УПРАВЛЯЮЩАЯ КОМПАНИЯ moscow 2010. УПРАВЛЯЮЩАЯ КОМПАНИЯ all gas...

УПРАВЛЯЮЩАЯ КОМПАНИЯ

Moscow2010


All gas turbine engines for pipelinesAll gas turbine engines for pipelines made and installed frommade and installed from 1991 1991 until until 2008 2008

Company TypeSpecifications

Basic air engine AmountPower, MW Efficiency, %

«Perm Motors» JSC

GTU-4PG 4,08 24,2 D-30 1

GTU-6PG 6,29 27,37 D-30 2

GTU-10P 10,26 31,9 PS-90A 40

GTU-12P 12,4 33,8 PS-90A 74

GTU-16P 16,44 35,8 PS-90A 169

GTU-25P 25,56 38,5 PS-90A 3

Total 289

«Saturn – Gas Turbines» JSC

GPA-4RM 4,1 32,5 no 24

GPA-6,3RM 6,46 32,58 no 1

GPA-10RM 10,16 35,5 no 4

AL-31ST 16,8 36,0 AL-31F

Total 29

«Ufa Engine Industrial Association» JSC, «Motor» SPE

AL-31STN 16,8 37,0 AL-31F 31

Total 31

«Kuznetsov» JSC, N.D.Kuznetsov STC

NK-12ST 6,3 26,3 NK-12MV 459

NK-14ST-8 8,54 32,0 NK-12MP 181

NK-14ST-10 10,6 34,0 NK-12MP 7

NK-36ST 26,5 36,0 NK-32 15

Total 662

«Klimov» JSCGTP-1,25 1,276 26,0 TVЗ-117 3

GTP-2,5 2,55 26,0 TVЗ-117

Total 3

Total - Total - 10141014


Main world energy market sectors for gas turbines

Main world energy market sectors for gas turbines

Oil and gas extractionOil and gas extraction – extraction from depth, pumping of water and gas into stratums.

Oil and gas processingOil and gas processing – petroleum refining, gas cleaning.

Oil and gas transportOil and gas transport – gas liquation, oil and gas pumping to storages and pipelines.


Gas turbines for gas pipelines by«Perm Motors» JSC


GTU-4PG Industrial Gas Turbine

Specification(ISO Conditions, loss-free,fuel: Methane (LHV=11958 kCal/kg)Power turbine shaft output, MW 4,0Efficiency at power turbine shaft, % 24,0Exhaust gas temperature, °С 419Power turbine / step-up gearrotation speed, rpm 7 000 - 7 500 / 14 000Exhaust gas flow, kg/s 28,7Service life:- overhaul interval, h 25 000- assigned, h 100 000

GTU-4PG gas turbine with M-45PHG step-up gear is used as a mechanical drive of centrifugal natural gas compressors in "Ural" GPA-4PHG gas turbine pumping packages of underground gas storages. The gas turbine is suitable for operation under moderate and cold climate conditions.The core of the gas turbine is the D-30EU-2 gas turbine engine developed on the basis of the D-30 III Series aero-engine. M-45PHG step-up gear matches the power turbine speed (7014 rpm) and mechanical drive shaft nominal speed (14000 rpm).M-45PHG step-up gear makes it possible to optimize the parameters of a gas turbine pumping package.The first gas turbine has been installed at Kasimovskaya compressor station of Mostransgaz. It is currently in experimental commercial operation in "Ural" GPA-4PHG gas pumping package.


GTU-6PG Industrial Gas Turbine Engine

Specification(ISO Conditions, loss-free,fuel: Methane (LHV=11958 kCal/kg)Power turbine shaft output, MW 6,17Efficiency at power turbine shaft, % 26,82Exhaust gas temperature, °С 472Power turbine / step-up gearrotation speed, rpm 7000-7500 / 9000Exhaust gas flow, kg/s 33,3Service life: - overhaul interval, h 25000- assigned, h 100000

The updated GTU-6PG gas turbine with M-60 step-up gear was developed as a mechanical drive for centrifugal compressors used in gas turbine pumping packages.M-60 step-up gear makes it possible to optimize the parameters of a gas turbine pumping package.In 2006 the first gas turbine was installed at Myldzhinskoe gas-compressor field of Tomskgazprom. The gas turbine is currently in pilot operation in "Ural" GPA-6DKS gas pumping packaged unit.The gas turbine is also used as part of "Ural-6000"gas turbine pumping package, which was delivered to the Booster Station-2 within the Sakhalin-2 Project.




