DOCSLIB.ORG

Ellipse Spirit MH−46 Eclipse Legend UL-LSA AIRCRAFT

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Ellipse Spirit MH−46 Eclipse Legend UL-LSA AIRCRAFT UL-LSA AIRCRAFT AeroSette MH−46 Eclipse Ultralight two−seat braced high−wing mono- plane. It is very controllable and features a spacious cockpit for two side−by−side pilots. The tricycle undercarriage is fixed, power is provided by Rotax 912S engine, turning a three−bladed variable−pitch pro- peller. (5 aircraft produced so far.) Span 9,80 m, length 6,75 m, wing area 11,30 m2, cruising speed 190 − 250 km/h. AeroSette, spol. s r.o., Nádražní 20, 463 31 Chrastava, Cze ch Republic www.aerosette.eu DRAFTDRAFTe−mail: [email protected] DRAFT A2 CZ Ellipse Spirit A side-by-side two seat low-wing aircraft with T-tail and retractable landing gear made of carbon fiber and honeycomb sandwich. Powered by Rotax 912/914, UL Power 260/350 or Lycoming 233. Two prototypes are flying and the certification process is in progress. Basic price from 82 000 EUR. Span 8 m (8,6 m), length 6,55 m, wing area 9,48 m2 (10,34 m2), empty weight 295 - 339 kg, (with BRS and safety fuel cells), cruising speed 230 - 290 km/h. A2 CZ, s.r.o. Ráby 23 533 52 Staré Hradiště Czech Republic www.ellipse-spirit.com DRAFTe-mail: [email protected] DRAFT Aeropilot DRAFT Legend Full-composite high-wing aircraft Legend is intended for sport, recreation and touristic flying. This aircraft is suitable for flight tra- ining. LSA (600 kg) / UL (472 kg) / ELSA (540 kg) versions are powered by Rotax 912 UL or 912 ULS engines. LSA (600 kg) version is powered by Lycoming 0235 engine. The propeller is two- or three-bladed, fixed or adjustable. 3 prototypes have been built. Span: 9,06 m, Length: 7 m, wing area: 10,54 m2, weight: 280 – 297 kg, max. horizontal speed: 225 km/h. Aeropilot, s.r.o. Jeníkovská 1815 28601 Čáslav Czech Republic http://www.aeropilotcz.com e-mail: [email protected] DRAFT6 DRAFTDRAFT CZECH AVIATION 2012 Aerospool CZ ULL Classic A two-seat, side-by-side high-wing braced composite monoplane for both ULL and LSA category. Powered by the Rotax 912 UL / ULS with on-ground adjustable or constant speed propeller. Span 9,1 m, lenght 6,3 m, wing area 9,9 m2, empty weight 285 kg, cruising speed 180 - 220 km/h. Aerospool CZ, s.r.o., Hlavní 439, 687 25 Hluk, Czech Republic www.aerospool.cz DRAFT DRAFTDRAFTe-mail: [email protected] AirLony Skylane UL A two-seat side-by-side braced high-wing ultralight monoplane of mixed, mainly com- posite structure. Fixed tricycle undercarriage. The aircraft is designed for a wide range of use – from a trainer to a long distance tourer. Main features are: roomy luggage compart- ment, high useful load, high cruising speed, long flying range. It is powered by Rotax 912. (So far 62 aircraft built.) Span: 8,95 m, length: 6,65 m, wing area: 10,57 m2, empty weight: 248 kg, cruising speed: 135 - 210 km/h. AirLony, Nové Náměstí 702, 411 08 Štětí, Czech Republic www.airlony.cz DRAFT DRAFTe−mail: [email protected] DRAFT AirLony Highlander A tandem two-seat ultralight biplane of mixed, mainly composite structure. Fixed tailwheel undercarriage. Highlander is designed for leisure and joyful flying with emphasis on safety. The aircraft is pow- ered by Rotax 912 ULS and has increased G-limits up to +6/-4g. Span: 7,3 m, length: 6,05 m, wing area: 14,3 m2, empty weight: 230 kg, cruising speed: 100 – 140 km/h. AirLony, Nové Náměstí 702, 411 08 Štětí, Czech Republic www.airlony.cz e−mail: [email protected] DRAFTDRAFT DRAFT7 UL-LSA AIRCRAFT Atec Atec 122 Zephyr A two−seat side−by−side low−wing ultra light airplane of mixed (composite and wood) structure. Fixed tricycle undercar- riage. Powered by Rotax 912UL or ULS, with fixed or variable−pitch propellers. (220 units built so far.) Span 9,40 m, length 6,20 m, wing area 10,30 m2, empty weight 275 kg, max. level speed VH 245 km/h. Atec, v.o.s., Opolanská 350, 289 07 Libice nad Cidlinou, Czech Republic www.atecaircraft.eu DRAFTDRAFTe−mail: [email protected] DRAFT Atec Atec 321 Faeta A two−seat side−by−side low−wing ultra light airplane of mixed (composite and wood) structure. Fixed tricycle undercar- riage. Powered by Rotax 912UL or ULS, with fixed or variable−pitch propellers. The aircraft is also certified for towing. The Atec 322 Faeta is the LSA version. (So far 80 machines built.) Span 9,60 m, length 6,20 m, wing area 10,10 m2, empty weight 268 kg, max. level speed VH 250 km/h. Atec, v.o.s., Opolanská 350, 289 07 Libice nad Cidlinou, Czech Republic www.atecaircraft.eu DRAFTe−mail: [email protected] DRAFT Atec DRAFT Atec 212 Solo A single−seat ultralight airplane of com- posite structure. Fixed tailwheel undercar- riage. Stressed for +6/−3 g. Powered by Rotax 582 UL DCDI or 912 UL. (So far 8 machines built.) Span 7,50 m, length 5,26 m, wing area 7,30 m2, empty weight 200 kg, max. level speed VH 245 km/h. Atec, v.o.s., Opolanská 350, 289 07 Libice nad Cidlinou, Czech Republic www.atecaircraft.eu e−mail: [email protected] DRAFT8 DRAFTDRAFT CZECH AVIATION 2012 BRM Aero Bristell UL, ELSA, LSA, RG – an all-metal two- seater powered by Rotax 912 ULS, 912 iS, Jabiru 2200/3300 engines. Ultralight aero- plane Bristell is intended for flight training in flight schools, glider towing and recre- ational flying. Thanks to large cockipt and good ergonomy Bristell is an ideal vehicle for long cross country flights. 25 Bristells have been built so far. Span 8,13 m, length 6,45 m, wing area UL/LSA,RG 10/11,75 m2, empty weight UL/LSA, RG 290/320 kg, cruising speed UL/LSA,RG 214/240 km/h. BRM Aero s.r.o., Václava Kulíška 1224, 686 05 Uherské Hradiště, Czech Republic DRAFT www.brmaero.com DRAFT [email protected] Czech Sport Aircraft PS-28 Cruiser All-metal, two-seater, low-wing LSA air- plane, intended for training, tourist flying and towing of gliders. The aircraft is normally equipped with Rotax 912 ULS engine and a three-blade fixed propeller. Nevertheless, a variable pitch propeller installation is possible as well. The total number of aircraft produced is 469. Span 8,53 m, length 6,16 m, wing area 12,3 m2, empty weight 370 kg, cruising speed 200 km/h. Czech Sport Aircraft a.s., Na Záhonech 1177/212, Kunovice 686 04, Czech Republic Phone: + 420 576 514 032 Fax: + 420 576 519 394 e-mail: [email protected] DRAFT DRAFTwww.czechsportaircraft.com DRAFT Czech Sport Aircraft PS-10 Tourer All-metal, two-seater, high-wing LSA air- plane, intended for training, tourist and patrol flights. The airframe design concept is adjusted to this purpose – self-supporting wing and the cockpit situated on the wing leading edge level to provide en excellent view for the crew. Powered with Rotax 912 ULS engine and a three-blade fixed propel- ler. One prototype of this model was built. Span 9,5 m, length 7,1 m, wing area 11,5 m2, empty weight 375 kg, cruising speed 210 km/h. Czech Sport Aircraft a.s., Na Záhonech 1177/212, Kunovice 686 04, Czech Republic Phone: + 420 576 514 032 Fax: + 420 576 519 394 e-mail: [email protected] www.czechsportaircraft.com DRAFTDRAFT DRAFT9 UL-LSA AIRCRAFT Direct Fly Alto An all−metal cantilever low−wing ultralight monoplane, seating two side−by−side. Alto can be delivered in the TW version with a tailwheel or in the TG version with a tricycle