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United States Patent (19) 11 Patent Number: 5,836,541 Pham (45) Date of Patent: Nov
USOO5836541A United States Patent (19) 11 Patent Number: 5,836,541 Pham (45) Date of Patent: Nov. 17, 1998 54) EASILY-CONVERTIBLE FIXED-WING 3,986,686 10/1976 Girard ..................................... 244f7 A ROADABLE AIRCRAFT 4,269,374 5/1981 Miller .......................................... 244/2 4,720,061 1/1988 Abdenour et al. ... 244/46 76 Inventor: Roger N. C. Pham, 625 Veranda Ct., 4.881,701 11/1989 Bullard - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 244/2 #1140, Grand Prairie, Tex. 75050 5,050,817 9/1991 Miller .......................................... 244/2 21 Appl.ppl. No.: 859,7329 Primary Examiner-Galen L. Barefoot 57 ABSTRACT 22 Filed: May 21, 1997 57 A fixed-wing four-seat light aircraft that can be easily Related U.S. Application Data converted to a roadway vehicle within minutes by a single perSon in the field, comprising a one-piece wing center panel 63 Continuation-in-part of Ser. No. 811,503, Mar. 5, 1997. with foldable wing tips on each sides. The whole wing unit (51) Int. Cl. ............................................... B64C37.00 is then rotatably mounted on top of the fuselage. The aircraft 52 U.S. CI 24412; 244/46; 244/49 features a conventional front-engine-and-propeller lay-out, 58 Fi la fs - - - - - - - - h - - - - - - - - - - - - - - - - - - - - - - - s 2442. 46.49 with a short fuselage for convenient roadability and 58) Field of Searc 244/135R, 1 R, 100 R. 1 02 R 50 garageability, with horizontal Stabilizer of Significant Span s s s s with foldable tips for adequate flight stability. The vehicle 56) References Cited has a low ride-height with a low center of gravity, four wheels with independent Suspension, nose-height leveling U.S. -
Eclipse and Kestrel Are One!
INTERNATIONAL FLYING THE DIY TRAVEL PREP MAGENTA LINE Border crossings made easier Will you fall victim? EJOPA EDITION PAGE 14 THE PRIVATE JET MAGAZINE • SUMMER 2015 ECLIPSE AND KESTREL ARE ONE! AUTOMATED FORECASTS Why computer WX prediction is worrisome READY FOR A FLYING CAR? Lots of manufacturers race from freeways to airways PAGE 54 FAA Type Ratings & Recurrent Flight Training Sales • Training • Delivery Your Turbine Transition Specialists jetAVIVA is an authority on owner/operator flown turbine aircraft, oering acquisition and sales services backed with the experience of completing hundreds of transactions. Furthermore, we provide acceptance, delivery, and training services in all production light turbine aircraft. jetAVIVA is focused Featured in AOPA PILOT Magazine on providing Clients with comprehensive services to choose the right aircraft and operate it with maximum eciency and safety. Customized Flight Training Programs on Your Time at Your Location FAA Type Rating Practical Tests & Recurrent Training Per FAR 61.58 CE-500 • CE-510 • CE-525 • CE-560 XL • CE-650 • LR-JET • RA-390 • DA-50 John Azma is an FAA Designated Pilot Examiner qualified to provide Recurrent Training & Type Rating Practical Tests that may be added to your private, commercial and airline transport pilot certificate. Azma FLT Inc. is based in Orlando Florida at KORL. Our experienced & professional flight instructors are also available to provide training at your location. Highly regarded in the industry, and approved by insurance companies, Azma Contact Us To Learn More: FLT Inc. has been featured in aviation specific publications and editorials. Our 844-296-2358 commitment to excellence and superior services begins when you first contact Learn what jetAVIVA can do for you at www.jetAVIVA.com [email protected] us and continues beyond the completion of your training. -
Preparation of Papers for AIAA Technical Conferences
