Skt presentation

http://skthelicopters.ch

http://skthelicopters.ch/

http://skthelicopters.ch/

Propriatory of SKT / GP July 15 2

Contents

Legacy (Swiss Made / Italian Power - State of the Art Technologies

Mission and Utilization Skyrider Specifications / dimensions Technical descriptions

- Airframe, - Rotor System, - Drive System, - Power Plant - Cooling System, - Flight Controls, - Governor - Fuel System, - Electrical System, - Lighting System, Static System

Multi Function Displays (MFD) Pilot License Requirements Certification of the SKT 06 Skyrider Utilization

- Agriculture Spray Kit, - Float Configuration - FLIR, - ARATOS Swiss Border Monitoring and Security - Cargo Hook R22

YouTube channels and links


LEGACY By leveraging several decades of aeronautical experience, SKT’s

team has refined light helicopter technology to unmatched levels of simplicity, safety and performance.

State of the art technologies, harmoniously combined in a novel architecture bring a breakthrough in light helicopter operation and cheaper operating cost.

The SKT organization is headquartered in Stabio - Switzerland, while the test flights of each helicopter take place a short distance away at Ambri - Airport and in Lomazzo, near Lake Como - Italy.

Experienced test pilots with thousands of hours of flying, perform accurate tests on the helicopters, prior to delivery to Customers.


100 % SWISS MADE

The production facility is located in Stabio - Switzerland. Highly specialized technicians assemble the helicopters with parts manufactured by companies, which are all part of the SKT Helicopter group. Everything except the engines are produced in house at SKT. Final Assembly is processed under thorough supervision and controlled system.

ITALIAN POWER

The MW engine incorporates the latest in modern aviation technology and is produced based on the electronic management functions and specific performance needs of the SKT helicopter. Hours of test led to a very positive result on safety in flight.


State of the Art Technologies

A group of experts in the field of helicopter aviation engineered a new light helicopter different from some of the famed but now out-dated

Pilots brought their own precise ideas how the new helicopter should perform: simple and fluid in flying, solid and durable, with advanced air penetration, but not only a 'race car'. They wanted a helicopter perfect for recreation, but with possible applications in reconnaissance, fire control, instruction, rescue, aerial photography and observation

The technicians brought forth: the rotor drive belts, improved collective and cyclic movements and their respective controls. Engineers desired a fast, powerful aircraft, but with low power/fuel consumption while using high octane automotive gas, reducing the need for avgas


State of the Art Technologies, cont.

For better flying conditions, the rotor system incorporates a three blade system with specific characteristics. The person responsible for this delicate area, was a technician/engineer and at the same time, a true artist who has shaped and made the blades. He has achieved the best results by giving a ”hook in the sky” blade that makes this helicopter unique.

The design engineers created a new shape that could be only be made composing specific techniques using of composites, carbon fiber and to simulate their behavior in the wind tunnels.

All of these factors have created a magical alchemy, using the latest 3D technologies and machinery. The result is this world class helicopter that has now been flying since early 2013 and is called the SKT SKYRIDER.

Propriatory of SKT July 15 7

Mission and utilization SAR, Search and Rescue

As search could be a very low cost support to find missing people or boats

On board gargo hook R22, max payload 150Kg

FLIR, Forward Looking Infrared Camera

ARATOS Swiss, PROVISTA-300AO Border Monitoring and Security

Floats, application for fishing boats

Pilots training

Lasure flights

Guarantee for utilization, SKT garantees an utilization or availability of 80 % (8 of 10 helicopters in service at all time)

Warranty and maintenance schedule (airframe, engine, gearbox, Rotors, Accessories, Instrumentation), SKT: 2 years or 300 hours TT, whatever comes first


SKYRIDER SPECIFICATIONS • Takeoff or take off max weight: Kg 550 (AECi Reg. 495) • Main Rotor 3 Composite Blades • MW Flat 4 cylinder engine 155 Bhp • RoC Rate of Climb: 7,5m/s • HIGE 2260m/7000ft • HOGE 1550m/5100Ft • Service ceiling 3000m /10000Ft • Fuel: MO GAS gasoline 95 Oct • Consumption: 18/22 Litre per Hour • Fuel Tank 65 Lt (long range: 100 L) • Endurance 3 Hours (long range: 5 h) • Limit Temp.- OAT LIMIT 40 Degrees • VNE 200 Km/h ISA Conditions • Cruise Speed 160 Km/h • Economy Speed 85 Km/h


SKYRIDER EXTERNAL DIMENSIONS AND TECHNICAL IMAGES


Technical description Airframe

The SKYRIDER is a two-seat, single engine, single main rotor helicopter. Constructed primarily of metal and carbon, equipped with skid type landing gear

The primary structure of the fuselage is composed in carbon and the airframe in tubular pressurized steel. Above the pilot’s pedal bar is a barometric pressure indicator installed that indicates the pressure of the airframe tubing. Any drop in pressure would lead to a leakage in the airframe tubing due to possible fracture or cracks.

