vektor ng rus presentation

© 2012 Evektor spol. s r.o. | All rights reserved www.evektor.cz © 2012 Evektor spol. s r.o. | All rights reserved www.evektor.cz

23.8.2012

INNOVATIVE Approach to Aircraft Design

© 2012 Evektor spol. s r.o. | All rights reserved www.evektor.cz

Presentation Contents

1.Fundaments Background of Needs in Transportation and Use of Air

Transport

2.Key Challenges

3.Market Requirements for the Local Aviation Aircraft

4.Solution Suggested by the Evektor Company for the Russian Market

5.Broad Application and Operation Possibilities

6.EV-55 Outback – Key Figures

7.Unique Character of Design

8.Evektor Company Activities in Russia


●1.0 Needs in Transportation and Use of Air Transport

Connections with towns situated far from

local centres which are hard to reach by

ground within a reasonable time

Charter and regular flights

Medical emergency

Rescue missions

Supply under natural accidents (floods,

earthquakes)

Fire-preventing jobs and monitoring

Border control


2.0 Objective Reality and Challenges Faced by Russia

Lack of developed ground infrastructure

Limited number of airports

Unpaved runways

Short runways

Airports without aviation fuels reserves

Lack of navigational facilities

Operations in severe meteorological conditions


Multi-purpose aircraft

Aircraft price is below 2.5 million US Dollars

Launching serial manufacturing in Russia with further localization

Two-engine aircraft

Robust metal frame

Possibility to operate in a wide range of meteorological conditions

Safety

Robustness

Efficiency

Availability

Type of runway: unpaved surface, including low density

Short take-off/landing distance

Single pilot control

Easy and inexpensive service

Modern avionics (glass cockpit)

Engines on jet fuel

9 – 14 passengers or 1800 kg of cargo

Maximum range is 2000 km

Cruise speed 400 km/h

Operating cost less than 800 US Dollars (including depreciation)

3.0 Requirements for Domestic Aviation Aircraft


4.0 Proposed Solution:

EV-55 Outback

The only two-engine turboprop aircraft on today’s

market

Multi-purpose aircraft for carrying passengers or

cargo (9 – 14 passengers or up 1,724 kg of cargo)

Unique aircraft – operating with unpaved runways,

short take-off/landing (take-off distance is 373 m under

standard conditions)

Good power-to-weight ratio – two PT-6A-21 engines

(536 h.p. each)

Fast aircraft – cruise speed 408 km/h

Cost-saving aircraft – low operational cost below 800

USD

Affordable aircraft – base price is $2.1-2.2 M

Easy maintenance without overhauls

Sufficient life time i30,000 flight hours

TBO 3,600 flight hours

EASA CS-23/ FAA FAR Part 23 certification


5.0 EV-55 Outback:

Multi-purpose Aircraft

The variant for transportation of 9 – 14 passengers

The base interior version is ready

Transportation of 9 passengers to the distance of up to 1400 km

Maximum comfort for passengers

Sufficient volume over the heads of the passengers

Comfortable seats with the interval of 84 cm

Baggage compartment with the volume of 3.2 cu. m

Up to 38 kg of luggage per passenger

Cargo variant

Big main deck with the size of 5.02 x 1.61 x 1.37 m, and the volume of 9.47 cu. m

Transportation of 1,451 kg to the distance of up to 750 km

Transportation of cargo in standard containers

Distribution of cargo into small sections using nets

Combined version for 3 – 5 passengers and cargo


6.0 EV-55 Outback:

Key Figures

Effective trailing-edge flaps Weather radar antenna

Modern glass board

Effective anti-icing system

Solid chassis with big wheels Centralized filler point

Spacious luggage deck

Front luggage deck

Crew doors

Wide passenger and cargo door (port)

Turboprop engines

Big and effective rudder Spacious passenger/cargo cabin (9.47 cu. m)


7.1 EV-55 Outback: Frame Design – Everything for

the Comfort of Passengers and Uplift

Front luggage deck

Flight deck Passenger or cargo deck

Rear luggage deck

The basis of frame is made of aluminum alloys, all the doors and cowlings are made of composites

Corrosion prevention with the life time of 30,000 flight hours or 30 years

Easiness of service and inspection (no intermediate overhaul)

Sufficient volume for passengers and cargo or luggage:

Big main deck volume: 9.47 cu. m

Volume of rear luggage deck: 2.7 cu. m

Volume of front luggage deck: 0.5 cu. m

The door cut is only 0.8 m over the ground level for the cargo loading convenience