15th AIAA Aviation Technology, Integration, and Operations Conference 2015 Held at the AIAA Aviation Forum 2015 Dallas, Texas, USA 22-26 June 2015 Volume 1 of 3 ISBN: 978-1-5108-0818-8 Printed from e-media with permission by: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 Some format issues inherent in the e-media version may also appear in this print version. The contents of this work are copyrighted and additional reproduction in whole or in part are expressly prohibited without the prior written permission of the Publisher or copyright holder. The resale of the entire proceeding as received from CURRAN is permitted. For reprint permission, please contact AIAA’s Business Manager, Technical Papers. Contact by phone at 703-264-7500; fax at 703-264-7551 or by mail at 1801 Alexander Bell Drive, Reston, VA 20191, USA. TABLE OF CONTENTS VOLUME 1 TERMINAL & SURFACE OPERATIONS I A Robust and Practical Decision Support Tool for Integrated Arrival-Departure-Surface Traffic Management (AIAA 2015-2270)...............................................................................................................................................................................................1 Aditya Saraf, Valentino Felipe, Bruce Sawhill Identification of Local and Propagated Queuing Effects at Major Airports (AIAA 2015-2271)............................................................16 Husni R. Idris Taxi Time Prediction at Charlotte Airport Using Fast-Time Simulation and Machine Learning Techniques (AIAA 2015-2272)..........................................................................................................................................................................................................32 -
3.0 the Autonomous Transportation System (ATS)
3.0 The Autonomous Transportation System (ATS) Concept The world is on the cusp of a completely new mode of transportation using electric powered, networked, fully autonomous vehicles. A new Autonomous Transportation System (ATS) is needed to facilitate this transformation within the U.S., to include standards for the development, manufacture and operation of autonomous Aerial Vehicles (AVs) and Ground Vehicles (GVs). This document proposes strategic-level standards for the ATS and for autonomous AVs and GVs, to enable safe, secure, reliable and swift transport of cargo and human passengers. Further, it proposes standards to safely incorporate traditional manually operated ground vehicles, pilot-controlled aircraft, and smalls drones into the system – initially and perpetually. Topics, features, and design solutions presented in this document are the proposed strategic- level standards. The proposed new ATS includes the people, facilities, and hardware/software (HW/SW) required to manage, operate, and monitor all GVs operating on the ground, and all AVs operating within the authorized public airspace. The standards will ensure cargo, passengers, and people and property on the ground are kept safe, now and into the future. OVER’s vision and intention is that this proposed ATS be discussed and revised as necessary by transportation and aerospace industry experts, government experts (DOT, FAA, etc.), and the American public. Once revised, it can provide a baseline for final standards to govern the design, production, integration and operation of large, fully autonomous GVs traversing public roads and AVs flying within the public airspace. The final ATS will ensure that all autonomous GVs/AVs are safe, secure, reliable and fully compatible with the HW, SW, networking and communication requirements, regardless of manufacturer, or will not be allowed to operate. -
FLYING CARS / ROADABLE AIRPLANES AUGUST 2012 Please Send Updates and Comments to Tom Teel: [email protected] Terrafugia
FLYING CARS / ROADABLE AIRPLANES AUGUST 2012 Please send updates and comments to Tom Teel: [email protected] Terrafugia INTERNATIONAL FLYING CAR ASSOCIATION http://www.flyingcarassociation.com We'd like to welcome you to the International Flying Car Association. Our goal is to help advance the emerging flying car industry by creating a central resource for information and communication between those involved in the industry, news networks, governments, and those seeking further information worldwide. The flying car industry is in its formative stages, and so is IFCA. Until this site is fully completed, we'd like to recommend you visit one of these IFCA Accredited Sites. www.flyingcars.com www.flyingcarreviews.com www.flyingcarnews.com www.flyingcarforums.com REFERENCE INFORMATION Roadable Times http://www.roadabletimes.com