scholarly journals The Orlando Gas Turbines

Author(s):  
C. H. Stanton ◽  
H. C. Luff

In 1958, The Orlando Utilities Commission installed two gas turbines for peaking and standby service. These units were then the largest simple-cycle gas turbines in the United States and among the largest anywhere, Fig. 1. The operating and maintenance experience with these units should be of interest to other users and potential users of large simple-cycle gas turbines.

Author(s):  
John Hartranft ◽  
Bruce Thompson ◽  
Dan Groghan

Following the successful development of aircraft jet engines during World War II (WWII), the United States Navy began exploring the advantages of gas turbine engines for ship and boat propulsion. Early development soon focused on aircraft derivative (aero derivative) gas turbines for use in the United States Navy (USN) Fleet rather than engines developed specifically for marine and industrial applications due to poor results from a few of the early marine and industrial developments. Some of the new commercial jet engine powered aircraft that had emerged at the time were the Boeing 707 and the Douglas DC-8. It was from these early aircraft engine successes (both commercial and military) that engine cores such as the JT4-FT4 and others became available for USN ship and boat programs. The task of adapting the jet engine to the marine environment turned out to be a substantial task because USN ships were operated in a completely different environment than that of aircraft which caused different forms of turbine corrosion than that seen in aircraft jet engines. Furthermore, shipboard engines were expected to perform tens of thousands of hours before overhaul compared with a few thousand hours mean time between overhaul usually experienced in aircraft applications. To address the concerns of shipboard applications, standards were created for marine gas turbine shipboard qualification and installation. One of those standards was the development of a USN Standard Day for gas turbines. This paper addresses the topic of a Navy Standard Day as it relates to the introduction of marine gas turbines into the United States Navy Fleet and why it differs from other rating approaches. Lastly, this paper will address examples of issues encountered with early requirements and whether current requirements for the Navy Standard Day should be changed. Concerning other rating approaches, the paper will also address the issue of using an International Organization for Standardization, that is, an International Standard Day. It is important to address an ISO STD DAY because many original equipment manufacturers and commercial operators prefer to rate their aero derivative gas turbines based on an ISO STD DAY with no losses. The argument is that the ISO approach fully utilizes the power capability of the engine. This paper will discuss the advantages and disadvantages of the ISO STD DAY approach and how the USN STD DAY approach has benefitted the USN. For the future, with the advance of engine controllers and electronics, utilizing some of the features of an ISO STD DAY approach may be possible while maintaining the advantages of the USN STD DAY.


Author(s):  
Karen A. Walder ◽  
Steven D’Alessio

Demand for power in the United States is projected to increase between 2 and 4 percent per year for the next 10 years based on various studies. At the same time, the rise in environmental regulatory restrictions has made it increasingly difficult and expensive for utilities to meet these growing power demands with traditional power sources. During the 1960’s and 70’s hundreds of gas turbine electric generating units were installed in the United States. Many are now approaching the end of their useful economic lives owing to increased maintenance and fuel costs. With the major advances in both fuel efficiency and exhaust gas emission quality power producers are looking toward the repowering of existing plants with modern gas turbines such as the FT8. (Day and Koehler, 1988) This paper describes the design of Turbo Power and Marine Systems’ (Turbo Power) FT8® repowering package for the present FT4 powered plant at Public Service Electric and Gas Company’s (PSE&G) Burlington Generating Station. Given the objectives of minimum design effort and minimum field construction time, the retrofit package provides an optimal blending of existing FT4 and standard FT8 equipment. Performance, impact on operation, reliability, and availability of the FT8 industrial gas turbine were also important considerations in the retrofit design.


Author(s):  
Justin Zachary

Since 1998, the United States has experienced a tremendous increase in power generation projects using gas turbine technology. By burning natural gas as the primary fuel and low sulfur oil as a back-up fuel, gas turbines are the cleanest form of fossil power generation.


