LOCATION. LOCATION HISTORY Turbine Plant «Zorya» for marine turbines manufacturing was established – Design Bureau for marine gas turbines.

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Presentation transcript:

LOCATION

HISTORY 1953 - Turbine Plant «Zorya» for marine turbines manufacturing was established. 1954 – Design Bureau for marine gas turbines development was established. 1961 –Design Bureau «Mashproekt» was established. 2001 – Both companies merged into – Gas Turbine Research & Production Complex «ZORYA-MASHPROEKT».

GENERAL INFORMATION ► Total area – 2 km2 ► Facilities for gas turbine production over 1 000 MW per year ► Gear boxes manufacturing 150 - 55 000 kW ►Gas Turbine Propulsion units manufacturing ►Gas Turbine Mechanical Drive units manufacturing ► Gas Turbine Generators manufacturing ► Gas turbine’s auxiliary systems – lubricating, fuel, pneumatic, etc manufacturing ► After-sales service

ZORYA - MASHPROEKT GAS TURBINE ENGINES FOR MARINE PROPULSION» Rated power, kW Efficiency, % UGT 3000 reversible 3,360 29.0 non reversible 3,360 31.0 Rated power, kW Efficiency, % UGT 6000 reversible 7,350 30.0 non reversible 7,350 32.0 UGT 6000+ Rated power, kW Efficiency, % reversible 8,800 31.0 non reversible 8,800 33.0 Rated power, kW Efficiency, % UGT 15000 reversible 14,700 32.0 non reversible 17,650 35.4

ZORYA - MASHPROEKT GAS TURBINE ENGINES FOR MARINE PROPULSION» UGT 15000+ Rated power, kW Efficiency, % non reversible 20,000 36.0 UGT 16000 Rated power, kW Efficiency, % reversible 16,550 30.0 UGT 25000 Rated power, kW Efficiency, % non reversible 28,700 37.0

UGT 3000» DESIGN FEATURES Three-shaft gas turbine comprising two-spool turbocompressor and free power turbine. Compressor - axial. 8 stages low pressure compressor, 9 stages high pressure compressor. Combustion chamber - can-annular reverse flow with 9 combustion liners.

UGT 3000» FEATURES 1 - Variable geometry inlet guide vane 2 - Low pressure compressor 3 - High pressure 4 - Combustion chamber 5 - High pressure turbine 6 - Low pressure turbine 7 - Power turbine 8 - Power flange 9 - Auxiliary gearbox 10 - Electric starter 11 - Frame

MAIN CHARACTERISTICS OF DE76 & DS76 ENGINES ACCORDING TO ISO 2314 MODEL DE76 DS76 Rated power, kW 3,360 Efficiency, % 31.0 29.0 Output shaft speed, rpm 9,700 8,800 Specific fuel consumption, kg/kWh 0.272 0.291 Exhaust gas mass flow , kg/s 15.5 16.0 Exhaust gas temperature, 0C 440 470 Pressure ratio 13.5 14.0 Dimensions (LxWxH), m 2.5 х 1.3 х 1.25 2.5 х 1.8 х 1.8 Weight, t 2.5 2.8

DP71 DS77 DS71 UGT 6000» Compressor end (cold end) power extraction Power turbine end (hot end) power extraction DS71 Power turbine end (hot end) power extraction

UGT 6000+» DP73 Power extraction from both sides (hot and cold ends) DP79 Compressor end (cold end) power extraction

MAIN CHARACTERISTICS OF UGT6000 TYPE ENGINES ACCORDING TO ISO 2314 MODEL DP71 DP79, DP73 * DS71 DS77 Rated power, hp (kW) 10,000 (7,350) 11,970 (8,800) 9,994 (7,350) Efficiency, % 32.0 33.0 30.0 31.0 Output shaft speed, rpm 7,000 4,750 7,300 Specific fuel consumption, kg/kWh 0.263 0.255 0.281 0.272 Exhaust gas mass flow , kg/s 32 34 32.5 34.5 Exhaust gas temperature, 0C 460 470 500 Dimensions (LxWxH), m 3.2 x 1.7 x 1.8 3.2 x 1.6 x 1.7 3.4 x 1.7 x 1.8 Weight, t 3.5 * DP79 – engine with single end power flange DP73 – engine with double end power flanges

UGT 15000 » DESIGN FEATURES Three-shaft gas turbine combines with two-spool gas generator and free power turbine. Compressor - axial. 9 stages low pressure compressor, 10 stages high pressure compressor. Combustion chamber - can-annular reverse flow with 16 combustion liners. Start - electric motors U=380 V AC, N=60 kW (2 x 30 kW).

