scholarly journals Development of low cost ceramic recuperator technology applicable to automotive gas turbine engines. Final report, April 1972--April 1977

1978 ◽  
Author(s):  
K.R. Kormanyos
Keyword(s):  
Gas Turbine ◽  
Low Cost ◽  
Turbine Engines ◽  
Final Report ◽  
Gas Turbine Engines ◽  
Ceramic Recuperator

Design, Development and Application of Vehicle Gas Turbine Engines

1966 ◽  
Vol 181 (1) ◽  
pp. 149-172
Author(s):  
P. A. Phillips ◽  
Peter Spear
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Low Cost ◽  
Engine Performance ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Design Development ◽  
Turbine Engine ◽  
Wide Range ◽  
Cycle Temperature

After briefly summarizing worldwide automotive gas turbine activity, the paper analyses the power plant requirements of a wide range of vehicle applications in order to formulate the design criteria for acceptable vehicle gas turbines. Ample data are available on the thermodynamic merits of various gas turbine cycles; however, the low cost of its piston engine competitor tends to eliminate all but the simplest cycles from vehicle gas turbine considerations. In order to improve the part load fuel economy, some complexity is inevitable, but this is limited to the addition of a glass ceramic regenerator in the 150 b.h.p. engine which is described in some detail. The alternative further complications necessary to achieve satisfactory vehicle response at various power/weight ratios are examined. Further improvement in engine performance will come by increasing the maximum cycle temperature. This can be achieved at lower cost by the extension of the use of ceramics. The paper is intended to stimulate the design application of the gas turbine engine.

Evaporative Cooling of Gas Turbine Engines

2013 ◽  
Vol 135 (8) ◽  
Author(s):  
Mustapha Chaker ◽  
Cyrus B. Meher-Homji
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Low Cost ◽  
Evaporative Cooling ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
End User ◽  
Very High ◽  
Improve Reliability ◽  
Selection Of

There are numerous gas turbine applications in power generation and mechanical drive service where power drop during the periods of high ambient temperature has a very detrimental effect on the production of power or process throughput. Several geographical locations experience very high temperatures with low coincident relative humidities. In such cases media evaporative cooling can be effectively applied as a low cost power augmentation technique. Several misconceptions exist regarding their applicability to evaporative cooling, the most prevalent being that they can only be applied in extremely dry regions. This paper provides a detailed treatment of media evaporative cooling, discussing aspects that would be of value to an end user, including selection of climatic design points, constructional features of evaporative coolers, thermodynamic aspects of its effect on gas turbines, and approaches to improve reliability. It is hoped that this paper will be of value to plant designers, engineering companies, and operating companies that are considering the use of media evaporative cooling.

Extreme Temperature Coatings for Future Gas Turbine Engines

2013 ◽  
Author(s):  
M. A. Alvin ◽  
B. Gleeson ◽  
K. Klotz ◽  
B. McMordie ◽  
B. Warnes ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Low Cost ◽  
Extreme Temperature ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Cyclic Testing ◽  
Barrier Coating ◽  
Regional University ◽  
Potential Use ◽  
External Coating

The National Energy Technology Laboratory-Regional University Alliance (NETL-RUA) has been developing extreme temperature coating systems that consist of a diffusion barrier coating (DBC), a low-cost wet slurry bond coat, a commercial yttria stabilized zirconia (YSZ) thermal barrier coating (TBC), and an extreme temperature external coating that are deposited along the surface of nickel-based superalloys and single crystal metal substrates. Thermal cyclic testing of these multi-layer coatings was conducted in steam-containing environments at temperatures ranging between 1100–1550°C. This paper discusses the response of these materials during bench-scale testing, and their potential use in advanced H- and J-class land-based gas turbine engines.

Generic, Low Cost, Aluminide Hot Section Coating for Gas Turbine Engines

1988 ◽  
Author(s):  
Dudley S. Engleby
Keyword(s):  
Gas Turbine ◽  
Low Cost ◽  
Turbine Engines ◽  
Gas Turbine Engines

Low Cost Electronically Controlled Fuel Metering System for Small Gas Turbine Engines

1999 ◽  
Author(s):  
S. S. Mohtasebi ◽  
H. Hong
Keyword(s):  
Gas Turbine ◽  
Low Cost ◽  
Turbine Engines ◽  
Gas Turbine Engines

NETL Research Efforts on Development and Integration of Advanced Material Systems and Airfoil Cooling Configurations for Future Land-Based Gas Turbine Engines