Author(s):  
D. E. Ridley ◽  
R. C. Case

United States seapower in the 70’s is synonymous with a new class of destroyers developed to maintain America’s strength on the world’s seas. When the DD963 joins the fleet in 1974, she will be unlike any destroyer ever to fly the United States flag. She will be bigger, faster, and more sophisticated. As a vital part of the main propulsion plant of this ship, controllable pitch propellers were used in conjunction with marine gas turbines. This paper addresses the description and operation of the CP propellers, and various improvements in the “state of the art” of propeller design and manufacture which have been incorporated in the ship.


Author(s):  
Jeffrey A. Benoit

Increasingly restrictive emission regulations for gas turbines are driving key technology decisions across the United States and Europe. For example, in Texas, United States, regulations are forcing permit holders in certain non-attainment areas to ratchet down industrial oxides of nitrogen (NOx) emission levels by over 80% by 2008. Improvements today in the technology of lean pre-mix combustion for gas turbines can result in reduction of NOx and carbon monoxide (CO) emissions to ultra-low levels without using Selective Catalytic Reduction (SCR’s) or Oxidation Catalysts (OCAT’s); and often provides the end user with the most cost effective solution to addressing these requirements. This paper describes the demonstrated current field performance of a dry, lean-premixed combustion system developed for direct replacement in MS7E/EA gas turbines previously configured with either the OEM’s DLN-1 combustion system or converted from a standard diffusion combustion system. The LEC-III® combustion system, developed by Power Systems Mfg. LLC (PSM), owned by Alstom, has proven sub-4ppm NOx and single digit CO emissions levels over the entire premix load operating range with natural gas fuel, from full load down to below 55% of full load conditions in customer machines. A recent conversion effort completed by PSM in 2006 & 2007 now has five gas turbines currently operating at a Texas industrial power producer operating at below 4ppm NOx with the LEC-III system. The conversion scope will also be detailed. Dynamic pressure sensing instrumentation was installed on each combustion chamber to measure and record combustion dynamic oscillations or “noise” to optimize fuel splits within each combustor. Rugged construction and performance optimization enable the dynamics to be maintained within acceptable limits to ensure extended service intervals of over 16,000 equivalent fired hours. Detailed field-installed emissions results are provided for this Frame 7E/EA LEC-III site. Finally an overview of PSM’s Combustion Technology Roadmap (CTR) will be discussed, which leverages their high-pressure, high-airflow test rig to evaluate technology improves with the objective of achieving guaranteed LEC-III combustion system NOx emissions below 3ppm NOx with low levels of CO.


Author(s):  
Barry Davidson ◽  
Dan Whitney ◽  
Niels Laursen ◽  
Art Cohn ◽  
George A. Hay

This paper describes the status of the Collaborative Advanced Gas Turbine (CAGT) Program’s initiative to commercialize interCooled AeroDerivative gas turbine (ICAD) technology. CAGT is a consortium of domestic and international electric companies, gas companies and research organizations. ICAD gas turbine technology was selected by CAGT member companies and potential suppliers in a competitive $5 million screening study of various advanced gas turbine options in the 1992–94 time frame. Efforts to commercialize ICAD began in 1994–95. The most attractive ICAD gas turbine options were based on high thrust engines produced by General Electric. Pratt & Whitney and Rolls Royce aircraft divisions. Simple cycle ICAD represents a new intermediate load gas turbine product class with costs and performance unlike any other product available today. Simple cycle efficiencies will approach Chose of many operating combined cycles, but with the low capital costs and rapid start times of a peaking gas turbine. ICAD simple cycle units would be in the 100–130 MW size range with efficiencies in the range of 45–48% + LHV and combined cycle efficiencies potentially as high as 60% + LHV. All efficiencies are presented in the paper in lower heating value (LHV). ICAD gas turbines will eddress a wide range of simple cycle, cogeneration. innovative repowering, combined cycle, distributed generation and renewable energy applications. CAGT members have several projects underway with the goal of the first ICAD unit to begin operation before the year 2000. Industry restructuring has reduced near-term demand for new generation in the United States with a corresponding drop in gas turbine prices. Given the large development cost for any new gas turbine product, potential ICAD suppliers have indicated the need for a launch order to proceed with development. CAGT is pursuing a number of project development and strategic alliance strategies globally to organize a launch order in the range of 10–15 projects. Efforts are also underway to examine options for demonstrating ICAD on a smaller scale (Small ICAD or SICAD) which would address the emerging market for distributed generation. CAGT members feel the low costs and flexibility offered by ICAD could be a significant source of competitive advantage in restructuring electric markets. CAGT members invite others to join the program.