UGT 15000» FEATURES 1 - Inlet device 2 - Variable geometry inlet guide vane 3 - Lubricating oil separator 4 - Low pressure compressor 5 - High pressure compressor 6 - Combustion chamber 7 - High pressure turbine 8 - Low pressure turbine 9 - Reverse mechanism 10 - Power turbine 11 - Power flange 12 - Auxiliary drive gearbox 13 - Electric starters 14 - Frame

MAIN CHARACTERISTICS OF UGT 15000 ENGINES MODEL DA90 DO90 Rated power, kW 17650 14700 Efficiency, % 35.4 32.0 Output shaft speed, rpm 5300 4400 Specific fuel consumption, kg/kWh 0.238 0.263 Exhaust gas mass flow , kg/sec 73.0 70.0 Exhaust gas temperature, 0C 430 Dimensions (LxWxH), m 4.8 x 2.1 x 2.2 5.0 x 2.8 x 2.8 Weight, t 9 11.5

UGT 15000+ » DESIGN FEATURES Three-shaft gas turbine combines with two-spool gas generator and free power turbine. Compressor - axial. 9 stages low pressure compressor, 10 stages high pressure compressor. Combustion chamber - can-annular reverse flow with 16 combustion liners. Start - electric motors U=380 V AC, N=60 kW (2 x 30 kW).

UGT 15000+» FEATURES 1 - Variable geometry inlet guide vane 2 - Low pressure compressor 3 - High pressure compressor 4 - Fuel atomizer 5 - Combustion chamber 6 - High pressure turbine 7 - Low pressure turbine 8 - Power turbine 9 - Power flange 10 - Auxiliary drive gearbox 11 - Electric starters 12 - Frame

MAIN CHARACTERISTICS OF UGT 15000+ ENGINES MODEL Rated power, kW 20,000 Efficiency, % 36.0 Output shaft speed, rpm 3,500 Specific fuel consumption, kg/kWh 0.234 Exhaust gas mass flow , kg/sec 76.5 Exhaust gas temperature, 0C 450 Pressure ratio 20.0 Dimensions (LxWxH), m 6.1 x 2.2 x 2.5 Weight, t 12.8

UGT 25000» DESIGN FEATURES Three-shaft gas turbine engine consists of two-spool gas generator and 4-stage free power turbine. Compressor - axial. 9 stages low pressure compressor, 9 stages high pressure compressor. Combustion chamber - can-annular reverse flow with 16 combustion liners. Start - electric motors U=380 V AC, N=90 kW (2 x 45 kW).

UGT 25000» FEATURES 1 - Variable geometry inlet guide vane 2 - Low pressure compressor 3 - High pressure compressor 4 - Fuel atomizer 5 - Combustion chamber 6 - High pressure turbine 7 - Low pressure turbine 8 - Power turbine 9 - Power flange 10 - Auxiliary drive gearbox 11 - Electric starters 12 - Frame

MAIN CHARACTERISTICS OF DA80 ENGINES ACCORDING TO ISO 2314 MODEL DA80 Rated power, kW 28,700 Efficiency, % 37.0 Output shaft speed, rpm 3,400 Specific fuel consumption, kg/kWh 0.228 Exhaust gas mass flow , kg/s 94.0 Exhaust gas temperature, 0C 500 Pressure ratio 22.5 Dimensions (LxWxH), m 6.4 x 2.5 x 2.7 Weight, t 16

UGT 5000» DESIGN FEATURES Single shaft gas turbine 11 stages compressor Combustion chamber – silo type, 8 combustion liners. Start - electric motors U=380 V AC, N=264 kW (2 x 132 kW)