Transformer - Coming to a Theater Near You? http://www.aviationweek.com/Blogs.aspx?plckBlo PARAJET AUTOMOTIVE - SKYCAR gId=Blog:a68cb417-3364-4fbf-a9dd- http://www.parajetautomotive.com/ 4feda680ec9c&plckController=Blog&plckBlogPage= In January 2009 the Parajet Skycar expedition BlogViewPost&newspaperUserId=a68cb417-3364- team, led by former British army officer Neil 4fbf-a9dd- Laughton and Skycar inventor Gilo Cardozo 4feda680ec9c&plckPostId=Blog%253aa68cb417- successfully completed its inaugural flight, an 3364-4fbf-a9dd- incredible journey from the picturesque 4feda680ec9cPost%253a6b784c89-7017-46e5- surroundings of London to Tombouctou. 80f9- Supported by an experienced team of overland 41a312539180&plckScript=blogScript&plckElement -
Some NASA Perspectives on H2 Presented by Steven Schneider NASA Glenn Research Center
National Aeronautics and Space Administration Some NASA Perspectives on H2 Presented by Steven Schneider NASA Glenn Research Center H2@Airports Workshop November 4, 2020 1 www.nasa.gov NASA Subsonic Transport Strategy Focus on 4 Key Technologies Electrified Aircraft Propulsion Small Core Gas Turbine Up to 5% fuel burn and maintenance benefit 5%-10% fuel burn benefit Transonic Truss-Braced Wing 7%-10% fuel burn benefit High Rate Composite Manufacturing 4x-6x manufacturing rate increase Ensure U.S. industry is the first to establish the new “S Curve” for the next 50 years of transports NASA Perspectives on H2 • H2 offers opportunity as a clean energy carrier • NASA has explored H2 applications for air transportation in past decades, which helped to highlight benefits and challenges • Noted recent increase in interest associated with H2-powered concepts and research in the air transportation community • NASA’s current research portfolio includes some investigation of H2 energy storage and hydrocarbon conversion for fuel cells on electric aircraft, though no current emphasis on other H2-related challenges • Need to consider off-aircraft challenges: the cost/ energy/ environmental impact of H2 production; the cost of developing H2 infrastructure; characterization of contrails and their atmospheric impacts Since NASA’s H2 interest has related to vehicle-level technology development and integration, we are happy to see workshops focused on solving the challenges of H2 airport infrastructure Examples of Renewed Interest in H2 ZeroAvia Commercial -
(12) United States Patent (10) Patent No.: US 9,555,681 B2 Klein (45) Date of Patent: Jan
USO09555681 B2 (12) United States Patent (10) Patent No.: US 9,555,681 B2 Klein (45) Date of Patent: Jan. 31, 2017 (54) TRANSFORMATION METHOD OF HYBRD B64C 3/54: B64C 3/56; B64C TRANSPORTATION VEHICLE FOR 25/04; B64C 25/54: B64C 37/00; B64C GROUND AND AIR, AND HYBRID 2025/003; B64C 3/58; Y02T 50/145 TRANSPORTATION VEHICLE ITSELF (Continued) (75) Inventor: Stefan Klein, Nitra (SK) (56) References Cited (73) Assignee: AEROMOBIL, S.R.O., Bratislava (SK) U.S. PATENT DOCUMENTS 1,793,494 A 2f1931 Lee (*) Notice: Subject to any disclaimer, the term of this 3,029,042 A * 4, 1962 Martin ...................... B6OF 3.00 patent is extended or adjusted under 35 180,119 U.S.C. 154(b) by 142 days. (Continued) (21) Appl. No.: 14/241,239 FOREIGN PATENT DOCUMENTS (22) PCT Filed: Aug. 22, 2012 CH 295.572 A 12/1953 DE 10346189 B3 5, 2005 (86). PCT No.: PCT/SK2O12/OOOO10 (Continued) S 371 (c)(1), (2), (4) Date: Aug. 19, 2014 OTHER PUBLICATIONS PCT International Search Report, Issued in International Applica (87) PCT Pub. No.: WO2013/032409 tion No. PCT/SK2012/000010 dated Dec. 12, 2012. PCT Pub. Date: Mar. 7, 2013 (Continued) (65) Prior Publication Data Primary Examiner — Timothy D Collins US 2015/OO2815O A1 Jan. 29, 2015 Assistant Examiner — Jessica Wong (74) Attorney, Agent, or Firm — Finnegan, Henderson, (30) Foreign Application Priority Data Farabow, Garrett & Dunner LLP. Aug. 30, 2011 (SK) ................................... 5O39-2011 (57) ABSTRACT Aug. 30, 2011 (SK) ............................... 5044-2011 U Transformation method of hybrid transportation vehicle for ground and air includes the following transformation and (51) Int. -
Il Modello Predittivo Degli Eventi Futuri Del CRNE - Centro Ricerche Nuove Energie
