Презентация "«ANSAT Helicopter»" – проект, доклад

«ANSAT Helicopter»

Key dates

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

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

Supplementary certificate on hydro-mechanic control system - June 2012. Supplementary certificate on HEMS module – October 2012.

General view

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

Main flight performance

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

Cockpit

Two shock-absorbing seats Fisher Two jettisonable doors Traditional controls Windscreen wipers

for one pilot (basic variant)

for two pilots (basic variant) for two pilots

Control system – hydromechanical control system

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

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

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

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.

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

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

Operational experience

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

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

Operation of Ansat - U

Total flight hours

Assigned service life

Supply support Facilities of towing, containment, tie-down, transport Lift facilities Assembly access facilities Assembly-dismantling facilities

Ground support facilities

Supply support Operating stock Handling facilities of the systems and units Helicopter protection facilities on the ground Helicopter support tool Power source

Training Complex - Structure Flight-navigation simulator Ground based complex of training Training simulator Training computer class Visual laboratory resources

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

Training complex – training computer class

Purpose for theoretical training: Computer aided training programs; electronic technical documentation; electronic cockpit.

Procedural simulator

Возможности Selecting various training exercises Registration Action trainee for analysis

Purpose: Aircrew training; intended for initial training; “light” version of flight-simulator;

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

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

Configurations

CARGO & PASSENGER PASSENGER EXECUTIVE SEARCH & RESCUE MEDEVAC SCAUT

The overall cabin volume is 8 m3 and there are six cargo retainers available…

CARGO & PASSENGER Configurations

… Simple transformation for 8 passengers transportation.

PASSENGER Configuration

Emergency exit Passenger seat «Sigma» Helios Wardrobe

ANSAT PASSENGER specialized configuration provides comfortable transportation of 6 persons.

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.

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

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

2 patients and 2 paramedics in HEMS configuration

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,

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

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 Andrey V. +7 (495) 6275545 +7 (915) 3848193 ivancov@rus-helicopters.com

Kiyamov Marat R. +7 (843) 550 0000 kiyamov_mr@kazanhelicopters.com

Let us know you need Ansat

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