GTU-10P Industrial Gas Turbine Engine

Specification(ISO Conditions, loss-free,fuel: Methane (LHV=11958 kCal/kg)Power turbine shaft output, MW 10,3Efficiency at power turbine shaft, % 33,1Exhaust gas temperature, °С 454Output speed, rpm 9 000Exhaust gas flow, kg/s 42,9Service life:- overhaul interval, h 25 000- assigned, h 100 000

GTU-10P industrial gas turbine is based on GTU-12P gas turbines and is used in the packaged modular gas pumping units, in gas boost compressor stations (BCS), and stations of underground gas storage (UGS), and in particular in GPA-10 BCS "Ural" and GPA-10 UGS "Ural" manufactured by Iskra, and also, for retrofitting the existing GPA-C-6,3 packages and others.The distinctive feature of the design are a high-speed power turbine that contributes to high efficiency of a gas compressor and a gas generator unified with GTU-12P gas turbine. The gas turbine inherited all advantages of GTU-12P.





Specification(ISO Conditions, loss-free,fuel: Methane (LHV=11958 kCal/kg)Power turbine shaft output, MW 12,37Efficiency at power turbine shaft, % 34,6Exhaust gas temperature, °С 470Output speed, rpm 6500Exhaust gas flow, kg/s 46,1Service life:- overhaul interval, h 25 000- assigned, h 100 000

GTU-12P gas turbine is used as a mechanical drive of a centrifugal natural gas compressor in gas turbine pumping packages. GTU-12P has been successfully proven in service at Russian gas pumping stations. It is operated as part of "Ural" GPA-12 packaged modular gas pumping unite manufactured by Iskra and is used to retrofit the existing gas pumping packages such as GTK-10, GPA-C-16 and some others.GTU-12P core is the PS-90GP-1 gas turbine engine based on the PS-90А aircraft engine, the only one Russian fourth generation civil aviation engine with International Type Certificate.






GTU-16P gas turbine has been designed on the basis of the gas generator of the high performance PS-90 aircraft engine and GTU-12P gas turbine.The gas turbine has higher cycle parameters (utilization of 14-stage compressor) and has a power turbine adapted to the existing gas turbine pumping packages.The gas turbine is used in the GPA-16 "Ural" packaged modular-type gas pumping units manufactured by Iskra, and for the reconstruction of the existing gas turbine pumping sets, such as GTK-10, GPA-C-16, GPU-16, GPU-10 and others. GTU-16P gas turbines have perfectly promoted themselves while running at gas compressor stations of Russia.It is unified and completely interchangeable with GTU-12P gas turbine, and inherits all the advantages and merits of the latter.






Among Perm gas turbines GTU-25P has got the highest power rated at 25 MW. It is intended to drive gas compressors in new-generation gas compressor packages, and to pump gas into underground gas storage.GTU-25P is based on the PS-90GP-25 gas turbine engine, which is an industrial derivative of the high efficiency PS-90A aero engine incorporating as well GTU-12P and GTU-16P gas turbine components.The engine consists of:two-shaft gas turbine gas generator module; power turbine module. The engine and power turbine located on the common engine mount are installed on the gas compressor package skid.




Reference list

Customer Location Amount Operation start

Gazprom transgaz Moscow Kasimovskoe UGS 1 Operation testing

Total 1

Operating time, h 7 498


Tomskgazprom Myldzhinskoe NGF 2 2007

Total 2


4 MW

6 MW




Reference list (continue)


