Paper 9: Operating Experience of Three Gas Turbines of Less than 1000kw Each

1963 ◽  
Vol 178 (11) ◽  
pp. 116-124
Author(s):  
W. C. Vickers
Keyword(s):  
Gas Turbines ◽  
Operating Experience

scholarly journals Gas Turbines for the Chemical Industry

1957 ◽  
Author(s):  
Z. Stanley Stys
Keyword(s):  
Nitric Acid ◽  
Gas Turbine ◽  
Chemical Industry ◽  
Gas Turbines ◽  
Operating Experience ◽  
And Performance ◽  
Design Construction

Application of the gas turbine in nitric-acid plants appears attractive. Several of these units have been installed recently in this country and performance and operating experience already have been gained. Design, construction, and layout of “package” units for this particular process are described.

Vent Gas Collection From Gas Compressor Dry Gas Seals

2004 ◽  
Author(s):  
Ari Suomilammi
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Operating Experience ◽  
Methane Emissions ◽  
Emissions Reduction ◽  
Transmission Pipeline ◽  
Reduce Emissions ◽  
Gas Seals ◽  
National Programs ◽  
Year 2000

Gasum is an importer of natural gas and is operating and maintaining the Finnish transmission pipeline in which the pressure is maintained with three compressor stations. Gasum’s compressor stations are unmanned and remotely controlled from the central control room. Some of the compressor units are equipped with dry gas seals. The otherwise satisfactory operation of dry gas seals has the disadvantage of methane emissions. Reduction of methane emissions has been stated as a target by international auspices of the Kyoto Protocol or through national programs seeking to reduce emissions. The application described in this paper to collect vent gases from the dry gas seals was installed into four of the compressor units during 2001. The compressors are centrifugal compressors: two of them are Nuovo Pignone PCL603 with PGT10DLE (10 MW) gas turbine and two are Demag DeLaval 2B-18/18 with Siemens Tornado gas turbines (6,5 MW). It is normal for dry gas seals to have a small leakage of gas through the seals due to the function principle and required cooling of the seals. This gas emitted from the seals is normally about of 5...10nm3/h per one compressor unit during operation and during the stand-still the leakage is almost zero. In the year 2000 the total amount of emitted gas in Gasum’s units was about 50.000 nm3 per four compressor units. The target was to find an efficient method to collect the dry gas seal vent gas and utilize it. The solution must be simple and its investment costs must be feasible. Injection of the vent gases to the gas turbine inlet air flow was selected as a solution among some alternatives. The operating experience so far has been several thousands of operating hours without any malfunctions. The amount of collected gas by this system has been in the range of 80.000 nm3 per annum. The total cost of the system for four compressor units was about 85.000€. The intention of this paper is not to describe any scientific approach to the issue but to present a practical solution with operating experience.

COGOG Propulsion Installations in Guided Missile and Standard Class Frigates of the Royal Netherlands Navy: A Review of the Development From the Specific Design Philosophies to the Actual Technical, Personnel and Maintenance/Logistic Management in Service

1977 ◽  
Author(s):  
P. van Staalduinen
Keyword(s):  
Gas Turbines ◽  
Operating Experience ◽  
Electronic Control ◽  
Specific Design ◽  
Recording Equipment ◽  
Overall Design ◽  
Logistic Management ◽  
Electronic Control System ◽  
State Surveillance ◽  
Logistic Support

This paper gives a brief survey of the overall design philosophies of the Olympus/Tyne twin shaft propulsion plants in the unmanned engine rooms of the Guided Missiles and Standard class frigates of the Royal Netherlands Navy, including the installation’s major auxiliaries, electronic control system, solid state surveillance and data recording equipment Complimentary to this paper is the paper by J. B. Kerpestein of Royal Schelde entitled, “Propulsion Gearing Transmission Systems for Guided Missile and Standard Frigates of the Royal Netherlands Navy” (ASME Paper No. 77-GT-67). The author further outlines briefly current ship operating experience and the reorganization undertaken by the RNN to satisfy the requirements for personnel training and technical and logistic support of the gas turbines.

