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Kamov Ka 62 for sale

Kamov Ka 62 for sale

In the beginning of 90-ies was a sad situation throughout the country, which, in turn, has led to a lack of funding to various normalized economic potential of the industry. In accordance with the OKB Kamov n. starts development of new civil helicopters-60 under the category of Ka-62. In 1990, the project was headed by lead designer Furman V.a. and Deputy Head of the Department on the question of technical projects Gubarev B. You can find Kamov Ka 62 for sale offers below. Kamov Ka 62 prices you can get by contacting our specialists. Average Kamov Ka 62 price – $15,500,000

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Kamov Ka 62 specifications:

ModificationKa-62
Main rotor diameter, m13.5.
Length, m13.25
Height, m4.1
Mass, kg
blank3730
Max takeoff6250
Engine typeGTD 2 Rd-600
Power, kW2 x 955
Maximum speed, km/h300
Cruising speed, km/h260
Combat range, km720
Rate of climb, m/min702
Service ceiling, m5000
Crew, pers1-2
Payload:16 passengers and 2500 kg of cargo

More information about Kamov Ka 62

Kamov Ka 62 for sale

Ka-62 was built on the model of the Kamov Ka-60, the Interior of the fuselage which was implemented for passenger and freight versions. Cabin transport type is up to 6 m2accommodates about ten passengers in economy class and six in VIP-class. Also, the helicopter is capable of carrying cargo weighing 450 kg in the mechanized order. The layout of this helicopter demonstrated the first international aviation show in the territory of the USSR.

Kamov Ka 32 prices about 15 500 000 USD.

In the cockpit at Ka-62 was attended by innovative cushioning seat and dashboard, and it is based for the first time in the Russian vertoletostroenii used liquid crystal display. It created the authors NIIAO not without participation Gubareva b. and Krygina in.

Virtually the entire period of 90-ies employees actively demonstrate new helicopter DESIGN BUREAU on all air shows for buyers search capabilities. Parallel negotiations are underway with European firms and companies on possible joint production of helicopters deployed. Ka-62 is the first air machine from OJSC “Kamov” type of helicopter, designed for single-schema, and is located in the vertical tail rotor feathering. First of all the main slope helicopter did at cruising speed, reducing fuel consumption and increase the weight return.

Thanks to the cooperation with TSAGI, conducted jointly by the theoretical and experimental investigations managed to reduce aerodynamic drag. It is also now possible to use the updated profiles and improvement of blades configuration solve the problem of increasing propulsion and relative efficiency. TSAGI Design Bureau and together could reach the maximum aerodynamic equivalent quality.

Tail rotor mnogolopastnyj. Glider and the rotor blades at 60% are made of composite plastic materials. Glider stands out as perfect charcoal trëhstročnym chassis with the presence of a tail supports and inspires transport-passenger cabin. Powerplant provided engines modular design (the new generation), developed in the Rybinsk Design Bureau motor. Unlike the basic military model, the civil Ka-62 has a great cruising speed, transport performance, fuel efficiency and wide door openings in transport cabin on both sides.

Thanks to the large fuselage helicopter can be used for civilian traffic with comfort and for transportation of cargo, which can be placed inside and outside the sling. High speed allows you to operate the helicopter when emergency medical assistance or emergency situations. Ka-62 can be used as a patrol helicopter or ice intelligence apparatus.

As originally planned, the DESIGN BUREAU staff to promote the helicopter in other countries, its design was carried out taking into account the international requirements of safe flights. In the event of an accident with a power unit planting is possible and with one engine. If committed rough landing, an energy-absorbing seats and chassis design will ensure safety for the pilot and crew. Additionally protected steering screw the keel. Among other things, a helicopter equipped with fire protection and de-icing systems.

An additional plus of the helicopter is that it can be equipped as for flights in normal conditions, weather permitting, and special set for flights in complex and night flight. If necessary and in the helicopter jonica engines may be foreign.

