Air Taxi SOLUTIONS GLENAIR
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Jay Carter, Founder &
CARTER AVIATION TECHNOLOGIES An Aerospace Research & Development Company Jay Carter, Founder & CEO CAFE Electric Aircraft Symposium www.CarterCopters.com July 23rd, 2017 Wichita©2015 CARTER AVIATIONFalls, TECHNOLOGIES,Texas LLC SR/C is a trademark of Carter Aviation Technologies, LLC1 A History of Innovation Built first gyros while still in college with father’s guidance Led to job with Bell Research & Development Steam car built by Jay and his father First car to meet original 1977 emission standards Could make a cold startup & then drive away in less than 30 seconds Founded Carter Wind Energy in 1976 Installed wind turbines from Hawaii to United Kingdom to 300 miles north of the Arctic Circle One of only two U.S. manufacturers to survive the mid ‘80s industry decline ©2015 CARTER AVIATION TECHNOLOGIES, LLC 2 SR/C™ Technology Progression 2013-2014 DARPA TERN Won contract over 5 majors 2009 License Agreement with AAI, Multiple Military Concepts 2011 2017 2nd Gen First Flight Find a Manufacturing Later Demonstrated Partner and Begin 2005 L/D of 12+ Commercial Development 1998 1 st Gen 1st Gen L/D of 7.0 First flight 1994 - 1997 Analysis & Component Testing 22 years, 22 patents + 5 pending 1994 Company 11 key technical challenges overcome founded Proven technology with real flight test ©2015 CARTER AVIATION TECHNOLOGIES, LLC 3 SR/C™ Technology Progression Quiet Jump Takeoff & Flyover at 600 ft agl Video also available on YouTube: https://www.youtube.com/watch?v=_VxOC7xtfRM ©2015 CARTER AVIATION TECHNOLOGIES, LLC 4 SR/C vs. Fixed Wing • SR/C rotor very low drag by being slowed Profile HP vs. -
Effectiveness of the Compound Helicopter Configuration in Rotorcraft Performance Increase
transactions on aerospace research 4(261) 2020, pp.81-106 DOI: 10.2478/tar-2020-0023 eISSN 2545-2835 effectiveness of the compound helicopter configuration in rotorcraft performance increase Jarosław stanisławski Retired doctor of technical sciences [email protected] • ORCID: 0000-0003-1629-4632 abstract The article presents the results of calculations applied to compare flight envelopes of varying helicopter configurations. Performance of conventional helicopter with the main and tail rotors, in the case of compound helicopter, can be improved by applying wings and pusher propellers which generate an additional lift and horizontal thrust. The simplified model of a helicopter structure, consisting of a stiff fuselage and the main rotor treated as a stiff disk, is applied for evaluation of the rotorcraft performance and the required range of control system deflections. The more detailed model of deformable main rotor blades, applying the Galerkin method, is used to calculate rotor loads and blade deformations in defined flight states. The calculations of simulated flight states are performed considering data of a hypothetical medium class helicopter with the take-off mass of 6,000kg. In the case of both of the helicopter configurations, the articulated main rotor hub is taken under consideration. According to the Galerkin method, the elastic blade model allows to compute blade deformations as a combination of the blade bending and torsional eigen modes. Introduction of additional wing and pusher propellers allows to increase the range of operational speed over 300 km/h. Results of the simulation are presented as time- runs of rotor loads and blade deformations and in a form of disk distribution plots of rotor parameters. -
Open Walsh Thesis.Pdf
The Pennsylvania State University The Graduate School College of Engineering A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT A Thesis in Aerospace Engineering by Gregory Walsh c 2016 Gregory Walsh Submitted in Partial Fulfillment of the Requirements for the Degree of Master of Science August 2016 The thesis of Gregory Walsh was reviewed and approved∗ by the following: Kenneth S. Brentner Professor of Aerospace Engineering Thesis Advisor Jacob W. Langelaan Associate Professor of Aerospace Engineering George A. Lesieutre Professor of Aerospace Engineering Head of the Department of Aerospace Engineering ∗Signatures are on file in the Graduate School. Abstract The desire for a vertical takeoff and landing (VTOL) aircraft capable of high forward flight speeds is very strong. Compound lift-offset coaxial helicopter designs have been proposed and have demonstrated the ability to fulfill this desire. However, with high forward speeds, noise is an important concern that has yet to be thoroughly addressed with this rotorcraft configuration. This work utilizes a coupling between the Rotorcraft Comprehensive Analysis System (RCAS) and PSU-WOPWOP, to computationally explore the acoustics of a lift-offset coaxial rotor sys- tem. Specifically, unique characteristics of lift-offset coaxial rotor system noise are identified, and design features and trim settings specific to a compound lift-offset coaxial helicopter are considered for noise reduction. At some observer locations, there is constructive interference of the coaxial acoustic pressure pulses, such that the two signals add completely. The locations of these constructive interferences can be altered by modifying the upper-lower rotor blade phasing, providing an overall acoustic benefit. -
