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«ANSAT Helicopter»

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«ANSAT Helicopter»


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Key dates Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 2 1995 – development star 17 августа 1999 года – first flight 2002 – certification test flights 2004 – type certificate 2005 – type certificate for two pilot helicopter 2005 – supplementary certificate for emergency splashdown system Aerazur 2005 – serial production start


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 3 Key dates Supplementary certificate on hydro-mechanic control system - June 2012. Supplementary certificate on HEMS module – October 2012.


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 4 General view


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 5 Main technical characteristics Meets AP-29 requirements to rotorcraft category А Design with single main rotor and tail rotor Hinge-free hub of main rotor Fiberglass plastic of main and tail rotors’ blades Two different control systems 4-fold redundant Fly-by-wire control system hydromechanical control system PW-207K engines by Pratt & Whitney (Canada) Onboard information check system Skid landing gear


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 6 Main flight performance


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 7 Power plant Comprises of two PW-207K engines with single-stage centrifugal compressor and single-stage axial turbine of gas generators Digital electronic regulators (FADEC) ensures continuous rotation speed of main rotor Emergency mechanical system of manual control is available Electric start-up in automatic or manual modes PW-207K operating modes: 2.5 min OEI 710 hp Continuous OEI 648 hp Take-off 630 hp Max continuous 558 hp


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 8 Cockpit Two shock-absorbing seats Fisher Two jettisonable doors Traditional controls Windscreen wipers for one pilot (basic variant)


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 9 Cockpit for two pilots (basic variant) for two pilots


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Control system – hydromechanical control system Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 10 СВА Flexball СВА Flexball control linkage Applied by: Eurocopter (EC120, Ecureuil, Dauphin, Super Puma, EC155, EC175 , EC135, EC145, NH90), Airbus (A320, A330, A380), Dassault Aviation (Falcon family) Areas of application in the helicopters: Main and tail rotor control (+ fenestron) MR brake control Manual engines control Rafts (floats) emergency release control Fire extinguishers control Advantages: Light weight Ease of routing in the helicopter No maintenance is required


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 11 Current status Control system – hydromechanical control system Main and tail rotor mechanical control system with the use of CBA Flexball flexible control linkage is developed System provides for installation of electrical actuators Stability augmentation system (SАS-А) allows application of electrical actuators


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 12 Fly-by-wire Control system Control system is electrohydraulic with 4-fold electric redundancy and 2-fold hydraulic redundancy Includes: Traditional controls with electric sensors Electronic module (computer) Panel Electrohydraulic control actuator Roll rate sensors Swash plate Rods in aft-booster bay


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 13 Main rotor Main rotor hug is hinge-free, torsion bar is a resilient element, made of composite materials. No lubrication required. Main rotor blade is rectangular in plan, made of composites, features erosion-preventive binding and trimmer plate.


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 14 Onboard information check system Composition: two electronic raster multifunctional displays ИМ-14 computation and formation unit БВФ-А indication control panel ПУИ-А Functions: input of parametric and signaling information from engines and systems formation and output of information to protected data storage device input of pre-flight details data gathering and real-time processing, output of data on systems’ status and remaining service life Provides: Duplicate check of onboard systems Complex intra-cockpit warning Data loading and off-loading to portable computer Pre-flight and post-flight check of systems’ and aggregates’ status


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 15 Operational features Features of Ansat operation by Forestry Aviation of South Korea Monitoring of forests, fire-fighting and pest control Most of the sorties performed at economical speed Performs terrain following flights in mountainous areas Features of Ansat operation by Radar-MMS, JSC Testing of special electronic equipment, including in the areas of HIRF impact Cleared for operation with MTOW 3,600 kg Features of Ansat operation by Aviation of Russian Federal Security Bureau Supervision and flight crew training Nap-of-the-earth flights, hot and high sorties


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 16 Operational experience


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 17 Program «Ansat» Ansat – U Main differences: Derived from Ansat Skid landing gear replaced with wheels Flight engineer introduced to the crew Amended onboard equipment suite Key tasks: Initial pilot training Training of instructors