Aviamašin at the exhibition HeliRussia-2012 presented layout Ka-62 with an updated design of the helicopter. The appearance and layout preserved, and chassis and powerplant changed completely. The Russian Turbo-abundant engine Rd-600 was replaced by the French TurbomecaArdiden 3 g. From Austria will be supplied transmission and gearbox. Production of the new helicopter is scheduled to begin at two plants: AAK “progress” and OJSC “Kumapp”. The first would be responsible for the Assembly of the whole structure, and the second for the creation and development of steering and bearing screws. Over-development manages Arsenevskij helicopter plant.

After tests carried out in 2013, the year it was decided to carry out a number of revisions. Certification will be held not earlier than the year 2015. The military sample Ka-62 flew the first prototype flight in March 2014 years. In July were delivered by Transas first three integrated pilot-navigating complex of the CCD-62 for op-1 and op-2. At the beginning of the year 2016 first delivery of helicopters is planned to export.

The design of Ka-62

Single-rotor helicopter, with two GTD and the presence of trëhparnogo chassis. Different mass application of KM (50% by weight of the whole structure). The fuselage of the helicopter is characterized by excellent aerodynamic profile. Metal frame with longitudinal beams and frames. Cladding consists of laminated panels of km and carbon. In turn, the fuselage is divided into four sections: the cockpit, passenger compartment, tail boom with vertical and horizontal opereniâmi. Crew specially convenient osteklili and implanted power lamp set of KM. Doors open outwards. The pilot’s seat is located on the right side of the cab in order to avoid duplication of controls.

Passenger/cargo cabin dimensions constitute 3.3 x 1.75 x 1.3 m with the presence of large doors. Tail boom is section èllipsovidnoe, which installed the stabilizer of the unmanaged type. Its wingspan is 3 meters. In a beam installed vertical with General plumage concealed screws. Kiel is mounted above it with an asymmetrical profile.

Tricycle landing gear landing gear retracted, a samoorientiruûŝaâsâ tail bearing with double wheels. Retracted into the tail boom. Supports working on lever type with nitrogen-oil shock absorbers, which are cleaned in the side and in front of the fuselage. In some versions it is possible to install ballonetov.

Main screw četyrëhlopastnyj, fixing elastic blades. Chassis bushings created from steklougleplastika. He raz″ëmnyj, and the sleeve is composed of self-lubricated bearings Vertical joints, torsionov of steel plates and elastic elements made of fiberglass. All-composite blades form a rectangle with the wake of the ending. Spar is presented in the form of a double-toe profile, along which lies a rubber coating (deicing system). Blade chord-0.53 m.

The composition of the powerplant comprises two GTD Rd-600 (takeoff power-955 kW, cruising capacity is 735 kW). Well thought out emergency power mode. Engines are, in General, are located above the air intakes Fairing fairing. They are also equipped with deicing air system. For adjustment and full redundancy of the engine meets the digital electronic system. Versions of compressor, annular combustion chamber and the turbine drive combines module generator. Free and drive two-stage turbine. The launch is carried out by means of supplementary installation of AI-9.

Fuel system-capacity 1100 litres, divided into four soft tank. They are at the bottom of the cabin with connected oil pumps. Transmission consists of two-stage main gearbox and tail single-phase. Hydraulic steering transmission control system together with hard rods merged in a common block and includes loading mechanisms. A part of the hydraulic system includes two autonomous subsystems. The first is responsible for recharge control surface actuators and the second regulates the system of cleaning the wheels. Down to the beginning of the 1990s known negative situation in the country caused by the painful period of the beginning of the formation of market relations in all industrial and economic structures, almost “obestočila” financial flows on development work.

And Sukhoi. N.i. Kamov helicopters with the aim of attracting investment in proactively in 1990 year expands the work on creation of a civilian helicopter version-60 under the designation Ka-62. Supervision is entrusted to the Deputy Head of the Department of technical projects of OKB Gubarevu Ba and Fuhrmann to a leading pattern designer of V.a.