Gazprom transgaz Tchaikovsky Karashurskoe UGS 2 2003

Gazprom dobycha Urengoy

GBS-2V/1 4 2006

GBS -2V 1balancing and commissioning

Gazprom dobycha Orenburg

Sovhoznoe UGS 6 shipment

GBS -3 6 2006

Gazprom dobycha Yamburg GBS -1V 6 2004

Gazprom transgaz Ufa Kanchurinskoe UGS 6 2007

Gazprom transgaz Saratov Elshanskoe UGS 4balancing and commissioning

10 MW





NOVATEK - Tarkosaleneftegaz Hancheiskoe NGF 2 assembling

NORTGAZ S-Urengoiskoe NGF 2balancing and

commissioning

Lukoil – Zapadnaya Sibir S-Gubkinskoe NGF 2balancing and

commissioning

Rosneft Priobskoe NGF 3 shipment

Total 44







Gazprom transgaz Tchaikovsky

GBS-2 Permskaya 1 1994




GBS-18 Ordinskaya 5 1995

Gazprom transgaz Samara GBS -11 Pavlovskaya 3 1997

Gazprom transgaz Ekaterinburg GBS -12 Shatrovskaya 3 1999

Gazprom transgaz Ufa GBS -6 Sharan 4 2000

Gazprom transgaz Moscow

GBS Tuma 4 1998

GBS Belousovo 2 2002

GBS Volokolamskaya 2 2006

GBS Voskresenskaya 3 2008

Gazprom transgaz YugorskGBS Novourengoiskaya-3 9 2003

GBS Novourengoiskaya-4 8 2007

12 MW






Surgutneftegaz

GBS-42 Fedorovskaya 3 2001

GBS -44 Fedorovskaya 4 2003

Gazprom transgaz Kuban GBS Kracnodarskaya 5 2003

Gazprom transgaz Stavropol GBS Stavropolskaya 5 2003

Gazprom transgaz Uhta

Mikun 2 shipment

Gryazovets 2 shipment

Myshkino 1 shipment

Yuganskneftegas Priobskoe NGF 3 2007

Total 72

Operating time, h 1 239 719






Gazprom transgaz Tchaikovsky

GBS-18 Ordinskaya 1 1995

GBS -2 Permskaya 2 1995

GBS -1 Gornozavodskaya 4 2001

GBS -19 Tchaikovskaya 4 2002

Gazprom transgaz Samara GBS Sokovka 2 2004

Gazprom transgaz EkaterinburgGBS -12 Shatrovskaya 9 2000

GBS Dolgoderevenskaya 1 shipment

Gazprom transgaz Ufa GBS -6 Sharan 2 2001

Gazprom transgaz Kuban GBS Kamensk Shahtinskaya 4 2007

Gazprom transgaz Yugorsk

GBS Purovskaya-2 6 2003

GBS Purovskaya-3 4 2003

GBS Novokomsomolskaya 1 2005

Gazprom dobycha Noyabrsk

GBS Zapadnotarkosalinskaya 4 2003

GBS Zapadnotarkosalinskaya 4balancing and

commissioning

Gazprom transgaz Stavropol GBS Salskaya 6 2003

16 MW




Reference list (continue)Customer Location Amount Operation start

Gazprom transgaz Volgograd GBS Volgogradskaya 5 2003

Gazprom transgaz UhtaGBS Urdoma 4 2006

GBS Vuktyl 2 2005

Gazprom dobycha YamburgGBS -2 7 2002

GBS -5 7 2002

Gazprom transgaz Surgut

GBS Purtazovskaya-1 6 2002




Gazprom dobycha Nadym

GBS Yamsoveiskaya 5 2003

GBС Yamsoveiskaya-2 6balancing and

commissioning

GBS Yubileinaya 6 2003

Yubileinaya GBS -2 6 2008

Gazprom transgaz Saint-PetersburgGBS Smolenskaya 6 2004

GBS Torzhokskaya 6 2004

Beltransgaz GBS Krupskaya 7 2005

Turkey GBS Sivas 3balancing and

commissioning






Severneftegaz Yuzhnorusskaya 4 shipment

Tarkosaleneftegaz Vostochnotarkosalinskaya GBS 6 2006

Total 160

Operating time, h 2 358 536






Gazprom transgaz Tchaikovsky GBS Igrinskaya 1 2004

Total 1


25 MW





Index GTU-4PG GTU-6PG GTU-10P GTU-12P GTU-16P GTU-25P

Availability ratio 1 0,99 0,99 0,99 0,99 0,99

Technical operation ratio

0,99 0,98 0,96 0,98 0,97 0,98

Starting safety factor 1 0,97 1 0,99 0,99 0,94

Total units 1 2 45 73 175 3

Total power, MW 4 12 450 876 2 800 75

Overall operating time, h

7 498 14 768 248 212 1 239 719 2 358 536 24 545

Leading unit operating time, h

7 498 7 724 25 022 50 036 30 643 14 717

Operating performance




Gas-Pumping Unit GPA-4RM

GPA-4RM - automated gas-pumping unit of container version with rated power about 4 MW. It is intended for use at stations of underground storage of gas and gas pipelines.Gas turbine GTD-4RM by capacity 4 MW is used as a drive of compressor, it was developed on base of ship engine М-75Р.