Il Modello Predittivo degli Eventi Futuri del CRNE - Centro Ricerche Nuove Energie: Analisi GeoPolitiche, Tecnologiche & Smart City Solution - Advice Service CRNE Science & Business Vision Il CRNE Centro Ricerche Nuove Energie nasce nel 1998, e nel 2015 la “Divisione Ricerca e Sviluppo” ha sviluppato “un modello predittivo degli eventi futuri basato sul censimento delle minacce ponderate”. Si tratta di “un servizio di consulenza sulle aspettative future” unico nel suo genere sul panorama nazionale e internazionale, in cui viene esposto in maniera chiara una visuale precisa degli eventi futuri, che noi riteniamo altamente probabili, sia sul breve, che nel medio, che nel lungo periodo. Il Modello Predittivo degli eventi futuri del CRNE è uno strumento prezioso per quanti vogliono avere una visione moderna e all’avanguardia dell’evoluzione degli eventi, per proteggersi nell’immediato futuro dalle minacce ponderate che abbiamo censito, che sono esposte in forma cronologica nel modello predittivo. Sta alla sensibilità del lettore tenere in considerazione per il proprio futuro quanto riportato in questa relazione. CRNE Science & Business Vision is an Advice Service to Avoid Future’s Systemic Crisis These Are Our Areas of Expertise: Geopolitical Analysis and Solutions - Investment in Work & Residential CRNE Concept Outside Italy, called “Smart City Project”, named “Backup Italy” Advice Service for Human Resources & Capital Money Protection - Scientific and Technological Research - Development Service for Start Up, Patent and Prototype for CRNE’s Smart City - International Financial Analysis & Development Performance’s Strategy for Stock Market CRNE leads the way to the future to the best Italians, Serenity is our goal, Choose to live under CRNE wings&vision. -
AMT Model Kits
AMT Model Kits CARS — 1/16 SCALE CARS — 1/25 SCALE (Cont) CARS — 1/25 SCALE (Cont) 872 1965 Ford Mustang $39.99 841 2013 Chevy Camaro ZL1 898 1969 Mercury Cougar $22.99 Showroom Replica $21.99 1005 ‘55 Chevy Nomad Wagon 38.99 899 1937 Chevy Coupe 24.99 849 ‘68 Plymouth Roadrunner-yellow 23.99 900 Piranha Spy Car 23.99 850 ‘40 Ford Coupe—orange 22.99 , 854 Baldwin Motion 872 ‘70 1/2 Chevy Camaro—white 21.99 855 Baldwin Motion 900 ‘70 1/2 Chevy Camaro—dk green 21.99 860 Nestle 1923 Ford Model T Delivery 23.99 CARS — 1/20 SCALE 861 ‘63 Chevy Corvette 22.99 1030 ‘94 Chevy Camaro Conv. 26.99 902 1932 Ford Victoria 25.99 862 ‘51 Chevy Bel Air 21.99 CARS — 1/25 SCALE 904 1966 Ford Galaxie 23.99 634 ‘68 Shelby GT500 15.99 906 1941 Ford Woody 24.99 635 ‘70 1/2 Camaro Z28 15.99 907 Tee Vee Dune Buggy 23.99 636 ‘66 Chevy Nova Pro Street 15.99 638 ‘57 Bel Air 15.99 862 671 2010 Dodge Challenger R/T 907 Classic 19.99 704 ‘66 Ford Mustang 21.99 729 Buick Opel GT- white 864 ‘97 Ford Mustang GT 21.99 Original Art Series 24.99 865 ‘62 Chevy Bel Air SS 409 908 Li’l Hot Dogger Show Rod 26.99 730 ‘40 Ford Coupe –white Joe Gardner Racing 22.99 Original Art Series 22.99 868 ‘68 Chevy Camaro Z/28 21.99 750 Ghostbusters Ecto-1A 22.99 871 Jack Reacher 768 ‘75 Gremlin 21.99 ‘70 Chevy Chevelle SS 23.99 908 873 Chevy CheZoom Corvair F/C 24.99 876 1967 Chevy Chevelle Pro Street 21.99 768 909 USA-1 1963 Chevy Corvette 22.99 910 1953 Chevy Corvette 23.99 912 ‘69 Mercury Cougar—orange 22.99 876 916 Piranha Spy Car Original Art Series 26.99 769 Gene Winfield ‘40 Ford Sedan 917 1964 Chevy Impala 22.99 Delivery 22.99 919 1941 Plymouth Coupe 21.99 772 ‘66 Chevy Nova-Bill Jenkins 24.99 920 1971 Ford Thunderbird 25.99 791 The Three Stooges ‘40 Ford Sedan 877 1953 Studebaker Starliner Delivery 22.99 “Mr. -
The the Roadable Aircraft Story
