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Russian engine company UEC Clemor has
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developed the VK 650V, a contemporary
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turbos shaft engine that has been
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expressly engineered for light
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helicopters with a takeoff weight of up
0:16
The first demonstrator engine was
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assembled within 6 months, a remarkable
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feat of engineering efficiency following
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the project's inception in the third
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During the subsequent 5 years, the
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development team conducted a rigorous
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cycle of endurance testing and
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engineering, which culminated in the
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engine receiving its type certificate in
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The demand for domestically produced
0:41
power plants of this class was
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substantially increased by the urgent
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need to replace imported engines as a
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result of Western sanctions and the
0:49
withdrawal of foreign suppliers, which
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drove this rapid development.
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The VK 650V will be fine-tuned and the
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first flights of three helicopter
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equipped with this new engine will
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initiate in the current year. According
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to Yukimov's press service, the VK 650V
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is anticipated to enhance the efficacy
1:14
and reliability of these helicopters
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which are essential to Russia's light
1:20
The VK 650VS design is based on
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cuttingedge digital engineering
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technologies such as additive
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manufacturing, 3D modeling, and digital
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Components manufactured through 3D
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printing comprise approximately 12% of
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the engine's mass, particularly in
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critical parts like the turbine and
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combustion chamber. This method not only
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expedites the development process but
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also improves the precision and quality
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of the final product. Engineers were
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able to reduce the engine's weight to
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105 to 115 kg while maintaining the
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engine's long-term durability and
2:00
strength through the implementation of
2:02
advanced heatresistant alloys and a
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modular construction philosophy.
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The VK 650VS dual channel digital full
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authority digital engine control system
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is a critical feature that enhances
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operational reliability and provides
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highly accurate parameter control. The
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engine is capable of producing 650
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horsepower during launch and up to 750
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horsepower in emergency mode which can
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be maintained for a maximum of 2.5
2:30
minutes. The VK 650V is positioned as a
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direct replacement for foreign engines,
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particularly the Pratt and Whitney
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which previously powered the ANSAT and
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helicopters based on these performance
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figures. The Russian engine not only
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matches, but in some instances surpasses
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the launch power and specific
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performance characteristics of its
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Western counterparts.
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The VK 650VS attraction to helicopter
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manufacturers and operators is further
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enhanced by its high powertoweight ratio
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and closed loop autonomous oil system.
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The engine's modular design enables easy
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adaptation to various aircraft classes
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such as both manned and unmanned aerial
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vehicles. It is designed to operate
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consistently in a broad range of
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temperatures from as low as -55°
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centigrade to as high as plus 60°
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centigrade and at altitudes of up to
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7,000 m rendering it suitable for
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various geographical and climatic
3:36
The VK 650V project's assimilation into
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hybrid power plants is one of its most
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innovative features. UEC Cleorf has
3:45
already created a hybrid propulsion
3:47
system that integrates a conventional
3:49
gas turbine engine with electric motors
3:51
and batteries using the VK 650V.
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This composite system has been showcased
3:58
at numerous aviation and helicopter
4:00
exhibitions and is considered a
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promising solution for advanced
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aircraft, air taxes, and next generation
4:08
The hybrid demonstrator is intended to
4:10
considerably broaden the potential
4:12
applications of the VK 650V engine
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family by generating up to 500 kW of
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Chinese MMP, CIAM, and VIAM collaborated
4:26
extensively to develop and manufacture
4:31
These organizations ensure a
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comprehensive and integrated approach to
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the project by contributing to the
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engine's design, manufacturing, and
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testing. The use of additive
4:41
manufacturing is particularly noteworthy
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as VIM provides 3D printed components,
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including turbine nozzles and transition
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ducts, and UECO implements welding and
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brazing technologies for additive parts.
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Certification of the VK 650V was
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accomplished in an unprecedented amount
5:00
of time from the inception of the
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project to type approval in a mere 5
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years. The engine was initially verified
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with a takeoff power rating of 545
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horsepower with the intention of
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increasing this to the design target of
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650 horsepower after undergoing
5:18
additional certification tests. The free
5:20
turbine shaft's initial time before
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overhaul is set at just under 75 hours,
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while other main components are subject
5:28
to a life limit of 100 cycles.
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These figures are anticipated to
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substantially increase over time with
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future objectives of 4,500 hours or
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3,000 cycles for hot section parts and
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up to 9,000 hours or 6,000 cycles for
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The VK 650V is designed to be the
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standard engine for a new generation of
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light Russian helicopters such as the
5:59
It is also being considered for export
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and for installation on foreign
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helicopters including Iran's Saba 248,
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China's Chanhar Z11, and the Shard 285.
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The VK 650V is currently being assessed
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for potential use in unmanned aerial
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vehicles and training aircraft such as
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the Yak 152 in addition to its
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application in helicopters.
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The engine is a critical component of
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Russia's endeavors to establish
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technological independence in the
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aerospace sector and to effectively
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compete in the global aviation market
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due to its adaptability and
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sophisticated features.
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The VK 650V based engine family is
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anticipated to expand in the future with
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the introduction of hybrid and electric
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modifications that are specifically
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designed for various aircraft classes.
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The ongoing development and refinement
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of the VK 650V and its derivatives are
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indicative of Russia's dedication to the
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advancement of its domestic aerospace
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industry and the reduction of its
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dependence on foreign technology.
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Now, do you think the Russians have now
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mastered the art of creating aircraft
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engines in short notice, even if they
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are a bit less efficient than their
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Western counterparts?
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Let us know in the comments. Please feel
7:19
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