The dimensions of the cargo door: 1,.5 m in width and 1.37 m in height


7.2 EV-55 Outback:

Wing – Unique Design

High lift force coefficient in the take-off and landing

configuration (effective and aerodynamically optimized

trailing-edge flaps)

Low drag force at the cruise speed

Excellent stall characteristics

Integrated fuel tank (1,930 l)

Big ailerons – controllability at low speeds

Single metal centre-section

Flap

Aileron


7.3 EV-55 Outback:

Tail

Stability and controllability (engine

shutdown, crosswind) at all operation

conditions, including icing

Low drag at the cruise speed

Sufficient reserve in lift power in the icing

conditions

Anti-damage protection during take-off and

landing at unpaved airfields

Aerodynamically optimized in the air tunnel

All-metal construction


7.4 EV-55 Outback:

Chassis

Big wheels of main landing gear – possibility of operation on

unpaved runways

Gears are controlled by an effective and reliable

high-pressure hydraulic system

Hydraulic servos are equipped with an internal locking system

Hydraulically controlled nose leg

ABS for shortening the landing distance

Main landing gear:

Parker 30-244B brakes

Tyre pessure: 55 + 3 PSI

Wheel size: 8.50-10" Parker 40-424В

Nose gear:

Wheel size 5.00-5" Parker 40-77H

Pressure: 54 + 3 PSI

Traverse gear

•by footplates - +- 5

•by the stick +- 50

Ground density for take-off and landing (comparison of EV-55 and L-410)

0

200

400

600

800

1000

0

1

2

3

4

5

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8

9

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0 1 2 3 4 5 6 7 8 9 10 11

Gro

un

d d

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sity

, kP

а

Gro

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d d

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sity

, кg/

sq.

cm

Track depth, cm

L-410M

EV-55


7.5 EV-55 Outback:

Hydraulic System

Electrohydraulic aggregates

Accumulators

Actuators

Conduit pipes

Effective high-pressure hydraulic system (21 MPa)

Principal and emergency sysytem

The hydraulic system supplies:

gear actuation

wheel brakes

nose landing gear steering control

flap extension and retraction

The electrohydraulic aggregates are without

hydraulic pumps, located on the engines

Electrohydraulic aggregates, accumulators and

distribution slides are situated in the frame nose –

convenient and easy service


7.6 EV-55 Outback:

Anti-icing System

Designed for flights in the known icing

conditions

A reputable reliable system of rubber boots

Leading edges of the wing and tail are

covered with rubber boots

Propeller blades and windows are electrically

heated

Automatic anti-icing system operating –

decrease of burden of the pilot

Engine air inlet is equipped with an

electromechanical separator

Cooler

Pressure Regulator Valve

De-ice Distributors Valves

Vertical Stabilizer De-ice Boot

Pressure Switch

Electronic Timer and Control Unit


7.7 EV-55 Outback:

Modern Avionics

Smart Deck by CMC Electronics company

is configured for single pilot operations

2 primary displays + 1 multifunctional +

central console

Fully integrated with all the aircratf systems

– engine monitoring system, quality and

consumption of fuel, fuel pressure, hydraulic

system…

Digital autopilot

GPS, NAV/LOC/GS, DME, ADF receivers

VHF and HF tranascievers

Radio altimeter

Weather radar

TAWS

TAS

Satellite weather receiver

Synthetic vision system


7.8 EV-55 Outback:

Technical Data

Dimensions

Weights

Characteristics

Length 14,35 m

Wingspan 16,10 m

Height 4,66 m

Operation empty 2,626 kg

Maximum takeoff 4,600 kg

Maximum fuel 1,656 kg

Maximum payload 1,824 kg

Speed 220 to 408 km/h

Flight range up to 2,200 km (max. project)

Take-off distance 420 m

Landing distance 510 m

Fuel consumption 200 kg/h or less


7.9 EV-55 Outback:

Flight Range

Flight range with 9 passengers Maximum flight range

2250 km

1400 km Ulyanovsk

Ulyanovsk


8.0 Collaboration with Russia:

Joint Venture with the Vektor NG Rus Company

The company management undertakes the following steps within the

framework of expanding the Evektor Group of Companies presence on the

territory of the Russian Federation and the CIS countries:

The status of OOO Vektor NG Rus as the authorized strategic partner in implementing and using

the Evektor company technological products on the territory of the Russian Federation and the CIS

countries has been officially confirmed;

A complex plan on facilitating local airlines development on the territory of the Russian Federation

using the technical and the intellectual potential of the Evektor company is being carried out

together with the Russian partner;

The long-term Group of Companies development strategy is developed together with the Russian

partner, taking into consideration the Russian small aviation market and local airlines development

needs.

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