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 18 Ansat - U 29.10.2008 – signed Act on State Joint Trials 2 prototypes built 2009 – launch of production Delivered: 2009 – 6 helicopters 2010 – 2 helicopters 2011 – 5 helicopters (in production) Over 40 helicopters to be produced by 2018


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 19 Operation of Ansat - U


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 20 Total flight hours


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Assigned service life Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 21


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 22 Supply support Facilities of towing, containment, tie-down, transport Lift facilities Assembly access facilities Assembly-dismantling facilities Ground support facilities


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 23 Supply support Operating stock Handling facilities of the systems and units Helicopter protection facilities on the ground Helicopter support tool Power source Ground support facilities


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 24 Training Complex - Structure Flight-navigation simulator Ground based complex of training Training simulator Training computer class Visual laboratory resources


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 25 Training complex visual aid Назначение Design description Operation specifics Flight crew instructions Technical stuff instructions Состав Posters set (6 sets) Printed materials (19 books) 12 flight crew instructions 7 Technical stuff instructions


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 26 Training complex – training computer class Purpose for theoretical training: Computer aided training programs; electronic technical documentation; electronic cockpit.


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 27 Procedural simulator Возможности Selecting various training exercises Registration Action trainee for analysis Purpose: Aircrew training; intended for initial training; “light” version of flight-simulator;


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 28 Flight simulator Purpose: Aircrew training Total simulation of the flight Intended for initial training (engine start, takeoff) Crew training on the main training stage on the entire task complex Effect: reducing the cost of training; reducing (50-70%) fuel consumption; reducing the preparation time; improving safety


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 29 ILS. Development prospects “One stop shop” concept Global Service Net Rise of aircrew and technical staff level New cooperation format IT technology (web-portal, cMRO system) Complex service contracts Power by the hour scheme


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 30 Configurations CARGO & PASSENGER PASSENGER EXECUTIVE SEARCH & RESCUE MEDEVAC SCAUT


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 31 The overall cabin volume is 8 m3 and there are six cargo retainers available… CARGO & PASSENGER Configurations … Simple transformation for 8 passengers transportation.


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 32 PASSENGER Configuration Emergency exit Passenger seat «Sigma» Helios Wardrobe ANSAT PASSENGER specialized configuration provides comfortable transportation of 6 persons.


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 33 EXECUTIVE Configuration ANSAT EXECUTIVE Configuration is a combination of the high level comfort and mobility. The cabin provides an opportunity to install different types of interior parts, cloakroom, luggage compartment and lavatory.


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 34 ANSAT Basic Multipurpose can be easily transformed to Search and Rescue (SAR) configuration by special equipment setting. Unique performances of Ansat permit to operate helicopter in all-weather conditions at Day and Night time. SEARCH & RESCUE Configurations


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 35 MEDEVAC Configurations Light medical issues can be solved by ANSAT Basic Multipurpose with limited medical equipment. The Medevac is used for the following purposes: Urgent delivery of an emergency medical team to the scene of accident; Rendering emergency medical aid to the injured and suffering; Evacuation of casualties and survivors to healthcare facilities


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2 patients and 2 paramedics in HEMS configuration Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 36 Functionality Transportation up to 7 passengers HOT&HIGH operations Compliance with  SAR helicopter requirements Up to 2 stretchers installation HIGE 3000 м Service ceiling 4 800 м ОАТ -50 до +50 Largest capacity in light twin turbo class 8 m3 SAR winch installation High climb rate (12 m/s) maximum speed ( 270 km/h) wide sliding door,


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 37 Why Ansat Ansat – is the best proposal for your business. It is best in terms price-vs-functionality Balanced performance Price – more than 20% lower than other in class Lower operational expenses


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 38 We are waiting for your interest. We would be proud to give you more information on the static. We would be glad to provide you with information about PRICE on every configuration. Let us know you need Ansat


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Авторские права. 2011. ОАО "Вертолеты России". Все права защищены 39 Thank you for your attention! Россия, 107113, Москва Сокольнический вал 2А, стр. 2 Тел.: +7(495) 6275545 add. 228 Моб.: +7(915) 384-8193 E-mail: ivancov@rus-helicopters.com


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