2014 ◽  
Author(s):  
M. A. Alvin ◽  
J. Klinger ◽  
B. McMordie ◽  
M. Chyu ◽  
S. Siw ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Film Cooling ◽  
Low Cost ◽  
Oxide Dispersion Strengthened ◽  
Advanced Materials ◽  
Turbine Engines ◽  
Internal Cooling ◽  
Gas Turbine Engines ◽  
Near Surface ◽  
Material Systems

As future land-based gas turbine engines are being designed to operate with inlet temperatures exceeding 1300°C (2370°F), efforts at NETL have been focused on developing advanced materials systems that are integrated with novel airfoil cooling architectures. Recent achievements in the areas of low cost diffusion bond coat systems applied to single- and poly-crystalline nickel-based superalloys, as well as development of thin nickel-based oxide dispersion strengthened layers are presented in this paper. Integration of these material systems with commercially cast, novel, pin-fin internal cooling airfoil arrays, tripod film cooling hole architectures, trailing edge cooling geometries, and near surface micro-channel concepts is also presented.

Evaporative Cooling of Gas Turbine Engines

2012 ◽  
Author(s):  
Mustapha Chaker ◽  
Cyrus B. Meher-Homji
Keyword(s):  
Gas Turbine ◽  
Gas Turbines ◽  
Low Cost ◽  
Evaporative Cooling ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
End User ◽  
Very High ◽  
Improve Reliability ◽  
Selection Of

There are numerous gas turbine applications in power generation and mechanical drive service where power drop during the periods of high ambient temperature has a very detrimental effect on the production of power or process throughput. Several geographical locations experience very high temperatures with low coincident relative humidities. In such cases media evaporative cooling can be effectively applied as a low cost power augmentation technique. Several misconceptions exist regarding their applicability of evaporative cooling the most prevalent being that they can only be applied in extremely dry regions. This paper provides a detailed treatment of media evaporative cooling, discussing aspects that would be of value to an end user including selection of climatic design points, constructional features of evaporative coolers, thermodynamic aspects of its effect on gas turbines and approaches to improve reliability. It is hoped that this paper will be of value to plant designers, engineering companies and operating companies that are considering the use of media evaporative cooling.

Evaporative Cooling of Gas Turbine Engines: Climatic Analysis and Application in High Humidity Regions

2007 ◽  
Author(s):  
Mustapha Chaker ◽  
Cyrus B. Meher-Homji
Keyword(s):  
Gas Turbine ◽  
Detrimental Effect ◽  
Low Cost ◽  
Evaporative Cooling ◽  
Turbine Engines ◽  
Climatic Data ◽  
High Humidity ◽  
Gas Turbine Engines ◽  
Ambient Temperatures ◽  
Augmentation Techniques

There are numerous power generation and mechanical drive gas turbine applications where the power drop caused by high ambient temperatures has a very detrimental effect on the production of power or process throughput. Media evaporative cooling and inlet fogging are common low cost power augmentation techniques applied to reduce these losses. Several misconceptions exist regarding the applicability of evaporative cooling to what are often called “high humidity” regions. There is a sizable evaporative cooling potential in most locations when climatic data is evaluated based on an analysis of coincident wet bulb and dry bulb data. This data is not readily available to plant users and designers. This paper provides a detailed treatment of available climatic data bases and presents actual climatic data from several world wide locations to show that considerable cooling potential actually exists even in high humidity regions. It is hoped that this paper will be of value to plant designers, engineering and operating companies that are considering the use of evaporative cooling for power augmentation.

Extreme Temperature Coatings for Future Gas Turbine Engines

2014 ◽  
Vol 136 (11) ◽  
Author(s):  
M. A. Alvin ◽  
K. Klotz ◽  
B. McMordie ◽  
D. Zhu ◽  
B. Gleeson ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Low Cost ◽  
Extreme Temperature ◽  
Turbine Engines ◽  
Multilayer Coatings ◽  
Gas Turbine Engines ◽  
Barrier Coating ◽  
Regional University ◽  
Potential Use ◽  
External Coating

The National Energy Technology Laboratory-Regional University Alliance (NETL-RUA) has been developing extreme temperature coating systems that consist of a diffusion barrier coating (DBC), a low-cost wet slurry bond coat, a commercial yttria stabilized zirconia (YSZ) thermal barrier coating (TBC), and an extreme temperature external coating that are deposited along the surface of nickel-based superalloys and single crystal metal substrates. Thermal cyclic testing of these multilayer coatings was conducted in steam-containing environments at temperatures ranging between 1100 and 1550 °C. This paper discusses the response of these materials during bench-scale testing, and their potential use in advanced H- and J-class land-based gas turbine engines.

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