MAIN CHARACTERISTICS OF UGT5000 ENGINES ACCORDING TO ISO 2314 MODEL Rated power, kW 5250 Efficiency, % 32.0 Output shaft speed, rpm 3000, 1500 (1800) Specific fuel consumption, kg/kWh 0.263 Exhaust gas mass flow , kg/s 21.5 Exhaust gas temperature, 0C 480 Pressure ratio 14 Dimensions (LxWxH), m 7.8 x 2.4 x 2.4 Weight, t 10.1

MAIN MARINE PROPULSION PLANTS FOR DISPLACEMENT SHIPS MARINE PROPULSION PLANTS FOR HOVERCRAFTS AND HYDROFOILS MARINE PROPULSION PLANTS FOR MERCHANT VESSELS

CODOG Marine Propulsion Plants Gas turbine engine: UGT15000 (DO90) - 2 units Diesel - 1 unit Gearbox: RO44 - 1 unit MISSILE FREGATE «GEPARD» Speed – 32 knots Displacement – 1,500 t Power – 33,000 hp

Reduction Gear for CODOG Non reversible two-stage reduction gearbox for CODOG installation provides separate operation of the gas turbine or diesel engine. M A I N D A T A Engine type GT Diesel Rated power - ahead, hp Gear ratio Output shaft speed, rpm 17,000 14.03 250 7,500 5.12 190 Weight, t 25 Dimensions , m 4.0 x 3.6 x 2.9

COGAG Marine Propulsion Plants Gas turbine engine: UGT15000 (D090) – 2 units UGT6000 (DS71) – 2 units Gearboxes: R058 – 2 units R063 – 2 units R1063 – 1 unit (for transmitting power to another shaft line) COGAG DS71 R063 R1063 D090 R058 GUARD-SHIP «YASTREB» Speed – 30 knots Displacement – 3,700 t Power – 54,000 hp

CODOG Marine Propulsion Plants Gas turbine engines: UGT15000+ (DA91) – 2 units Diesels – 2 units Gearboxes: RO56 – 2 units CODOG DESTROYER Speed – 29 knots Displacement – 4,500 t Power – 64,800 hp

Reduction Gear for CODOG Reversible two-stage reduction gearbox for CODOG installation provides separate operation of the gas turbine or diesel engine. Gearbox reversing is accomplished by means of set of friction and jaw clutches and fluid couplings, and the power turbine fluid brake. M A I N D A T A Engine type GT Diesel Rated power - ahead, hp Gear ratio ahead astern Output shaft speed, rpm Weight, t 27,200 14.39 9.91 240 125 37 5,200 6.89 6.69 145 82 Dimensions , m 3.9 x 3.8 x 4.0

CODOG Marine Propulsion Plants Gas turbine engines: UGT25000 (DA80) – 2 units Diesels – 2 units Gearboxes – 2 units CODOG DESTROYER Speed – 29 knots Displacement – 7,000 t Power – 79,600 hp

CODLAG Marine Propulsion Plants Gas turbine engines: UGT15000+ (DA91) – 2 units Electric motors – 2 units Gearboxes – 2 units CODLAG DESTROYER Speed – 30 knots Displacement – 4,500 t Power – 65,300 hp

Reduction Gear for CODLAG Reversible two-stage reduction gearbox for CODLAG installation provides operation of the gas turbine and electric motor. Gearbox reversing is accomplished by means of set of friction and jaw clutches and fluid couplings, and the power turbine fluid brake. Engaging of the gearbox to the shaft-line provides via tires-pneumatic clutch. Shaft Electric Motor GT Port Gearbox Link Gear M A I N D A T A Engine type GT El. motor Rated power - ahead, hp Gear ratio Output shaft speed, rpm 27,200 14.39 240 5,500 1 145 Dimensions , m 4.0 x 3.9 x 4.0 Starboard Gearbox

COGAG Marine Propulsion Plants Gas turbine engines: UGT6000+ – 2 units Gearboxes – 2 units Link gearbox – 1 unit COGAG PATROL BOAT Speed – 40 knots Displacement – 200 t Power – 15,000 hp

Reduction Gear for COGAG 1 – starboard gearbox 2 – port gearbox 3 – link gearbox M A I N D A T A Rated power - ahead, hp Gear ratio Output shaft speed, rpm 15000 7.56 910 Dimensions , m 2.4 x 2.5 x 1.7

