Request a Quote 0

TV3-117VM Series 3

turboshaft engine

AvailabilityOut of stock
Availability
Out of stock
Warranty
6 Months
Condition
Repairable
Price on request

Price and lead time are confirmed before payment.

Description

TV3-117VM Series 03 turboshaft engine for civil helicopters

TV3-117VM Series 03 is a turboshaft aircraft engine with a free turbine, designed mainly for civil helicopters of the Mi-8 / Mi-17 family. The engine is a further development of the TV3-117 family and is intended to provide stable power output, fuel efficiency and reliable operation in a wide range of climatic conditions. It is used as part of the helicopter powerplant system and supplies mechanical power to the transmission. The Series 03 modification is especially relevant for helicopters operating in hot climates, high-altitude areas, dusty regions and other demanding environments.

Full descriptionCollapse description

Hot-and-high performance of TV3-117VM Series 03

The TV3-117VM Series 03 is optimized to retain power in hot and high-altitude conditions. Reduced air density and elevated ambient temperature normally reduce engine power margin, especially during takeoff, hover and one-engine-inoperative operation. This modification supports reliable operation on high-altitude landing sites and in hot climates where stable output is required for civil and transport helicopter missions. According to the provided technical data, the engine is capable of starting and stable operation on sites up to approximately 4000 m above sea level, depending on aircraft configuration and operating conditions.

Power modes of the TV3-117VM Series 03 engine

The TV3-117VM Series 03 provides several controlled power regimes for helicopter operation. Takeoff power is used for high-load flight phases, while nominal and cruise regimes support longer operation with controlled fuel consumption. Emergency power is used for abnormal conditions, including one-engine-inoperative situations, when the remaining engine must provide additional output for safe continuation of flight and landing. The use of all power modes must follow the engine and aircraft operating documentation, because power level, duration, gas temperature and environmental limits are controlled parameters.

Construction of TV3-117VM / VMA Series 03

The TV3-117VM / VMA Series 03 engine uses a single-shaft gas generator with a free power turbine. Its main gas path includes a 12-stage axial compressor, annular combustion chamber, two-stage compressor turbine, two-stage free turbine and exhaust unit. The engine also includes an accessory gearbox for installed units that support starting, fuel supply, lubrication, control and monitoring. The free-turbine configuration allows the power turbine to transmit torque to the helicopter transmission while the gas generator operates according to engine control requirements and load conditions.

Accessory equipment and support systems of TV3-117VM Series 03

The TV3-117VM Series 03 includes systems for anti-icing, lubrication and breather operation, fuel supply, automatic control, engine monitoring and starting. Installed accessories may include the NR-3VM fuel pump-regulator, SV-78BA air starter, DCN-70A centrifugal fuel pump, MA-78 oil unit, rotor speed sensor, manual turning mechanism, fuel manifold with 12 injectors, drain valve, compressor bleed valves, ignition unit and SP-26P ignition plugs. These units support stable engine operation during starting, acceleration, steady regimes and shutdown. Actual accessory configuration should be confirmed by engine documentation.

Application and interchangeability of TV3-117VM Series 03

The TV3-117VM Series 03 is intended for Mi-8 / Mi-17 family helicopters, including Mi-8MTV variants, Mi-17, Mi-171 and Mi-172, depending on approved aircraft configuration. The engine may be used on helicopters with single-rotor and coaxial rotor configurations where the applicable documentation permits installation. It supports operation with inlet particle separators and exhaust screening devices, preserving helicopter performance in dusty, smoky and maritime environments. The engine is described as interchangeable with earlier TV3-117 family modifications within approved limits, but exact interchangeability must be confirmed through service bulletins, aircraft records and engine documentation.

Technical details

Product Type
Turboshaft aircraft engine with free turbine
Engine Designation
TV3-117VM Series 03
Alternative Designations
TV3-117VM Series 3, TV3-117VM / VMA Series 3, TV3-117VM seriya 03, TV3-117VM seriya 3
Function
Primary helicopter powerplant for civil and transport helicopters
Application / Where Used
Helicopter powerplant system
All specificationsCollapse specifications
System / Installation Area
Engine installation / helicopter propulsion system
Compatible Aircraft / Equipment
Mi-8MTV, Mi-8MTV-1, Mi-8MTV-2, Mi-8MTV-5, Mi-17, Mi-171, Mi-172 and related Mi-8 / Mi-17 family helicopters
Engine Configuration
Single-shaft gas generator with free power turbine
Rotation Direction, Gas Generator Rotor
Counterclockwise
Rotation Direction, Free Turbine Rotor
Counterclockwise
Compressor Type
Axial
Number of Compressor Stages
12
Combustion Chamber
Annular
Compressor Turbine
Two-stage
Free Turbine
Two-stage
Exhaust Unit
Installed
Accessory Gearbox
Installed
Emergency Power Mode
2200 hp
Takeoff Power
2000 hp
Nominal Power
1700 hp
Cruise Power
1500 hp
Specific Fuel Consumption
0.220 kg/hp·h at takeoff mode
Compressor Pressure Ratio
9.4
Airflow Through Compressor
Not less than 8.7 kg/s
Maximum Gas Temperature Before Turbine
1263 K / 990 °C
High-Altitude Capability
Start and stable operation on sites up to approximately 4000 m above sea level
Power Retention
Maintains rated power in hot and high-altitude conditions
Environmental Resistance
Stable operation in dusty, smoky and maritime environments
Compatibility with IPS and Exhaust Devices
Supported
Length with Exhaust Pipe
2055 mm
Width
660 mm
Height
728 mm
Dry Weight
294–295 kg
Fuel Control Unit
NR-3VM pump-regulator
Air Starter
SV-78BA
Fuel Pump
DCN-70A centrifugal fuel pump
Oil Unit
MA-78 oil unit
Ignition Equipment
Ignition unit, including SK-22-2K type where applicable, and two SP-26P ignition plugs
Compressor Bleed Valves
Installed
Manual Turning Mechanism
Installed
Interchangeability
Interchangeable with earlier TV3-117 family modifications within approved limits
Maintenance
High maintainability and repairability
Time Between Overhaul
1500 h
Assigned Service Life
Up to 3000–7500 h, depending on production year and applicable service bulletins
Technical Documentation
Technical and operational documentation, passport, engine logbook, service bulletins and maintenance records, if available

Payment & delivery

Orders ship from our hub in Dubai. Partner stock is first transferred to Dubai, then shipped to you.

Dubai stock: 100% before dispatch. Partner stock (Remote stock) and Pre-order: 50% advance payment to start the order and 50% before shipment from Dubai to you.

Availability, lead time, delivery cost and payment terms are confirmed for your order before payment.

Payment & delivery terms

Questions about this part?

Send your requirements — we’ll clarify the details for your order.

Share this part

TV3-117VM Series 3