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 -
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). -
(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. -
Zhejiang Geely Holding Group Co. Ltd. Assigned 'BBB-' Rating; Outlook Stable
Zhejiang Geely Holding Group Co. Ltd. Assigned 'BBB-' Rating; Outlook Stable 19-Mar-2019 05:38 EDT View Analyst Contact Information We expect Zhejiang Geely Holding Group Co. Ltd. to continue to gain market share, supported by good product design, improving quality, and a strong pipeline of new models at its subsidiaries. This is despite uncertainties in global auto demand. In our view, the China-based automaker will maintain modest leverage, thanks to its stable profitability and strong operating cash flows. On March 19, 2019, S&P Global Ratings assigned its 'BBB-' long-term issuer credit rating to Zhejiang Geely Holding. The stable outlook reflects our view that Zhejiang Geely Holding will continue to gradually grow its auto revenue and profit, and sustain moderate leverage over the next 12-24 months, despite a competitive and volatile market. HONG KONG (S&P Global Ratings) March 19, 2019--The rating on Zhejiang Geely Holding reflects our expectation that the company will continue to strengthen its position in the global and China's automotive industry over the next 12-24 months. In our view, Zhejiang Geely Holding could also improve its groupwide competitive position. This will be supported by sustained technology improvement, strong product pipeline, platform synergy, and successful marketing and sales execution of its major subsidiaries Geely Automobile Holdings Ltd. (Geely Auto), Lynk & Co, and Volvo Car AB (Volvo Car). We expect Geely Auto to continue its solid sales momentum over the next 12-24 months, outpacing market growth. The sales momentum would stem from the sustained quality improvements on the back of its research and development (R&D) effort and comprehensive cooperation with Volvo Car. -
Portola Valley Aircraft Noise Monitoring
Portola Valley Aircraft Noise Monitoring Prepared by San Francisco International Airport Aircraft Noise Abatement Office Technical Report #012017-978 January 2017 San Francisco International Airport Portola Valley Aircraft Noise Monitoring Report Page | 2 Table of Contents Executive Summary ................................................................................................................................ 3 Community and SFO Operations............................................................................................................ 3 Equipment ............................................................................................................................................... 3 Aircraft Noise Analysis........................................................................................................................... 4 Aircraft Operations ................................................................................................................................. 6 Track Density.......................................................................................................................................... 8 Noise Reporters....................................................................................................................................... 9 Conclusion ............................................................................................................................................ 10 Figure 1 ................................................................................................................................................ -
A New VTOL Propelled Wing for Flying Cars
