,400 Piston: 3,654 2% ASIA-PACIFIC AFRICA Turbine: 509 Piston: 37 18% LATIN AMERICA 5% Turbine: 3,983 Turbine: 1,173 Piston: 2,102 13% Piston: 635 Turbine: 3,224 Piston: 1,192 WORLD total Turbine: 24,287 Piston: 10,266 Note: In-service fleet information based on operator’s location. An additional 1% of the fleet hasn’t been included in the above figures for helicopters based in unknown locations. SOURCE: Flightglobal’s Fleets Analyzer database (September 2015) 3 | Flightglobal CIVIL HELICOPTERS: TOP 10 COUNTRIES RANK COUNTRY TURBINE SHARE RANK COUNTRY PISTON SHARE 1 USA 6,667 27% 1 USA 3,084 30% 2 RUSSIA 1,881 8% 2 AUSTRALIA 1,084 11% 3 CANADA 1,733 7% 3 BRAZIL 578 6% 4 BRAZIL 1,234 5% 4 CANADA 570 6% 5 AUSTRALIA 778 3% 5 SOUTH AFRICA 566 6% 6 ITALY 674 3% 6 UK 413 4% 7 UK 663 3% 7 NEW ZEALAND 381 4% 8 JAPAN 617 3% 8 RUSSIA 339 3% 9 MEXICO 588 2% 9 FRANCE -
Careflite Orders an Agusta Westland AW109 Power Helicopter
Date: 3/7/08 CareFlite Dallas/Fort Worth Orders An AgustaWestland AW109 Power Helicopter AgustaWestland is pleased to announce that CareFlite Dallas/Fort Worth has ordered another AW109 Power light twin turbine helicopter. This purchase adds to the five AW109 Powers ordered in 2001 and further expands CareFlite’s fleet dedicated to emergency medical service purposes. Speaking on behalf of CareFlite, President and CEO James Swartz stated “This latest contract further confirms the reliance CareFlite, as a leading US air medical operator servicing a major metropolitan area, places upon the exceptional performance, operational economies, support and EMS capabilities of the AW109 Power. AgustaWestland’s AW109 meets and exceeds our load and range requirements while adding superior single engine performance. Its unequalled maximum and cruise speed facilitates an expeditious response to CareFlite’s medical emergencies when seconds are critical.” (Above L to R) Eric Crawford – Agusta Westland Account Executive, James C. Swartz – CareFlite President & CEO, Louis Bartolotta – Agusta Westland’s Executive VP of Sales, Bob Cleland - Agusta Westland’s Director of Sales, photo taken at HAI Convention in Houston, Texas Louis Bartolotta, AgustaWestland’s Executive VP of Sales, stated “This AW109 Power is testimony to both the strong relationship we have had with CareFlite Dallas over the past 7 years and will continue to enjoy into the future, and the high level of critical care services that they will be able to provide the Dallas-Ft. Worth metropolitan area. We remain honoured to assist in the provision of that care.” CareFlite’s AW109 Power is certified for single pilot IFR operations and powered by twin Pratt & Whitney 206C engines. -
Aip Supplement 012/2019 United Kingdom
AIP SUPPLEMENT 012/2019 UNITED KINGDOM Date Of Publication 14 Mar 2019 UK Aeronautical Information Services Notes NATS Swanwick (a) All times are UTC. Room 3115 (b) References are to the UK AIP. Sopwith Way (c) Information, where applicable, Southampton SO31 7AY [email protected] should also be used to amend http://www.ais.org.uk appropriate charts. 07469-441832 (Content - DfT/Aviation Policy Division) 0191-203 2329 (Distribution - Communisis UK) LONDON HEATHROW, LONDON GATWICK AND LONDON STANSTED AIRPORTS NOISE RESTRICTIONS NOTICE 2019 (Published on behalf of the Department for Transport) Whereas: a) By virtue of the Civil Aviation (Designation of Aerodromes) Order 1981(a) Heathrow Airport - London, Gatwick Airport - London and Stansted Airport - London (‘the London Airports’) are designated aerodromes for the purposes of Section 78 of the Civil Aviation Act 1982 (‘the Act’)(b); b) Pursuant to the powers set out in section 78 of the Act, the Secretary of State considers it appropriate, for the purpose of avoiding, limiting or mitigating the effect of noise and vibration connected with the taking-off or landing of aircraft at the London Airports, to prohibit aircraft of specified descriptions from taking off or landing and to limit the number of occasions on which other aircraft may take off or land at those aerodromes during periods specified in this Notice throughout the period specified as the summer season 2019 in this Notice; c) For the purposes of Section 78(4)(a) of the Act, the circumstances under which a particular occasion or series of occasions on which aircraft take off or land at the London Airports will be disregarded for the purposes of this Notice are specified in paragraph 11 of this Notice. -