A cowl door on the right side provides access to the main rotor gearbox, drive system, engine and oil

The battery is place between (underneath) instrument panel


Technical description Rotor System

The main rotor has three composite

symmetrical blades mounted to the

hub by fully articulated hinges

covered by carbon coverage

Droop stops for the main rotor

blades provide a teeter hinge

friction restraint which normally

prevents the rotor from teetering

while stopping or starting

Tail rotor has two composite blade

MAIN ROTOR MAST AND SWASHPLATE


Technical description Drive System

A gears group is bolted directly to the engine output shaft.

These gears transmit power to the gearbox of main and tail

rotor. The main gearbox contains a single-stage spiral-bevel

gear set which is splash lubricated. The gears function as

freewheel when engine shutdown during flight

The long tail rotor drive shaft has one hanger bearing and

the Tail cone is a monolithic carbon tube

The tail gearbox contains a splash-lubricated spiral-bevel

gear set


Technical description Power Plant

MW aero power B25R four cylinders, horizontally opposed, water cooled, ignition valve with a wet sump oil system powers the helicopter. Engine has two alternator, first mounted between transmission gear and gearbox, second installed directly onto the engine.

Aero Power engines are an extraordinary expression of Italian style and technology. The engines are impressive, not only for the high technology content but also for beauty, for the accuracy of the details and for sleek design, result of a complete project.

@ 50% load


MW aero power B25R

Technical description Power Plant


Technical description Cooling System

Two cooling fans are mounted over the airframe for cooling

the radiator, behind this there is an electrical pump for water

supply

ENGINE DRIVEN FAN FOR WATER COOLING


Technical description Flight Controls

Dual controls are standard equipment and all primary control are actuated through cables. Dual cyclic and collective are removable, whereas pedals remain fixed

The collective stick is conventional with a twist grip throttle control

Flight controls have no friction with the exception of collective, which includes a magnetic break that allows moving the lever only by clicking the button disposed under the collective. When the pilot releases the button, the collective maintain in the last position.


Technical description Governor

The governor maintains engine RPM by sensing changes and applying corrective throttle inputs which may be easily overridden by the pilot

The governor is designed to assist in controlling RPM under normal condition. I will not prevent over or under-speed conditions generated by aggressive flight manoeuvres.

When operating at high density altitudes, governor response rate may be too slow to prevent over speed during gusts, pull-ups, or when lowering collective


Technical description Fuel System

The fuel system is configured with two electrical pumps connected to the main fuel tank. The dual pump configuration was designed for safety purposed in case of pump failure.

The fuel gages are electrically operated by float-type transmitters in the tank. When the gages read E, the tanks are empty


Technical description Electrical System

A 12 volt electrical system consists of two alternator, voltage controller, battery relay a capacitor and two batteries

First alternator (engine alternator) and load battery 1 dispense electrical requirement to engine, EFIS and light

Second alternator (located between main gearbox and transmission gear) dispense electrical requirement to fuel pumps, water pumps, pre-starter and radiator fan

If alternator discharges, terminate flight as soon as practical.


Technical description Lighting System

An anti-collision strobe light is installed on the radiator fan. Night lights include navigation lights on each side of the cabin and on the tail. Twin landing lights are installed in the nose at different vertical angles to increase the pilot’s field of vision.

Technical description Static System

The Pitot-static system supplies air pressure to operate the airspeed indicator, altimeter and vertical speed indicator. The Pitot tube is located on the front edge of the helicopter. The static source is located in the control panel.


Multi Function Displays (MFD)



Page 1, Artificial Horizon



Page 2, engine, fuel, water & time scale



Page 3, split panel artificial horizon / engine scales



Page 4, senosor indications


Pilot License requirements

Theoretical training including aerodynamics, navigability, radio and communication, human factors form the minimum requirement for student pilots prior commencing practical flying training.