A new VTOL propelled wing for flying cars: critical bibliographic analysis TRANCOSSI, Michele <http://orcid.org/0000-0002-7916-6278>, HUSSAIN, Mohammad, SHIVESH, Sharma and PASCOA, J Available from Sheffield Hallam University Research Archive (SHURA) at: http://shura.shu.ac.uk/16848/ This document is the author deposited version. You are advised to consult the publisher's version if you wish to cite from it. Published version TRANCOSSI, Michele, HUSSAIN, Mohammad, SHIVESH, Sharma and PASCOA, J (2017). A new VTOL propelled wing for flying cars: critical bibliographic analysis. SAE Technical Papers, 01 (2144), 1-14. Copyright and re-use policy See http://shura.shu.ac.uk/information.html Sheffield Hallam University Research Archive http://shura.shu.ac.uk 20XX-01-XXXX A new VTOL propelled wing for flying cars: critical bibliographic analysis Author, co-author (Do NOT enter this information. It will be pulled from participant tab in MyTechZone) Affiliation (Do NOT enter this information. It will be pulled from participant tab in MyTechZone) Abstract 2. acceleration of the fluid stream on the upper surface of the wing by mean of EDF propellers [13] that produces a much higher lift coefficient, with respect to any other aircrafts (up to 9-10); This paper is a preliminary step in the direction of the definition of a 3. very low stall speed (lower than 10m/s) and consequent increase radically new wing concept that has been conceived to maximize the of the flight envelope in the low speed domain up to 10÷12 m/s; lift even at low speeds. It is expected to equip new aerial vehicle 4. -
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. -
Geely Holding Group and Renault Group to Sign MOU on Joint Cooperation in China and South Korean Markets
Geely Holding Group and Renault Group to sign MOU on joint cooperation in China and South Korean Markets • Geely Holding and Renault Group have signed a MOU to accelerate ‘Renaulution Plan’ in China and South Korea. • In China, both partners will jointly introduce Renault-branded hybrid vehicles. • In South Korea, Geely Holding and Renault Group will explore localization of vehicles based on Lynk & Co energy efficient platforms. • Geely Holding and Renault Group will enhance their competitive advantages in technology and industrial systems to create leading mobility experience. 9th August 2021, Hangzhou China and Paris France. Renault Group, a global company with French roots and 120 years of history in the automotive industry, and Geely Holding Group, China’s largest privately-owned automotive group, today jointly announced an MoU framework agreement to create an innovative cooperation. The cooperation, focused on China and South Korea as initial key core markets, will allow Renault Group and Geely Holding to share resources and technologies. The focus will be on hybrid vehicles in the fast-growing Asian markets. Following the adoption by Geely Holding’s opensource strategy for its full vehicle architectures, Geely Holding will partner with Renault Group in the Chinese and Korean markets. In China, based on Geely Holding’s existing technologies and mature industrial footprint, both partners will jointly introduce Renault- branded hybrid vehicles. Renault will contribute on branding strategy, channel and service development, defining appropriate customer journey. In South Korea, where Renault Samsung Motors has over two decades of experience, the MoU allows Renault Group and Geely Holding to jointly explore localization of vehicles based on Lynk & Co’s energy-efficient vehicle platforms for local markets. -
Scottsdale Airport Advisory Commission Meeting Notice and Agenda
SCOTTSDALE AIRPORT ADVISORY COMMISSION MEETING NOTICE AND AGENDA Wednesday, June 16, 2021 5:00 p.m. Meeting will be held electronically and remotely AIRPORT ADVISORY COMMISSION John Berry, Chair Cory Little Charles McDermott Vice-Chair Peter Mier Larry Bernosky Rick Milburn Ken Casey Until further notice, Airport Advisory Commission meetings are being held electronically. While physical facilities are not open to the public, Airport Advisory Commission meetings are available on Scottsdale’s YouTube channel to allow the public to virtually attend and listen/view the meeting in progress. 1. Go to ScottsdaleAZ.gov, search “live stream” 2. Click on “Scottsdale YouTube Channel” 3. Scroll to “Upcoming live streams” 4. Select the applicable meeting Spoken comment is being accepted on agenda action items. To sign up to speak on these please click here. Request to speak forms must be submitted no later than 90 minutes before the start of the meeting. Written comment is being accepted for both agendized and non-agendized items, and should be submitted electronically no later than 90 minutes before the start of the meeting. To submit a written public comment electronically, please click here Call to Order Roll Call Aviation Director’s Report The public body may not propose, discuss, deliberate or take legal action on any matter in the summary unless the specific matter is properly noticed for legal action. 18894560-v1 Approval of Minutes Regular Meeting: May 19, 2021 REGULAR AGENDA ITEMS 1-9 How the Regular Agenda Works: The Commission takes a separate action on each item on the Regular Agenda 1. Discussion and Possible Action regarding application for Airport Aeronautical Business Permit for C.