Document

Report
Мi-38
Utility Helicopter
Mi-38 concept
• Advanced technologies, components, systems and materials have been applied
• Full compliance with aviation regulations AP-29 (Russia), CS-29 и FAR-29
• High cargo capacity, range and fuel efficiency
• Legacy of Mi-17 helicopters
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OVERVIEW
21, 1 m
4,44 m
5,10 m
Ø 3,84 m
25,22 m
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POWER PLANT OPTION
ТV7-117V (KLIMOV)
PW127TS (PRATT & WHITNEY)
Mi-38-2 (Prototype 1)
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Мi-38-1 (Prototype 2)
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CARGO CABIN
1.86 m
7.0 m
8.63 m
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Clamshell/ramp with hydraulic actuator
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1.43 m wide sliding door
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Up to 6,000 kg of cargo (up to 29.9 м3 in
volume carriage) inside the cabin
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Fast loading of wheeled vehicles
2.36 m
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CARGO CABIN
EC-225
S-92
Mi-8
AW-101
Mi-38
Cabin Volume 29.9 m3
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MISSIONS
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Internal/External cargo transportation
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Passenger transportation
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Corporate / VIP
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Offshore
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Search and rescue
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Medevac
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INTERNAL AND EXTERNAL
CARGO TRANSPORTATION
External sling allows transporting up to 7 tons of cargo
Equipment installed:
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system of standard and emergency cargo drop
•
cable inertia reel
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automatic damping of underslung cargo oscillations
7 000 kg
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PASSENGER HELICOPTER
29 passengers + flight attendant
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OFFSHORE
Emergency floatation system
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SAR
FLIR
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VIP/Corporate
 4 VIP seats;
 Table-cabinet with on-board entertainment system
accommodating DVD-player, amplifier
 Two four-seater sofas with seatbelts
 LCDs, acoustic systems
 Additional thermal and acoustic insulation
 Dual-pane windows reducing noise level
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MEDEVAC
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FLIGHT PERFORMANCE
Cruise speed (TOW=14,200 kg)
290 km/h
Max speed (TOW=14,200 kg)
320 km/h
Hover ceiling OGE, ISA (TOW=14,200 kg)
3,510 m
Service ceiling, ISA (TOW=14,200 kg)
Flight range with 3,000 kg of cargo ( Н=500 m, ISA +, 30-min fuel reserve)
Flight range with 5,000 kg of cargo at MTOW (Н=1,000 m, ISA+10°С, 30-min fuel reserve)
Flight range with auxiliary fuel tanks and 2,700 kg of cargo at MTOW (Н=1,000 m, ISA+10°С, 30min fuel reserve)
Number of passengers
MTOW
Max payload:
at the external cargo sling
inside transport cabin
6,000 m
1000 km
490 km
1,350 km
30
15,600 kg
7,000 kg
6,000 kg
Fuel capacity of main fuel tanks (at 0.8 g/cm³ fuel density)
3,160kg (3,955l)
Fuel capacity with auxiliary fuel tanks (at 0.8 g/cm3 fuel density)
3,992 kg (4,990l)
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AIRFRAME AND SYSTEMS
Composite main rotor blades
Titanium MR hub
with elastomeric bearings
Х-shape tail rotor
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SAFETY
anti-icing
protection
of blades
jettisonable
emergency
doors
improved
fuel system
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crashworth
y seats
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AVIONICS
IBKO-38 by TRANSAS includes:
• flight and navigation management
systems
• data control system
• test and control system BSK-38
• radio
• emergency kits
• emergency and reserve indicators
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AVIONICS
IBKO-38 provides control of all radio equipment by two
multifunctional control desks and has pre-flight control of all systems.
IBKO-38 can be connected with different devices:
• Video cameras
• Electronic optical system
• Surveillance system
Databases of IBKO-38 can be regularly updated:
• Navigation database (including regional airlines)
• Landscape database
All databases can be updated by developer through the Internet.
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WHY MI-38?
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Compliance with AP-29, FAR -29, CS-29 standards
Reliability and safety
Low operating costs
On-condition maintenance
Operational range +50ºC÷ -50ºC
Operations in icing conditions
Bearing ratio 3…5 kg/sq.cent
Safe emergency evacuation
Centralized tank fuelling
Helicopter hydro systems of improved reliability
Spacious cargo cabin
Low noise and vibration level
Independent electrics and air conditioning
Energy absorbing landing gear
© 2014 Russian Helicopters, JSC All rights reserved
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MILESTONES
Gate
Research and design
2013
2014
2015
2016
Completed
Prototype OP-1 (TV7-117V engine)
Prototypes, flight tests
Prototype OP-2 (PW 127/5 engine)
Prototype OP-3 (TV7-117V engine)
Prototype OP-4 (TV7-117V engine)
Russian Aviation Authorities
TC
Certification
Contracts/Deliveries
(+6)
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THANK YOU!
© 2014 Russian Helicopters, JSC All rights reserved

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