M35 Marine Propulsion Plants Gas turbine engine: UGT6000 (DP71) – 5 units Gearboxes: R035-10 – 3 units R035-20 – 2 units R035-21 – 2 units R035-22 – 2 units DP71 R035-20 R035-21 R035-22 R035-10 M35 LANDING HOVERCRAFT «ZUBR» with installation M35 Speed – 63 knots Displacement – 550 t Power – 50,000 hp (pr. 1232, HOVERCRAFT «KEFALLINIA», 2001-2005)

M73 Marine Propulsion Plants Gas turbine engine: UGT 6000+ (DP73) – 2 units Gearboxes: RC73-10 – 2 units RC73-20 – 2 units RC73-30 – 2 units LANDING HOVERCRAFT «ACV-1» with 2 installations M73 Speed – over 50 knots Displacement – 175 t Power – 2 x 10,000 hp

MT70 Marine Propulsion Plants Gas turbine engine: UGT 6000 (DP71) - 2 units Gearboxes: R071 - 2 units R1071 - 2 units R2071 - 2 units LANDING HOVERCRAFT «MURENA» with 2 installations MT70P Speed - 60 knots Displacement - 130 t Power - 20,000 hp

compliance with Customer’s technical specifications. DEVELOPMENT AND DELIVERY TESTS Development and delivery tests of gas turbine units (GTU) are divided into the following stages: – pre-delivery and acceptance tests at GTRPC «Zorya»- «Mashproekt» test rig; – assembly testing at Customer’s full-sized test rig; – mooring trials; – sea trials and delivery tests. GTU М79R at test rig Tests objective is to check GTU workmanship and quality of assembly as well as its compliance with Customer’s technical specifications.

MODERNIZATION OF M36 and M15 GTA Existing GTA Modernize GTA Fuel equipment Old fuel system with hydraulic drive throttle valve New fuel system with fuel control valve with electrical driver Ignition system СКНА-22 (with radioactive elements) СPВI-2-2Н Reverse mechanism control unit Excluded. The instrument functions are implemented in microprocessor local control system (LCS). Control system (relay-type), pulse temperature regulator, temperature pattern alarm and etc. Microprocessor local control system (LCS): performs the function of GTE modes control, GTE and RG protection, of restriction and protection in terms of temperature downstream of LPT, monitoring of MGTA parameters. Indicating instruments (located at control panels) All the instruments are excluded, the data are displayed on the screens of operator’s work stations

MODERNIZATION OF M36 and M15 GTA 1. Fully microprocessor based automatic control system (ACS) made in accordance with Naval requirements and provides all functions related to regulating, control, protection and monitoring parameters of GTU 2. The ACS is performed by the SE GT&PC “Zoria”-”Mashproekt” on the base of MicroNet™ Plus or GTC250 Digital Control System (Woodward), which is in public sale anywhere in the world, equipped with control units, peripheral units, consoles equipment, power units. 3. ACS is compliant with any IPMS. Connection between ACS and IPMS, as well as connection between ACS and equipment of main and emergency control panels, is made by a doubled Ethernet network (protocols Modbus TCP / IP or Modbus RTU), which is currently the most popular. 4. The ACS software conforms to open architecture standards. The SW adjustment (if necessary) is carried out by “Zoria”-”Mashproekt” specialists or the customer. ACS of GTA M15

MODERNIZATION OF M36 and M15 GTA P15 with GTA M36E modernization

QUALITY MANAGEMENT SYSTEM Company's quality management system matches to ISO 9001-2008 international standard.

Guarantee obligations MAINTENANCE Guarantee obligations ► Enterprise provides guarantee maintenance and after-guarantee maintenance of engines. ► In the process of operation (till overhaul) on board the ship no replacement of the engine inner parts and components is required. ► Engines repair is carried out at specialized enterprise on expiry of TBO life or service life. ► During GTE delivery GTRPC «Zorya» - «Mashproekt» provides Customer with complete set of spare parts, tools and appliances necessary for maintaining of engine operation till overhaul and also provide with devices for engine loading and installation on board the ship. Delivery of the engine spares set is guaranteed under separate contracts to ensure long operating life.

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