«ANSAT Helicopter»

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

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

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

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

seats Fisher
Two jettisonable doors
Traditional controls
Windscreen wipers

for one pilot (basic variant)

(basic variant)

for two pilots

Все права защищены

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

– 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

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

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.

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

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

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

– 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

- U

towing, containment, tie-down, transport
Lift facilities
Assembly access facilities
Assembly-dismantling facilities

Ground support facilities

facilities of the systems and units
Helicopter protection facilities on the ground
Helicopter support tool
Power source

Ground support facilities

Structure

Flight-navigation simulator

Ground based complex of training

Training simulator

Training computer class

Visual laboratory resources

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 computer class

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

exercises
Registration Action trainee for analysis

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

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

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

PASSENGER
PASSENGER
EXECUTIVE
SEARCH & RESCUE
MEDEVAC
SCAUT

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

CARGO & PASSENGER Configurations

… Simple transformation for 8 passengers transportation.

seat «Sigma» Helios
Wardrobe

ANSAT PASSENGER specialized configuration provides
comfortable transportation
of 6 persons.

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.

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

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

ОАО "Вертолеты России". Все права защищены

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,

– 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

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