Gas turbines for gas pipelines by«Saturn – Gas Turbines» JSC


Specification

Power turbine shaft output, MW 3,5 - 3,8Exhaust gas flow, m3/s 27,4 – 91,1


Reference list GPA-4RM

Manufacturer Customer Location AmountOperation

start

Saturn – Gas Turbines

Lentransgaz GBS Izborskaya 5 2007

Mostransgaz UGS Kaluzhskoe 2 2006

Mostransgaz UGS Kasimovskoe 6 2004-2007

Lentransgaz GBS Krasnoznamenskaya 2 2005

Total 15




GPA-6,3RM - automated gas-pumping unit of container version with rated power 6,3 MW. It was developed according to modern requirements of the gas industry for use at reconstruction of existing compressor stations (with replacement of drives D-336-2T and NK-12ST which have developed the resource) and building of new compressor stations for GAZPROM. GTD-6,3RM is the drive of this unit, it was created on base GTD-4RM. GTD-4RM are successfully maintained at compressor stations of GAZPROM now.

Gas-Pumping Unit GPA-6,3RM



Specification

Power turbine shaft output, MW 5,7 – 9,6Output speed, rpm 8000 - 8200Exhaust gas flow, m3/s 127,3 – 167,8


Reference list GPA-6,3RM

Manufacturer Customer Location Amount Operation start


Mostransgaz GBS Gavrilov Yam 1 2007

Total 1




Gas-Pumping Unit GPA-10RM

According to the program of long-term cooperation with Gazprom, Saturn has developed and serially makes gas-pumping units GPA-10RM (on a basis of GTD-10RM drive). It is used for reconstruction of existing and buildings of new compressor stations.Units are completely correspond to the technical and operational requirements of GAZPROM, have the developed system of remote control with high degree of protection.



Specification

Power turbine shaft output, MW 9,3 – 10,0Output speed, rpm 4800Exhaust gas flow, m3/s 227,4 – 347,2


Reference list GPA-10RM

Manufacturer Customer Location Amount Operation start


Severgazprom GBS Nuksenitsa 2 2007

Total 2




AL-31ST-based GPA-16-AL URAL Modular Gas-Pumping Unit

Specification

Power turbine rated shaft output, MW 16

Efficiency, % 36

Fuel gas characteristics at gas-turbine engine inlet:

-fuel gas pressure, MPa (kgf/cm2): 2,74+0,2(28+2)

-fuel gas temperature , °С +20..+60

Fuel gas flow at rated conditions, kg/s (max), 0,902

Air mass flow throughcompressor, kg/s (max) 64,5

Gas turbines for gas pipelines by«UEIA» JSC, «Motor» SPE

Gas turbines for gas pipelines by«UEIA» JSC, «Motor» SPE


NK-12ST Industrial Gas Turbine Engine

The engine NK-12 ST is the first gas- turbine engine of the aviation type created in 1974 for the gas industry on the base of the aircraft turboprop engine NK-12 MV, which was installed on the aircrafts TU-95, TU-114, AN-22 and other.The engine NK-12ST has a high degree of the reliability and economy in the operation. The output of the gas-pumping units with this engine is 11 million m3 of the gas in twenty-four hours.About 2000 engines were manufactured during the series production. Their total operating time made up about 40 000 hours.The engines are operated at more than 100 compressor stations as part of the more 800 gas-pumping units. These engines showed they-selves to the best advantage during their operation.At present time the plant prepared the substitution for the engine NK-12ST and began the production of more perfect engine NK-14ST.