Air Yorkshire Aviation Society
Air Yorkshire Aviation Society Volume 42 Issue 1 January 2016 HS-VSK Gulfstream 650 Leeds/Bradford 1 November 2015 David Blaker www.airyorkshire.org.uk SOCIETY CONTACTS Air Yorkshire Committee 2016 Chairman David Senior 23 Queens Drive, Carlton, WF3 3RQ 0113 282 1818 [email protected] Secretary Jim Stanfield 8 Westbrook Close, Leeds, LS18 5RQ 0113 258 9968 [email protected] Treasurer David Valentine 8 St Margaret's Avenue, Horsforth, Distribution/Membership Pauline Valentine Leeds, LS18 5RY 0113 228 8143 Managing Editor Alan Sinfield 6 The Stray, Bradford, BD10 8TL Meetings coordinator 01274 619679 [email protected] Photographic Editor David Blaker [email protected] Visits Organiser Mike Storey 0113 252 6913 [email protected] Dinner Organiser John Dale 01943 875315 Publicity Howard Griffin 6 Acre Fold, Addingham, Ilkley LS29 0TH 01943 839126 (M) 07946 506451 [email protected] Plus Reynell Preston (Security), Paul Windsor (Reception/Registration) Geoff Ward & Paula Denby Code of Conduct Members should not commit any act which would bring the Society into disrepute in any way. Disclaimer the views expressed in articles in the magazine are not necessarily those of the editor and the committee. Copyright The photographs and articles in this magazine may not be reproduced in any form without the strict permission of the editor. SOCIETY ANNOUNCMENTS Happy New Year! You may notice a few changes in the magazine for 2016. The first change is that I am now using OpenOffice to produce the magazine which I find easier to use, saving me some time! Secondly I have changed the order of the items within the magazine – the front part of the magazine now includes members articles, a historical look back at items from past magazines, a table of airline updates and a page of photographs from hotels around the world. -
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 ........................................................................................................................ -
Quest Kodiak Aircraft Profile a Irbus A320neo
Nº16 2016 M A G A Z I N E Nº16 VOLANDO EN EL QUEST KODIAK AIRCRAFT PROFILE A IRBUS A320NEO BELL 407GXP MÁS POTENCIA WWW.VORTEXXMAG.COM ENTREVISTA A LUIS VIDAL: LOS AEROPUERTOS 4G DEL FUTURO How can I fly more passengers to the most popular airports at peak times? Fly the A380. The world’s most spacious commercial aircraft. Capture more high-yield traf c on the busiest routes and offer the highest passenger appeal with 18+ inch seats in economy. Airbus is the answer. airbus.com © AIRBUS, 2016. All rights reserved. Airbus, its logo and the product names are registered trademarks. Airbus_VortexX_June.indd Pg1 Prodigious UK 09/05/2016 11:09 VORTEXX MAGAZINE Contacto e Informaciones: [email protected] Publicidad y Marketing: [email protected] Suscripciones: [email protected] EN Los contenidos de esta publicación son de responsabilidad de la editorial y sus entrevistados. De ESTAEDICIÓN no coincidir con la realidad contemporánea, se debe al desfase de publicación del medio. BELL GXP MÁS POTENCIAP.18 PILOTO AUTOMÁTICOP. 26 P. 32 KODIAKA TODA PRUEBA DE AGUSTAWASTELAND A LEONARDO HELICOPTERSP.46 P. 54 ECOS TURBOHÉLICES DE FIDAE P. 40 MONOMOTOR CESSNA ENTREVISTA ROCKWELL DENALIP. 60 A LUIS VIDALP. 62 COLLINSP. 6 6 FABRICANTES DE AERONAVES Y SUS PROYECCIONES P.76 AIRCRAFT PROFILE XTREME AIRBUS 320 NEO P.7 0 XA42P. 8 4 Vortexx Magazine es una marca registrada, división de la editorial Vortexx Publishing, una marca Vortexx Studio. La confección, contenidos, marca y diseño están protegidos por la ley Nº17.336 de propiedad intelectual de la República de Chile que considera propiedad de los productos desarrollados en la región de Latinoamérica gracias a los convenios del Mercosur, por lo que se prohíbe la reproducción parcial o total de su contenido. -