www.PDHcenter.com www.PDHonline.org Table of Contents What Next, Slide/s Part Description Flying Cars? 1N/ATitle 2 N/A Table of Contents 3~53 1 The Holy Grail 54~101 2 Learning to Fly The 102~155 3 The Challenge 156~194 4 Two Types Roadable 195~317 5 One Way or Another 318~427 6 Between the Wars Aircraft 428~456 7 The War Years 457~572 8 Post-War Story 573~636 9 Back to the Future 1 637~750 10 Next Generation 2 Part 1 Exceeding the Grasp The Holy Grail 3 4 “Ah, but a man’s reach should exceed his grasp, or what’s a heaven f?for? Robert Browning, Poet Above: caption: “The Cars of Tomorrow - 1958 Pontiac” Left: a “Flying Auto,” as featured on the 5 cover of Mechanics and Handi- 6 craft magazine, January 1937 © J.M. Syken 1 www.PDHcenter.com www.PDHonline.org Above: for decades, people have dreamed of flying cars. This con- ceptual design appeared in a ca. 1950s issue of Popular Mechanics The Future That Never Was magazine Left: cover of the Dec. 1947 issue of the French magazine Sciences et Techniques Pour Tous featur- ing GM’s “RocAtomic” Hovercar: “Powered by atomic energy, this vehicle has no wheels and floats a few centimeters above the road.” Designers of flying cars borrowed freely from this image; from 7 the giant nacelles and tail 8 fins to the bubble canopy. Tekhnika Molodezhi (“Tech- nology for the Youth”) is a Russian monthly science ma- gazine that’s been published since 1933. -
From Flying Rockets to Tesla: Examining the Sustainable Mobility Preferences of Primary School Children in Denmark and the Netherlands
From flying rockets to Tesla: examining the sustainable mobility preferences of primary school children in Denmark and the Netherlands Article (Accepted Version) Kester, Johannes, Sovacool, Benjamin K and Heida, Vimke (2019) From flying rockets to Tesla: examining the sustainable mobility preferences of primary school children in Denmark and the Netherlands. Energy Research and Social Science, 56 (101204). pp. 1-11. ISSN 2214-6296 This version is available from Sussex Research Online: http://sro.sussex.ac.uk/id/eprint/84145/ This document is made available in accordance with publisher policies and may differ from the published version or from the version of record. If you wish to cite this item you are advised to consult the publisher’s version. Please see the URL above for details on accessing the published version. Copyright and reuse: Sussex Research Online is a digital repository of the research output of the University. Copyright and all moral rights to the version of the paper presented here belong to the individual author(s) and/or other copyright owners. To the extent reasonable and practicable, the material made available in SRO has been checked for eligibility before being made available. Copies of full text items generally can be reproduced, displayed or performed and given to third parties in any format or medium for personal research or study, educational, or not-for-profit purposes without prior permission or charge, provided that the authors, title and full bibliographic details are credited, a hyperlink and/or URL is given for the original metadata page and the content is not changed in any way. -
Wing Flap System for Flying Car
(19) TZZ¥___T (11) EP 3 418 184 A1 (12) EUROPEAN PATENT APPLICATION (43) Date of publication: (51) Int Cl.: 26.12.2018 Bulletin 2018/52 B64C 9/16 (2006.01) B60F 5/02 (2006.01) (21) Application number: 17176991.2 (22) Date of filing: 20.06.2017 (84) Designated Contracting States: (72) Inventors: AL AT BE BG CH CY CZ DE DK EE ES FI FR GB • MACANDREW, Kenneth Douglas Alexander GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO 841 06 Bratislava-Zahorska Bystrica (SK) PL PT RO RS SE SI SK SM TR • URIK, Tomas Designated Extension States: 908 41 Sastin-Straze (SK) BA ME • ROOMS, William Simon Designated Validation States: 841 02 Bratislava (SK) MA MD (74) Representative: Finnegan Europe LLP (71) Applicant: AeroMobil R&D, s. r. o. 1 London Bridge 82106 Bratislava-mestska cast Podunajske London SE1 9BG (GB) Biskupice (SK) (54) WING FLAP SYSTEM FOR FLYING CAR (57) A wing and flap system for an aircraft compris- mechanism for moving the flap between the first, second, ing: a wing (16); and a deployable flap (30) connected to and intermediate positions, comprising: a driven toothed the wing, the flap being moveable between a first position pinion (52) mounted in the wing; and first (36) and second in which a trailing edge portion of the wing substantially (38) struts, each substantially aligned with a plane includ- overlaps the flap and the angle of incidence of the flap ing a chord of the wing and extending between the pinion is substantially the same as the angle of incidence of the and the flap, each strut having a toothed rack (40, 42) wing, and a