undercarriage. Powered by Rotax 912 or Jabiru (60 kW / 80 hp to 90 kW / 120 hp range). Also available as a kit for homebuilders in various stages of assem- bly. (41 aircraft have been built so far) Span 8,20 m, length 6,25 m, wing area 10,50 m2, empty weight 285 kg, cruising speed 195 km/h. Direct Fly, s.r.o., Cihelní 573, 687 25 Hluk, Czech Republic DRAFT www.directfly.cz DRAFT DRAFTe−mail: [email protected] Direct Fly Argo Classical all-metal high-wing ultralight or LSA aircraft, with side-by-side seats, powered by Rotax 912 UL/ULS. Designed to be ideal for training and also for cross-country flying. Span 9,0 m, length 5,58 m, wing area 9,9 m2, empty weight UL / LSA, ELSA 282 / 297 kg, cruising speed 200 km/h. Direct Fly, s.r.o., Cihelní 573, 687 25 Hluk, Czech Republic www.directfly.cz DRAFTe−mail: [email protected] DRAFT Distar DRAFT UFM−13 Lambada A side-by-side two-seat, mid-wing ultra- light of composite structure. Fixed tricycle or tailwheel undercarriage. Powered by Rotax 912 UL, ULS or Jabiru 2200 engi- nes, with fixed or variable-pitch propeller. The wing may be fitted with wingtip exten- sions, increasing the span to 15 m. (About 140 aircraft in the UFM-11-13 version have been produced so far.) Span 13,0 0 m, length 6,60 m, wing area 12,60 m2, empty weight 265 − 280 kg, cruising speed 135 km/h. Production division: Company headquarters: Distar − Air, Distar CZ, a.s., U Letiště 1381 1. máje 228 562 01 Ústí nad Orlicí 504 01 Nový Bydžov Czech Republic Czech Republic e-mail: [email protected] e-mail: [email protected] www.sambaXXL.com www.distar.cz DRAFT10 DRAFTDRAFT CZECH AVIATION 2012 Distar Samba XXL A low-wing, composite side-by-side two- seat ultra-light monoplane.
Load more

Recommended publications
  • TŘICÁTÁ LÉTA – ZLATÝ VĚK Třicátá Léta – Zlatý Věk
    TŘICÁTÁ LÉTA – ZLATÝ VĚK Třicátá léta – zlatý věk Světová hospodářská krize, která vypukla v roce prací přidělovalo jednotlivým aeroklubům. Kromě 1929, se v negativním smyslu slova podepsala tradičních výrobců letadel Aero, Avia a Letov zamě- i na rozvoji našeho sportovního letectví. Průmys- řených spíše na státní a zejména vojenské zakázky lová výroba prudce klesala, v roce 1933 až na 60 % se výrobou sportovních letadel začaly zabývat firma úrovně dosažené v roce 1929, a úměrně s klesající Baťa v Otrokovicích, kopřivnická Tatra, leteckou průmyslovou produkcí rostla nezaměstnanost, která výrobu v koncernu ČKD takřka v hodině dvanácté v roce 1934 dosáhla více než 17 %. Tato situace se zachraňuje slavná Praga E 114 Air Baby a 1. dubna pochopitelně odrazila i poklesem aktivity v oblasti roku 1935 je založena firma Ing. Pavel Beneš, Ing. J. sportovního letectví. Ve výrobních programech Mráz, továrna na letadla v Chocni. Kromě sportov- našich leteckých továren nebylo pro sportovní leta- ních letadel vzniká celá řada projektů tzv. lidových dla místo, ostatně nebyl nikdo, kdo by je kupoval, letadel. Druhá polovina třicátých let minulého století a tak byl výrobní program orientován až na výjimky by se skutečně mohla nazvat zlatým věkem v historii na zakázky určené pro Ministerstvo národní obrany. našeho letectví. V aeroklubech si museli letečtí nadšenci vystačit s letitými „Branďáky“ – Aero A-1, A-15 a A-26, pří- padně „Sardinkami“ Letov Š-10. Pokud se aeroklubu Letov Š-25 1930 anebo i jednotlivým soukromníkům podařilo získat Cvičný, pokračovací výcvik – prototyp z armády vyřazené Letovy Š-18, Š-118, Š-218 nebo Avii BH-9, BH-10, BH-11, dalo se mluvit o velkém Na základě soutěže, kte- Technická data štěstí a možnosti létat s moderním letadlem umožňu- rou v roce 1931 vypsalo jícím akrobatické prvky.