Technical Note – Psa14
Technical Note – PSa14 D. Marchiori Pitot-static Adaptors DMA design and manufacture pitot-static adaptors for a wide range of aircraft types. Also, in addition to single adaptors, comprehensive kits of adaptors for a wide range of aircraft are available and the list is continuously growing. The kits are housed within strong lightweight cases and consist of all the necessary adaptors for the Pitot and Static test points for the particular aircraft. Additionally the DMA kits feature the vacuum hold down fixtures on the Static adaptors and the appropriate vacuum hose is incorporated to allow the DMA air data tester to provide the appropriate source. The all important warning flags are also incorporated as is the matching gasket maintenance kit for in-service support. Adaptors are available for the following aircraft at the present time; DMA-SJ100 Adapter Kit - Sukhoi SJ100 DMAK-A109 Adapter Kit - A109 pitot 369D-022 DMAK-A109N Adapter Kit - AgustaWestland A109 Nexus DMAK-A320 Adapter Kit - Airbus A320 & A310/200/300 DMAK-A330 Adapter Kit - Airbus A330 DMAK-A330 Adapter Kit - Airbus A330 DMAK-A380 Adapter Kit - Airbus A380 DMAK-AB412 Adapter Kit - Agusta AB212 & AB412 DMAK-ALH2 Adapter Kit - ALH2 DMAK-AS350 Adapter Kit - Eurocopter A350 DMAK-ATR42 Adapter Kit - ATR42 & ATR72 DMAK-AW109-1P Adapter Kit - AgustaWestland AW109 DMAK-AW139-1P Adapter Kit - AgustaWestland AW139 DMAK-B737-2345 Adapter Kit - Boeing B737 (20,300,400,500) DMAK-B737-678 Adapter Kit - Boeing B737 (600,700,800,900) DMAK-B747 Adapter Kit - Boeing B747 DMAK-B757 Adapter Kit - Boeing 757 DMAK-B767 Adapter Kit - Boeing 767 DMAK-B777 Adapter Kit - Boeing 777 DMAK-BAE146 Adapter Kit - British Aerospace BAe146 & RJ85 DMAK-C27J Adapter Kit - Alenia C27J DMAK-CESN3 Adapter Kit – CESSNA CESN3 DMAK-CESNT182T Adapter Kit - Cessna T182T. -
Rotor Wing Aircraft Rotor Wing Aircraft. a General
LECTURE 2: ROTOR WING AIRCRAFT. A GENERAL APPROACH Oriol Lizandra i Dalmases Course 2013‐2014 (Anna typography, by courtesy of Anna Vives) TYPICAL DESGIGNS AND CONFIGURATIONS 2 Oriol Lizandra i Dalmases MAIN ELEMENTS OF A HELICOPTER Vertical Stabilizer Blade Tail Rotor (anti‐torque) Rotor Head Tail Boom Horizontal Stabilizer Fuselage and Cabin Skid 3 Oriol Lizandra i Dalmases FORCES ON A HELICOPTER Rotor Lift Thrust Propulsive force Drag Weight 4 Oriol Lizandra i Dalmases AgustaWestland AW109 5 EUROCOPTER AS350BA 6 MAIN ELEMEN TS OF AN AUT OGYRO Right Vertical Left Vertical Stabilizer Horizontal Stabilizer Stabilizer Right Tail Boom Propeller Rotor Head Right Wing Left Tail Boom Fuselage and Cabin Blade Left Wing Forward Gear Left Main Gear 7 Oriol Lizandra i Dalmases FORCES ON AN AUTOGYRO T F L D T : Rotor Thrust W W : Weight L : Wing lift D : Airframe drag F : Propulsive force 8 Oriol Lizandra i Dalmases ELA 07S 9 GBA HAWK 4 10 GENERAL DESCRIPTION OF HELICOPTERS (CONVENTIONAAAL CONFIGURATION) 11 Oriol Lizandra i Dalmases HELICOPTER MAIN SYSTEMS • ENGINE/S: – Reciprocating engines, used in small helicopters (low power, say below 300 H.P.). – Turboshaft (gas turbine engine), with a much higher power‐weihight ratio. • TRANSMISSION SYSTEM: – Main rotor transmission. – Tail rotor transmission. – Clutch. – Free wheel unit. • MAIN (AND TAIL) ROTOR: – Swash plate. – Rotor head. – Blad es. 12 Oriol Lizandra i Dalmases TRANSMISSION SYSTEM MISSION: to transfer the output power from the engine to the main rotor and tiltail rotor, and is subdivided into: • MAIN ROTOR TRANSMISSION SYSTEM. Reduces the turn speed (with respect to that of the engine) to an optimum value for the main rotor.