1955 ◽  
Vol 59 (530) ◽  
pp. 127-150 ◽  
Author(s):  
J. L. Edwards

Some five years ago the author was privileged to deliver a Section Lecture to the Royal Aeronautical Society on the subject of reheat. The present paper attempts to summarise the problems which now arise and to give some idea of the progress which has been made in the intervening years.In 1949, reheat was in its infancy in Great Britain. A certain amount of progress had been made in the United States but the information from that source was scanty and vague. Tests at the National Gas Turbine Establishment (N.G.T.E.) had given some engine data but this was in the nature of preliminary information only and was by no means complete. In fact the majority of the problems which now beset us were then completely unknown or were considered unimportant. The N.G.T.E. work was valuable, however, in that it demonstrated the practicability of reheat, although at the time the comments of many who saw this and other schemes in operation were somewhat sceptical and definitely unflattering.


Author(s):  
E. G. Barry ◽  
S. P. Cauley

The use of heavy distillates in gas turbines used for electric power generation is expected to increase in the United States and special analytical procedures have been developed to assist in evaluating the handling characteristics of these fuels. Data obtained on wax melting temperatures, and energy required, for a number of different heavy distillate fuels are presented. Special hot filtration method for measuring non-wax fuel sediment is also described.


Author(s):  
Blace C. Albert ◽  
A. O¨zer Arnas

The mission of the United States Military Academy (USMA) is “To educate, train, and inspire the Corps of Cadets so that each graduate is a commissioned leader of character committed to the values of Duty, Honor, Country; professional growth throughout a career as an officer in the United States Army; and a lifetime of selfless service to the nation.” [1] In order to accomplish this mission, USMA puts their cadets through a 47-month program that includes a variety of military training, and college courses totaling about 150 credit-hours. Upon completion of the program, cadets receive a Bachelor of Science degree and become Second Lieutenants in the United States Army. A very unique aspect of the academic program at USMA is that each cadet is required to take a minimum of five engineering classes regardless of their major or field of study. This means that about 500 cadets will have taken the one-semester course in thermodynamics. The thermodynamics course taught at USMA is different from others throughout the country because within every class there is a mixture of cadets majoring in engineering and those that are in other majors, i.e. languages, history [2]. Topics on gas turbine machinery have been integrated into this unique thermodynamics course. Because the cadets will encounter gas turbines throughout their service in the Army, we feel that it is important for all of the students, not just engineering majors, to learn about gas turbines, their operation, and their applications. This is accomplished by four methods. The first is in a classroom environment. Cadets learn how actual gas turbines work, how to model them, and learn how to solve problems. Thermodynamics instructors have access to several actual gas turbines used in military applications to aid in cadet learning. The second method occurs in the laboratory where cadets take measurements and analyze an operational auxiliary power unit (APU) from an Army helicopter. The third method occurs in the form of a design project. The engineering majors redesign the cogeneration plant that exists here at West Point. Many of them use a topping cycle in this design. The final method is a capstone design project. During the 2001–02 academic year, three cadets are improving the thermodynamic laboratories. Among their tasks are designing a new test stand for the APU, increasing the benefit of the gas turbine laboratory through more student interaction, and designing a web-based gas turbine pre-laboratory instruction to compliment the actual laboratory exercise.


1984 ◽  
Vol 106 (4) ◽  
pp. 825-832 ◽  
Author(s):  
M. B. Hilt ◽  
J. Waslo

The role played by oxides of nitrogen in the formation of photochemical smog has been known for many years. However, because of the relatively small fraction of power generated by gas turbines, there were no significant attempts at limiting gas turbine NOx emissions in the United States until about 15 years ago. This paper outlines General Electric’s experience with NOx abatement techniques from then until the present.


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