20 Years Experience Burning Heavy Fuels in Heavy Duty Gas Turbines

1973 ◽  
Author(s):  
A. O. White
Keyword(s):  
Gas Turbines ◽  
Processing System ◽  
Operating Experience ◽  
Field Tests ◽  
Early Experience ◽  
Liquid Fuels ◽  
Heavy Duty ◽  
Fuel Processing ◽  
Wide Range ◽  
Heavy Fuels

This paper covers the early experience of the author’s company in burning residual oils in their gas turbines and the problems that occurred. The laboratory invesgations and field tests that resulted in a fuel processing system that permitted satisfactory operation on a wide range of liquid fuels are described. The operating experiences, where residual fuels were successfully burned in a large number of units, are described. The most recent operating experience with residual and crude oils and heavy distillates is also covered. A list of the various installations with dates and hours of operation is included and it is concluded that heavy duty gas turbines burning heavy fuels will be established as the up-to-date source of economical power in many applications.

Packaging of Gas Turbines Type 7 and Type S 7

1976 ◽  
Author(s):  
F. Porchet
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Main Part ◽  
Operating Experience ◽  
Auxiliary System ◽  
Positive Experience ◽  
Comprehensive Description

A few years ago, Sulzer introduced two new gas turbines to the market, namely the 9-MW single-shaft type 7 and split-shaft type S 7 machines. Twenty-six units have been delivered to date, and over 100,000 field operating hours accumulated. The positive experience with this machine has allowed an uprating to 10 MW. Changes in the structure of the market, particularly the importance of platform installations, have caused Sulzer to redesign the machine’s auxiliaries, which have been, to a great extent, integrated into the gas turbine package. Flexibility in the application of the machine, easy maintainability, and ruggedness were maintained by reducing the required space to less than half the ground area. The main purpose of this paper is to describe the improved turbine of today. The prototype is briefly described and operating experience is listed. The main part of the paper is devoted to a comprehensive description of the redesigned gas turbine package and its new auxiliary system.

Repair of Advanced Gas Turbine Blades

2005 ◽  
Author(s):  
Julie McGraw ◽  
Reiner Anton ◽  
Christian Ba¨hr ◽  
Mary Chiozza
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
High Efficiency ◽  
High Reliability ◽  
Turbine Blades ◽  
Base Material ◽  
Operating Experience ◽  
Cost Effective ◽  
Directionally Solidified ◽  
Hot Gas

In order to promote high efficiency combined with high power output, reliability, and availability, Siemens advanced gas turbines are equipped with state-of-the-art turbine blades and hot gas path parts. These parts embody the latest developments in base materials (single crystal and directionally solidified), as well as complex cooling arrangements (round and shaped holes) and coating systems. A modern gas turbine blade (or other hot gas path part) is a duplex component consisting of base material and coating system. Planned recoating and repair intervals are established as part of the blade design. Advanced repair technologies are essential to allow cost-effective refurbishing while maintaining high reliability. This paper gives an overview of the operating experience and key technologies used to repair these parts.

Operating Experience With the Latest Upgrade of Alstom’s Sequential Combustion GT26 Gas Turbine

2010 ◽  
Author(s):  
Matthias Hiddeman ◽  
Peter Marx
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Operating Experience ◽  
Business Case ◽  
Combined Cycle ◽  
Fuel Gas ◽  
Power Generators ◽  
Additional Degree ◽  
Performance Improvements ◽  
Main Driver

The GT26 gas turbine provides an additional degree of flexibility as the engine operates at high efficiencies from part load to full load while still maintaining low NOx emissions. The sequential combustion, with the EV burner as the basis for this flexibility also extends to the ability to handle wide fluctuations in fuel gas compositions. Increased mass flow was the main driver for the latest GT26 upgrade, resulting in substantial performance improvements. In order to ensure high levels of reliability and availability Alstom followed their philosophy of evolutionary steps to continuously develop their gas turbines. A total of 47 engines of this upgrade of the GT26 gas turbine have been ordered worldwide to date (Status: January 2010) enhancing the business case of power generators by delivering superior operational and fuel flexibility and combined cycle efficiencies up to and beyond 59%.

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