Mi-38
description
Transcript of Mi-38
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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
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21, 1 m 4,44 m
Ø 3,84 m
25,22 m
5,1
0 m
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Mi-38-2 (Prototype 1) Мi-38-1 (Prototype 2)
ТV7-117V (KLIMOV) PW127TS (PRATT & WHITNEY)
POWER PLANT OPTION
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7.0 m
8.63 m
1.86 m
2.36 m
• Clamshell/ramp with hydraulic actuator
• 1.43 m wide sliding door
• Up to 6,000 kg of cargo (up to 29.9 м3 in
volume carriage) inside the cabin
• Fast loading of wheeled vehicles
CARGO CABIN
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EC-225
S-92
Mi-8
AW-101
Mi-38
Cabin Volume 29.9 m3
CARGO CABIN
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Internal/External cargo transportation
Passenger transportation
Corporate / VIP
Offshore
Search and rescue
Medevac
MISSIONS
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External sling allows transporting up to 7 tons of cargo
Equipment installed:
• system of standard and emergency cargo drop
• cable inertia reel
• automatic damping of underslung cargo oscillations
INTERNAL AND EXTERNAL
CARGO TRANSPORTATION
7 000 kg
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PASSENGER HELICOPTER
29 passengers + flight attendant
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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
VIP/Corporate
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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) 6,000 m
Flight range with 3,000 kg of cargo ( Н=500 m, ISA +, 30-min fuel reserve) 1000 km
Flight range with 5,000 kg of cargo at MTOW (Н=1,000 m, ISA+10°С, 30-min fuel reserve) 490 km
Flight range with auxiliary fuel tanks and 2,700 kg of cargo at MTOW (Н=1,000 m, ISA+10°С, 30-
min fuel reserve) 1,350 km
Number of passengers 30
MTOW 15,600 kg
Max payload:
at the external cargo sling 7,000 kg
inside transport cabin 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)
FLIGHT PERFORMANCE
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Titanium MR hub with elastomeric bearings
Composite main rotor blades
Х-shape tail rotor
AIRFRAME AND SYSTEMS
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SAFETY
improved fuel system
anti-icing protection of blades
crashworthy seats
jettisonable emergency
doors
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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
AVIONICS
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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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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
AVIONICS
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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
WHY MI-38?
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Gate 2013 2014 2015 2016
Research and design Completed
Prototypes, flight tests
Certification
Contracts/Deliveries
Prototype OP-4 (TV7-117V engine)
Prototype OP-3 (TV7-117V engine)
Russian Aviation Authorities
TC
(+6)
Prototype OP-2 (PW 127/5 engine)
Prototype OP-1 (TV7-117V engine)
MILESTONES