Specification

Output shaft power, KW 6300Rotational speed of theturbine rotor, rpm 8200Exhaust gas temperature, K 843Fuel gas consumption, kg/h 1820Air consumption, kg/s 39Drive efficiency, % 26,1Mass, kg 3500Overall dimensions: Length, mm 4742Diameter, mm 1520Life, h 50 000

Gas turbines for gas pipelines by« Kuznetsov » JSC, N.D.Kuznetsov STC




The engine NK-14ST is designed by order of GAZPROM as a modification of the engine NK-12ST. This engine is created on the base of the engine NK-12ST and is completely interchangeable with it. The engine has improved general performance data.The change of the combustion chamber, turbo-compressor turbine, main and free turbines resulted in engine power and efficiency increase.The engine NK-14ST combines the great experience of NK-14ST engine operation and new achievements in the field of the aircraft engine manufacturing. It is distinguished by high reliability, simplicity in the maintenance, improved technical and ecological data, high efficiency.To date, we can manufacture an modified engine NK-14ST with regenerative cycle, increasing the engine efficiency up to 41.5%.

Specification

Output shaft power, KW 8600Rotational speed of theturbine rotor, rpm 8200Exhaust gas temperature, K 750Fuel gas consumption, kg/h 1930Drive efficiency, % 32Mass, kg 3600Overall dimensions: Length, mm 4742Diameter, mm 1520Life, h 50 000




NK-14ST-10 Industrial Gas Turbine Engine

The main kinds of the drive in the range of GPU of gas transportation system of Russia are gas turbine sets.The analysis of the operating indices of GPU with gas turbine drive at the compressor stations shows that the most part of them has worked their motor life ( 100 000 hours), physically weared out and morally became obsolete. The efficiency of the units range is on the level of 20… 21% at power 0.8 ..0.9 from the nominal value.In this connection during the reconstruction of the operating compressor stations there is question about the installation of the modern gas turbine engines with efficiency more 33%. With the great overhaul life and high reliability.The variant of GTK-10-4, GPU- TS- 10B, GPS -10 serial engine substitution as worked out the life for NK-14ST-10 engine was considered.The leading development engineer of NK-14ST-10 engine is JSC Samara Design bureau of machine building (Samara).The leading supplier of the Gas turbine complex -10-4 is JSC Motorostroitel (Samara).

Specification

Output shaft power, KW 10000Rotational speed of theturbine rotor, rpm 8200Exhaust gas temperature, K 507Fuel gas consumption, kg/h 1820Air consumption, kg/s 39Drive efficiency, % 26,1Mass, kg 3500Overall dimensions: Length, mm 4742Diameter, mm 1520Life, h 100000





The engine NK-36ST is created on the base of the production aircraft engine NK-32. It combines the last achievements in the field of the aircraft engine manufacturing and the great experience in the operation of the engines NK-12ST, NK-14ST on the cross-country gas pipelines.The engine NK-36ST id distinguished by the high reliability in the operation, high efficiency, the improved technical data. The level of the emission NOx is reduced up to 120 mg/m3 on the engine NK-36ST. This is less than the norm (150 mg/m3).The systems of the tolerance, of the control, of the protection and of the alarm, which secure the automatic starting, detection of the faults and parameters deviations at the operating engine are provided for the this engine. In addition, the anti-icing system, which permits to operate at the non-favorable atmospheric conditions is also provided for it.The modular construction of the engine permits to carry it by any kind of the transport, to make the replacement of the modules in the conditions of the compressor station.The gas-pumping unit with the engines NK-36 operates successfully at Tolyatti gas compressor station and has good operation data at the high degree of the reliability.

Specification

Output shaft power, KW 25000Rotational speed of theturbine rotor, rpm 5000Exhaust gas temperature, K 698Fuel gas consumption, kg/h 5163Drive efficiency, % 26,1Mass, kg 8690Overall dimensions: Length, mm 6000Diameter, mm 2300Life, h 45000




GTP-1,25 and GTP-2,5 Industrial Gas Turbine Engines

GTP industrial power units (power class from 1,25 to 2,5 MW) are developed and produced on the basis of TV2-117, TV3-117, GTD-1250 and other Klimov’s engines. These units are designed to operate as power station modules (electrical and thermal electrical stations, pump stations, compressor stations etc.).The GTP power units are highly reliable, whether running on natural gas, associated gas, diesel fuel, gasoline, kerosene or their mixtures in any proportion. Depending on the required power output, the unit consists of one or two engines and a gearbox mounted on a common frame together with the necessary auxiliary equipment. These industrial power units may also be installed on a variety of means of transportation (heavy dump trucks, locomotives, marine and river speed boats, hovercraft).

