Klimov TV7-117

TV7-117

TV7-117SM
Type	turboprop/turboshaft
National origin	Russia
Manufacturer	Klimov
Major applications	Ilyushin Il-112 Ilyushin Il-114 Mil Mi-38

The Klimov TV7-117 is a Russian turboprop engine certified in 1997 to power the Ilyushin Il-114 regional commuter aircraft. The new engine features enhanced reliability, fuel economy and greater service life compared with its predecessors produced in the former Soviet Union. The engine has a modular design. The nine modules can be replaced in the field, which dramatically reduces costs and accelerates repair and maintenance. The engine has an electronic-hydromechanical control system.

The TV7-117S engine has been offered to power the newest Russian turboprop aircraft such as Ilyushin Il-112 and Ilyushin Il-114. In addition, Klimov developed the TV7-117V turboshaft to power rotary-wing aircraft, such as the Mil Mi-38, and marine drives for power high-speed boats and industrial electric power plants. The TV7-117 engine family are produced by Klimov JSC (St. Petersburg), Chernishov JSC (Moscow) and the Baranov JSC (Omsk).

Variants

TV7-117SM (the S stands for the Russian word for aircraft, the M for airliner, as opposed to military cargo aircraft, the version for which is designated ST, with the T being for transport) is the turboprop variant for fixed wing aircraft, that was introduced by Klimov in 2002 featuring a Full Authority Digital Electric Control (FADEC) system based on the BARK-12 or BARK-57 electroniс engine control unit, as well as improved reliability, manufacturability and maintainability. It features an enclosed centrifugal wheel that increases its power by 10% while maintaining all the other performance parameters. The Klimov Company holds a patent for the design and manufacturing of such wheels. This engine is used on the Ilyushin Il-114 and is likely to be used on the new Ilyushin Il-112.

TV7-117V/VM (the V stands for the Russian word for helicopter) is the turboshaft variant for helicopters, a model with the power shaft in front dedicated to the new Mi-38 (VK-3000 family).

TV7-117VK is a version with the power shaft in the rear to upgrade Mi-28 and Ka50/Ka52 helicopters (VK-3000 family).

Applications

Specifications (TV7-117VM)

Data from ^[1]

General characteristics

Type: turboprop/turboshaft
Length: 1,614 mm (63.5 in)
Diameter: 640–820 mm (25–32 in)
Dry weight: 360 kg (790 lb)

Components

Compressor: single shaft axial flow centrifugal compressor, 5 axial + 1 centrifugal stages
Combustors: annular
Turbine: 2-stage axial flow

Performance

Maximum power output: 2800 hp
Overall pressure ratio: 16 (ratio on takeoff)
Fuel consumption: 199 g/hp/hr (takeoff)
Power-to-weight ratio:

References

Notes

↑ Klimov Web Site

External links

Wikimedia Commons has media related to Klimov TV7-117.

Klimov aircraft engines

Piston engines	M-100 M-103 M-105 M-110 M-120 VK-106 VK-107 VK-108 VK-109 VK-110 VK-150

Turbojets	RD-45 VK-3 RD-500

Turbofans	RD-33

Turboprops and turboshafts	GTD-350 TV2-117 TV3-117 TV7-117 VK-800 VK-1500 VK-2500 VK-3000

This article is issued from Wikipedia - version of the Thursday, April 21, 2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.