Medical examination, fit to fly

Skill Test

Minimum age

What are the requirement/regulations to fly a light helicopter Every Country introduce the Helicopters in National Category (FAR23 / FAR27 / Restricted / Experimental / ULM)

An applicant for a pilot licence, shall demonstrate a level of knowledge appropriate to the privileges of the licence by passing theoretical knowledge examinations in accordance with the requirements set out in National Licences Office

The student pilot should read and understand the content of the POH in all parts and to get familiarized with essential limitations, performance data, procedures, checks, etc prior getting on board for flight.

SKT provide basic practical training (type rating) for SKT 06 helicopters


Certification of the SKT 06

The SKT 06 Helicoper, category VLR (Very Light Rotorcraft) is not yet certified by EASA. The process is on-going but will take 18 months (end 2016)

The SKT 06 will be certified by Transport Canada within one month (August 2015)

EASA Certification specifications for very light rotorcraft (« CS-VLR »)

This airworthiness code is applicable to very light rotorcraft (helicopters) with maximum certified take-off weights not exceeding 600 kg which:

(a) Are of a simple design.

(b) Are designed to carry not more than two occupants.

(c) Are not powered by turbine and/or rocket engines.

(d) Are restricted to VFR day operations.


Agriculture Spray Kit


Float configuration


Forward Looking Infrared Camera; FLIR


PROVISTA-300AO Border Monitoring and Security

• Remotely Piloted Aircraft Systems - Small Target Detection • Mapping and Aerial Surveillance • Activity Control System • Patrol and Checkpoint Security • Cameras - CCTV/Thermal and Laser Illuminator

• ARATOS-SWISS Homeland Security AG is highly specialized in the security sector.

• Provide optimal turn key solutions to address the risks and challenges of our complex environment.

• Focused particularly on perimeter monitoring of border, critical infrastructure and pipelines


Cargo Hook R22


SKT YOUTUBE CHANNEL https://www.youtube.com/channel/UCguR9MWcyYFSfcNX2K2sP_Q/videos

SKT YOUTUBE LINKS https://www.youtube.com/watch?v=tJLUMGNe--4 https://www.youtube.com/watch?v=TqFn31pWlxA&list=UUguR9MWcyYFSfcNX2K2sP_Q https://www.youtube.com/watch?v=zl-CezCnytw&list=UUguR9MWcyYFSfcNX2K2sP_Q https://www.youtube.com/watch?v=9HnPQkiCO3I&list=UUguR9MWcyYFSfcNX2K2sP_Q https://www.youtube.com/watch?v=4qTK_ufF5C0&list=UUguR9MWcyYFSfcNX2K2sP_Q https://www.youtube.com/watch?v=CzXk2NRPXGM&list=UUguR9MWcyYFSfcNX2K2sP_Q https://www.youtube.com/watch?v=GSvYrESxVNo&list=UUguR9MWcyYFSfcNX2K2sP_Q https://www.youtube.com/watch?v=--TGaliE8t0&list=UUguR9MWcyYFSfcNX2K2sP_Q

https://www.youtube.com/channel/UCguR9MWcyYFSfcNX2K2sP_Q/videos







https://www.youtube.com/watch?v=tJLUMGNe--4



https://www.youtube.com/watch?v=TqFn31pWlxA&list=UUguR9MWcyYFSfcNX2K2sP_Q











https://www.youtube.com/watch?v=zl-CezCnytw&list=UUguR9MWcyYFSfcNX2K2sP_Q











https://www.youtube.com/watch?v=9HnPQkiCO3I&list=UUguR9MWcyYFSfcNX2K2sP_Q













https://www.youtube.com/watch?v=4qTK_ufF5C0&list=UUguR9MWcyYFSfcNX2K2sP_Q















https://www.youtube.com/watch?v=CzXk2NRPXGM&list=UUguR9MWcyYFSfcNX2K2sP_Q











https://www.youtube.com/watch?v=GSvYrESxVNo&list=UUguR9MWcyYFSfcNX2K2sP_Q









https://www.youtube.com/watch?v=--TGaliE8t0&list=UUguR9MWcyYFSfcNX2K2sP_Q















CONTACT: Aldo Dinelli , (Marketing Manager) Phone: +41 91 630 92 75 Mobile : +39 335 690 74 15 [email protected]

SKT Swiss Kopter Technology SA Via Santa Margherita, 33 6855 Stabio - Switzerland http://skthelicopters.ch

FRANZ KUNG Representative Middle East, ASIA 38/3 Moo 1, Si Prachan , 72140, Thailand Mobile: +66 92 427 4640, Email: [email protected]

SKT Helicopters reserves all rights to modify this presentation

All Images are illustrative only

July 15 35 Propriatory of SKT / GP

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