    [Show full text]
  • Download (4MB)
    https://theses.gla.ac.uk/ Theses Digitisation: https://www.gla.ac.uk/myglasgow/research/enlighten/theses/digitisation/ This is a digitised version of the original print thesis. Copyright and moral rights for this work are retained by the author A copy can be downloaded for personal non-commercial research or study, without prior permission or charge This work cannot be reproduced or quoted extensively from without first obtaining permission in writing from the author The content must not be changed in any way or sold commercially in any format or medium without the formal permission of the author When referring to this work, full bibliographic details including the author, title, awarding institution and date of the thesis must be given Enlighten: Theses https://theses.gla.ac.uk/ [email protected] RESEARCH, DEVELOPMENT AND MANUFACTURING POTENTIAL OF THE GENERAL AVIATION AIRCRAFT INDUSTRY IN THE CZECH REPUBLIC L. SMRCEK Department of Aerospace Engineering University of Glasgow. September 1996 © L. Smrcek ProQuest Number: 10391352 All rights reserved INFORMATION TO ALL USERS The quality of this reproduction is dependent upon the quality of the copy submitted. In the unlikely event that the author did not send a com plete manuscript and there are missing pages, these will be noted. Also, if material had to be removed, a note will indicate the deletion. uest ProQuest 10391352 Published by ProQuest LLC (2017). Copyright of the Dissertation is held by the Author. All rights reserved. This work is protected against unauthorized copying under Title 17, United States C ode Microform Edition © ProQuest LLC. ProQuest LLC.
    [Show full text]
  • Los Motores Aeroespaciales, A-Z
    Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 < aeroteca.com > Depósito Legal B 9066-2016 Título: Los Motores Aeroespaciales A-Z. © Parte/Vers: 1/12 Página: 1 Autor: Ricardo Miguel Vidal Edición 2018-V12 = Rev. 01 Los Motores Aeroespaciales, A-Z (The Aerospace En- gines, A-Z) Versión 12 2018 por Ricardo Miguel Vidal * * * -MOTOR: Máquina que transforma en movimiento la energía que recibe. (sea química, eléctrica, vapor...) Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 Este facsímil es < aeroteca.com > Depósito Legal B 9066-2016 ORIGINAL si la Título: Los Motores Aeroespaciales A-Z. © página anterior tiene Parte/Vers: 1/12 Página: 2 el sello con tinta Autor: Ricardo Miguel Vidal VERDE Edición: 2018-V12 = Rev. 01 Presentación de la edición 2018-V12 (Incluye todas las anteriores versiones y sus Apéndices) La edición 2003 era una publicación en partes que se archiva en Binders por el propio lector (2,3,4 anillas, etc), anchos o estrechos y del color que desease durante el acopio parcial de la edición. Se entregaba por grupos de hojas impresas a una cara (edición 2003), a incluir en los Binders (archivadores). Cada hoja era sustituíble en el futuro si aparecía una nueva misma hoja ampliada o corregida. Este sistema de anillas admitia nuevas páginas con información adicional. Una hoja con adhesivos para portada y lomo identifi caba cada volumen provisional. Las tapas defi nitivas fueron metálicas, y se entregaraban con el 4 º volumen. O con la publicación completa desde el año 2005 en adelante. -Las Publicaciones -parcial y completa- están protegidas legalmente y mediante un sello de tinta especial color VERDE se identifi can los originales.
    [Show full text]
  • National Air & Space Museum Technical Reference Files: Propulsion
    National Air & Space Museum Technical Reference Files: Propulsion NASM Staff 2017 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Scope and Contents........................................................................................................ 1 Accessories...................................................................................................................... 1 Engines............................................................................................................................ 1 Propellers ........................................................................................................................ 2 Space Propulsion ............................................................................................................ 2 Container Listing ............................................................................................................. 3 Series B3: Propulsion: Accessories, by Manufacturer............................................. 3 Series B4: Propulsion: Accessories, General........................................................ 47 Series B: Propulsion: Engines, by Manufacturer.................................................... 71 Series B2: Propulsion: Engines, General............................................................
    [Show full text]
  • Engines by Manufacturer
    mmmm 39002 10553 1272 WORK PROJECTS ADMIMISXRAIION BIBLIOGRAPHY OF AERONAUTICS Part 54 - Engines - By Manufacturer Compiled from the IUDEX OF AERONAUTICS of the INSTITUTE OF THE AERONAUTICAL SCIENCES 30 Rockefeller Plaza New York City This Index has been prepared for publication by workers under the supervision of the FEDERAL WORKS AGENCY V/QRK PROJECTS ADMINISTRATION For the City of New York 0.P.65-1-97-21-W. P. 14 December 1939 FOREWORD This bibliography is one of a series pertaining to aero­ nautics and is published by the Work Projects Adminis­ tration with funds allotted to 0- P. 65-1-97-21 - W.P. 14 for that purpose. They may not be sold. The project, sponsored by the Mayor of the City of New York, receives the cooperation of the Institute of the Aeronautical Sciences which directs the research and publish­ ing staff workers. Bequest for Additional References The Institute of the Aeronautical Sciences invites cor­ rections and criticism of the bibliographies and requests that additional references be forwarded to the Institute for inclusion in the final publications. Distribution Requests Persons and organizations desiring copies may apply for theia by letter, stating the use for Y/hich they are required. These requests will be considered in the order received. Should the supply be exhausted, such requests will receive first consideration when additional copies are published. Robert R. Dexter Aeronautical Engineer Address all correspondence to: John H. Palmer Work Projects Administration 5111 R.C.A. Building New York City ABBREVIATIONS A.R.C. R. & M. - Great Britain. Aeronautical research committee.
