Презентация на тему "«ANSAT Helicopter»"

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Презентация на тему "«ANSAT Helicopter»" по иностранным языкам. Состоит из 39 слайдов. Размер файла 6.99 Мб. Каталог презентаций в формате powerpoint. Можно бесплатно скачать материал к себе на компьютер или смотреть его онлайн с анимацией.

Формат

pptx (powerpoint)
Количество слайдов

39
Слова

английский язык
Конспект

Отсутствует

Содержание

Слайд 1
«ANSAT Helicopter»
Слайд 2
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
Слайд 3

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 3 Supplementary certificate on hydro-mechanic control system -June 2012. Supplementary certificate on HEMS module – October 2012.
Слайд 5
Main technical characteristics

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 5 Meets AP-29 requirements to rotorcraft category А Design with single main rotor and tail rotor Hinge-free hubof main rotor Fiberglass plastic of main and tail rotors’ blades Two different control systems 4-fold redundant Fly-by-wire control system hydromechanicalcontrol system PW-207K engines by Pratt&Whitney (Canada) Onboard information check system Skid landing gear
Слайд 7
Power plant

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 7 Comprises of twoPW-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 minOEI 710 hp ContinuousOEI 648hp Take-off 630 hp Max continuous558 hp
Слайд 8
Cockpit

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 8 Two shock-absorbing seatsFisher Two jettisonable doors Traditional controls Windscreen wipers for one pilot (basic variant)
Слайд 10
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), DassaultAviation (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
Слайд 11

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 11 Current status 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
Слайд 12
Fly-by-wireControl system

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 12 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
Слайд 13
Main rotor

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 13 Main rotor hug is hinge-free, torsion bar is a resilient element, made of composite materials. No lubrication required. Main rotor blade is rectangularin plan, made of composites, featureserosion-preventivebinding and trimmer plate.
Слайд 14
Onboard information check system

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 14 Composition: two electronic raster multifunctional displaysИМ-14 computation and formation unitБВФ-А indication control panel ПУИ-А Functions: input of parametric and signaling information from engines and systems formationand 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
Слайд 15
Operational features

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 15 Features of Ansat operation by Forestry Aviation of South Korea Monitoring of forests, fire-fightingand pest control Most of the sorties performed at economical speed Performs terrain following flights in mountainous areas Features of Ansat operation byRadar-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
Слайд 17

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
Слайд 18
Ansat - U

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 18 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
Слайд 22
Ground support facilities

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
Слайд 23

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
Слайд 24
Training Complex - Structure

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 24 Flight-navigation simulator Ground based complex of training Training simulator Training computer class Visual laboratory resources
Слайд 25
Training complex visual aid

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 25 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
Слайд 26
Training complex – training computer class

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 26 Purpose for theoretical training: Computer aided training programs; electronic technical documentation; electronic cockpit.
Слайд 27
Procedural simulator

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 27 Возможности Selecting various training exercises Registration Action trainee for analysis Purpose: Aircrew training; intended for initial training; “light” version of flight-simulator;
Слайд 28
Flight simulator

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 28 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
Слайд 29
ILS. Development prospects

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 29 “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
Слайд 31

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 31 The overall cabin volume is 8 m3 and there aresix cargo retainers available… CARGO & PASSENGER Configurations Program «Ansat» … Simple transformation for 8 passengers transportation.
Слайд 32

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.
Слайд 33

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.
Слайд 34

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
Слайд 35

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
Слайд 36
Functionality

2 patients and 2paramedics in HEMS configuration Авторские права.2011.ОАО "Вертолеты России". Все права защищены 36 Transportation up to 7 passengers HOT&HIGH operations Compliance with SAR helicopter requirements Up to 2stretchers 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,
Слайд 37
Why Ansat

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 37 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
Слайд 38
Let us know you need Ansat

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. Ivancov AndreyV. +7 (495) 6275545 +7 (915) 3848193 ivancov@rus-helicopters.com Kiyamov MaratR. +7 (843) 550 0000 kiyamov_mr@kazanhelicopters.com
Слайд 39
Thank you for your attention!

Авторские права.2011.ОАО "Вертолеты России". Все права защищены 39 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