Specification

Brand GTP-1,25 GTP-2,5Type of gas turbine TV3-117 TV3-117Power, MW 1,25 2,5

Gas turbines for gas pipelines by« Klimov » JSC

Gas turbines for gas pipelines by« Klimov » JSC


All types of engines for pipelines in Russian All types of engines for pipelines in Russian gas-transport systemgas-transport system

All types of engines for pipelines in Russian All types of engines for pipelines in Russian gas-transport systemgas-transport system

Gas turbines

Electric motors

Gasmotocompressors


Perm Motors

Saturn – gas turbines

Ufa Engine Industrial Association, Motor

Kuznetsov, N.D.Kusnetsov STC

Klimov

Market diagram of all UnitedMarket diagram of all United Engine Corporation’s Engine Corporation’s gas turbine engines made fromgas turbine engines made from 1991 1991 until until 2008 2008

Market diagram of all UnitedMarket diagram of all United Engine Corporation’s Engine Corporation’s gas turbine engines made fromgas turbine engines made from 1991 1991 until until 2008 2008

6 MW(459)

8 MW(181)

10 MW(7)

25 MW(15)

4 MW(1)

6 MW(2)

10 MW(40)

12 MW(74)16 MW

(169)25 MW

(3)

4 MW(24)

6 MW(1)

1,25 MW(3)

16 MW(31) 10 MW

(4)

Total – 1014 units


Power class, MW

Manufacturer Type Power, MW Amount

3,51 – 5,0 UEC Saturn – Gas Turbines GPA-4RM 4,1 5

5,1 – 7,5 UECPerm Motors GTU-6PG 6,29 2

Saturn – Gas Turbines GPA-6,3RM 6,46 1

10,01 – 15,0 UEC

Perm Motors GTU-10P 10,26 3

Saturn – Gas Turbines GPA-10RM 10,16 2

Perm MotorsGTU-12P 12,4 14

15,01 – 20,0 UEC

Perm Motors GTU-16P 16,44 10

Ufa Engine Industrial Association, Motor AL-31STN 16,8 7

All UnitedAll United Engine Corporation’s gas Engine Corporation’s gas turbine engines made inturbine engines made in 200 2007 for CIS7 for CISAll UnitedAll United Engine Corporation’s gas Engine Corporation’s gas

turbine engines made inturbine engines made in 200 2007 for CIS7 for CIS

Total 44


All UnitedAll United Engine Corporation’s gas turbine Engine Corporation’s gas turbine engines engines at global market

All UnitedAll United Engine Corporation’s gas turbine Engine Corporation’s gas turbine engines engines at global market

1.01 - 2.0 3 2.01 - 3.5 2 3.51 - 5.00 2 5.01 - 7.50 12 7.51 - 10.00 18 10.01 - 15.00 34 15.01 - 20.00 26 20.01 - 30.00 132 30.01 - 60.00 23 60.01 - 120.00 - 120.01 - 180.00 -

180.01 plus -Total 252

Power class, MW Amount

The amount of United Engine Corporation’s The amount of United Engine Corporation’s engines for pipelines in other countries is 252*engines for pipelines in other countries is 252*

The global market share of United Engine The global market share of United Engine Corporation’s engines for pipelines isCorporation’s engines for pipelines is ~~ 17,5% 17,5%

The amount of United Engine Corporation’s The amount of United Engine Corporation’s engines for pipelines in other countries is 252*engines for pipelines in other countries is 252*

The global market share of United Engine The global market share of United Engine Corporation’s engines for pipelines isCorporation’s engines for pipelines is ~~ 17,5% 17,5%

* Diesel & Gas Turbine WorldWide


Main gas pipelines: «South Stream»Main gas pipelines: «South Stream»

УПРАВЛЯЮЩАЯ КОМПАНИЯ moscow 2010. УПРАВЛЯЮЩАЯ КОМПАНИЯ all gas...

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