    [Show full text]
  • Czech Aviation 2011 Czech Aviation 2011 - Contents
    CZECH AVIATION 2011 CZECH AVIATION 2011 - CONTENTS AIRCRAFT AeroSette, spol. s r.o., MH−46 Eclipse 6 Shark.Aero CZ s.r.o. Shark 17 Aerospool CZ, s.r.o. ULL Classic 6 TL-ultralight s.r.o. TL-2000 Sting S4 17 AirLony Skylane 6 TL-ultralight s.r.o. TL-3000 Sirius 17 AirLony Highlander 7 TL-ultralight s.r.o. TL-2000 Sting 18 Atec, v.o.s., Atec 321 Faeta 7 Tomark Aero CZ s.r.o. Viper SD-4 18 Atec, v.o.s., Atec 212 Solo 7 Tomáš Podešva, VO ULL Tulák Dandy 18 Atec, v.o.s., Atec 122 Zephyr 8 Tomáš Podešva, VO ULL Piper UL Cubby 19 Aveko Aircraft, a.s., VL−3 Sprint 8 Tomáš Podešva, VO ULL Trener UL 19 BRM Aero s.r.o. NG 5 8 Zlin Aviation, s.r.o. Savage 19 Czech Sport Aircraft a.s. PS-28 Cruiser 9 Vladimír Rajchl S−Wing 20 Czech Sport Aircraft a.s. PS-10 Tourer 9 Tomi−Aviation - M. Řehák Tomi−Cross 5 Sport 20 Direct Fly, s.r.o., Alto 9 Gramex, s.r.o. Sonet 20 Direct Fly, s.r.o., Argo 10 Gramex, s.r.o. Sonata 21 Dova Aircraft, s.r.o., DV−1 Skylark 10 Gramex, s.r.o. Song 21 Distar CZ, a.s. UFM−13 Lambada 10 Phoenix Air, s.r.o. U−15 Phoenix 21 Distar CZ, a.s. Samba XXL 11 ProFe Banjo MH 22 Eurodisplay, s.r.o. SR−01 Magic 11 ProFe Duo Banjo 22 Evektor−Aerotechnik, a.s.
    [Show full text]
  • DIRECTORATE GENERAL of CIVIL AVIATION AIRWORTHINESS NOTICE No. 17 Issue 1 25 October 1990 USE of MOTOR GASOLINE (MOGAS) in CERT
    DIRECTORATE GENERAL OF CIVIL AVIATION AIRWORTHINESS NOTICE No. 17 Issue 1 25 October 1990 USE OF MOTOR GASOLINE (MOGAS) IN CERTAIN LIGHT AIRCRAFT 1- Introduction Because of the growing difficulties experienced in obtaining Aviation Gasoline (Avgas), particularly in small quantities, and the ready availability of Motor Gasoline (MOGAS), DGCA have been asked to consider permitting the use of motor gasoline in general aviation aircraft. As a first step it has been agreed to permit the use of MOGAS in certain defined aircraft using low compression ratio unsupercharged engines, (See Appendix, Schedule 1). In such aircraft any adverse effects of using MOGAS are likely to be minimal and, if present, are likely to become apparent over a sufficiently long period to enable them to be controlled satisfactorily by normal maintenance procedures. Accordingly, the DGCA has issued an Exemption, in the terms set out in the Appendix to this Notice, form compliance with the fuel specifications and associated limitations set out in the Official Manuals forming part of the Certificate or Airworthiness. DGCA will give Page 1 consideration to individual applications in respect of aircraft not listed in the Schedule. (See paragraph 2.3). Fuel Obtained direct from a filling station forecourt may be acceptable in accordance with the provisions of Airworthiness Notice No. 17A. CAUTION: BS 7070 (unleased) MOGAS or MOGAS of any standard other than BS 4040 is not permitted by either this Notice No. 17. or Airworthiness Notice No. 17A. 2 General 2.1 It should be noted that although DGCA is satisfied that the listed aircraft/engines may be operated with adequate safety on MOGAS, provided the limitations* are observed, DGCA takes no responsibility for infringement of manufacturer' s warranty, accelerated deterioration of the engine or airframe components, or any other long term deleterious effects.
    [Show full text]