On the basis of aerodynamic model forms glider helicopter Ka-60 built a mock helicopter Ka-62, the Interior of which was made in freight and passenger variants. Transport helicopter cabin up to 6.0 m2 allowed to hold up to 10 passengers in economy class or 6 students per class “VIP”, or provide mechanized loading of cargo weighing up to 450 lbs.

A mock helicopter Ka-62 in 1991 year, shown at the first international aviation saloon in Russia, held at the Expocenter.

The cockpit of the helicopter Ka-62 was equipped with damping armchairs, and the dashboard for the first time in the domestic vertoletostroenii is equipped with electronic equipment based on liquid crystal displays, created by authors NIIAO, including Ilyushin staff. N.i. Kamov √ Gubarev B.a. and Krygin V.g.

Beyond the nineties Sukhoi. N.i. Kamov strengthened market promotes the Kamov Ka-62, demonstrating its layout at all, have become regular, airshows and in parallel actively negotiating joint ventures with various Western European firms such as British firm Rolls-Royce and the Italian firm Agusta.

Ka-62 is the first helicopter “Kamov”, performed on a single circuit with steering screw in vertical plumage. A great deal of attention when designing the helicopter was drawn to increase its effectiveness by increasing the cruising speed, reducing fuel consumption and increase the weight of the impact, as well as by reducing labour input of maintenance.

Held in conjunction with the TSAGI theoretical and experimental research have significantly reduce aerodynamic resistance of the helicopter and the use of advanced profiles and configuration optimization of blades ensure increased relative and propulsive efficiency and achievement of maximum equivalent aerodynamic quality, equal to 4.

Ka-62 built on the single scheme with steering screw in ring channel vertical empennage. Blades and glider to 60 per cent by weight are made of polymer composite materials. The glider is distinguished by perfect aerodynamic shapes, large transport-passenger cabin and trehstoečnym chassis with tail support. The power plant includes engines of new generation modular development of Rybinsk motor design Bureau led by Chief Designer A. S. Novikov. Civilian modification of basic military uses a high cruising speed, fuel efficiency and transport performance, wide doorways transport cabin on both sides of the fuselage.

The helicopter can be used for the carriage of passengers with proper comfort, cargo transportation in the cabin and on the sling, emergency medical aid, rescue, maintenance of the ice reconnaissance and patrol operations, monitoring water boundaries and the boundaries of economic zones, maintenance of offshore gas and oil pipelines, etc.

Ka-62 was designed taking into account the international requirements for safety. Provided flight and landing with one engine running. Safety of the pilot and passengers in the event of a rough landing is guaranteed by a complex of measures, including energy-absorbing seats and chassis construction. Tail rotor in Kiel is protected from accidental damage. The machine is equipped with effective de-icing and fire systems.

Ka-62 can have as standard equipment the underlying transport choices for flights in terms of sight and complex for piloting vintokrylogo apparatus for instruments in all weather conditions using satellite navigation equipment. Export version of the helicopter may at the request of the customer to have the engines and avionics of foreign firms.

In the year 2012, at HeliRussia 2012 hosted a presentation layout Ka-62, which constitutes an updated design of the helicopter. External scheme and layout of the helicopter have been retained, major changes have affected the chassis and the engine compartment because instead of Russian turboshaft engines Rd-600 on the machine are installed French Turbomeca Ardiden 3 g. Gearbox and transmission will supply the Austrian firm Zoerkler.

You plan to deploy to production plants of the holding “Russia Helicopters”: AAA “progress” (build helicopters) and JSC “kumapp” (components of main and tail rotors). At the moment the arsen′evskom plant started production of two prototypes.

According to the results of tests in 2013 year helicopter demanded improvements, certification is scheduled for no earlier than the year 2015. On finalization of the additional funding is allocated. At the same time, trial flights of military version is scheduled to begin in March 2014 years. In July the year 2014 by Transas supplied the first three integrated pilot-navigating complex of the CCD-62 for advanced machines and conduct flight tests. Until the first quarter of 2016, should be the delivery of the first seven machines for export.

“Russia helicopters” were planning to demonstrate first flight sample Ka-62 on Maks 2013 at the end of August this year.

Design.

Single-rotor helicopter circuit with steering screw in vertical plumage, with two GTD and removed tricycle-equipped landing gear. Helicopter construction differs widely KM, constituting more than 50% of the mass of the structure.

The fuselage is characterized by good aerodynamic shapes (square equivalent harmful plates about 1.25 m2), has a metal frame with frames and longitudinal beams, and a covering of laminated panels of KM based on glass-and carbon. The fuselage consists of four sections: the cockpit, mid-section with a passanger cabin, tail boom with a horizontal tail and vertical tail with the tail rotor channel. The cockpit has a large glazing area and power set lantern from KM, on the sides of the cabin doors open outward against the stream. The pilot’s seat is located on the right side (a first for domestic helicopters), to avoid duplication of control bodies at the crew of two pilots, in this case establishes controls for the second pilot.

In the middle of the fuselage cabin mixed sizes posted 3.3 x 1.75 x 1.3 m with large sliding cargo door size 1.3 x 1.25 m. The tail boom-elliptical cross-section installed unmanaged stabilizer panache 3 m, rectangular in plan, with a large pin washers with asymmetrical profile to create lateral aerodynamic force and unloading of the tail rotor. The docked tail boom big vertical plumage with profiled channel for the tail rotor, on top of the keel with asymmetrical profile.

The chassis of the tricycle landing gear, with a contractile tail samoorientiruûŝejsâ prop telescopic type with double wheels, retractable back in the tail boom. The main Fulcrum lever type with nitrogen-oil shock absorbers retracts forward and sideways into the fuselage. The supports can be installed inflatable ballonets for emergency landing on water.

Rotor četyrehlopastnyj with elastic fastening blades. Chassis bushings made of steklougleplastika, detachable, Bush has only self-lubricating bearings vertical instead of horizontal hinges and axial joints used torsion bars of steel package inserts and elastic elements made of fiberglass.

All-composite blades, rectangular in plan, with the wake of the ending. Dual-spar has the shape of a sock, profile along the sock passes the rubber coating with electrical de-icing system. The chord of the airfoil 0.53 m.

Tail rotor diameter of 1.4 m, with a hard mount blade, with axial hinges. Blades with chord 0.089 m are rectangular in plan, part of the blade is protected titanium metallic.

The powerplant consists of two GTD Rd-600 take-off capacity of 955kVt and cruising capacity of 735 kW. Emergency mode power 1139kVt, built one engine for 2.5 min with another engine failure. Engines installed in General for the main rotor shaft fairing, air intakes on radome fitted with airborne thermal de-icing system. The motors are equipped with digital electronic control with fully redundant channels, is modular in design. Module generator combines racing with three axial compressor and single-stage centrifugal annular combustion chamber and two-stage turbine driving the compressor. Free turbine also two-step. The engine has a length of 1.56 m, width 0.76 m and 0.72 m height, dry weight 220 kg. Starting of engines is carried out from the auxiliary power unit AI-9.

Fuel system includes 4 soft tank with total capacity of 1100l placed under the floor of the cab, with oil pumps to supply engines from any group.

Transmission with two-stage main gearbox is designed for the transfer of power take-off, tail, single stage reducer 1910kVt.

Control system with hydraulic steering transmissions, United in a common block to the chassis of the gearbox and rigid rods, includes boot trimmernye mechanisms.

Hydraulic system consists of two autonomous subsystems, first provides power steering drives, second ≈ cleaning systems wheels and their brakes.

Electrical system consists of a dual system of alternating three-phase current with two contactless generators with a capacity of 30 kW and dual channel system with two DC rectifiers and battery.

Equipment. Flight navigation system provides improved stability and controllability, automated stabilizing angular positions of a helicopter flying at a specified rate and specified path line, warning the maximum permissible flight modes. In the cockpit is equipped with two multi-function indicator on the CRT. The rescue variant provides the winch with a lifting capacity of 300 kg.

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