ASME 1956 Gas Turbine Power Conference
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Published By American Society Of Mechanical Engineers

9780791879993

Author(s):  
A. H. Carameros

A summary of El Paso Natural Gas Company’s operating experience covering design and operating problems encountered during the period between September, 1952, to January, 1956. Some discussion on operating and maintenance costs is also offered.


Author(s):  
S. H. DeWitt ◽  
W. B. Boyum

An Internally fired semi-closed cycle gas turbine for Naval propulsion was designed and built for the U.S. Navy by the Westinghouse Electric Corporation. Due to a revision of the overall Navy propulsion program the plant was not tested at design conditions or mode of operation, but feasibility information for this configuration of gas turbine plant was obtained. Plant tests indicated that this cycle configuration can be expected to attain a significant reduction in shipboard space and weight requirements while matching existing conventional propulsion plant fuel and air consumption rates over a wide load range. The plant further is simply controlled to minimize manning personnel, permit bridge control, and has a brief transient period from cruise power to full load. Plants of this cycle configuration can be expected to produce large powers such as required for main ship propulsion while employing components of the size where considerable industrial experience has been accumulated. Fouling and corrosion of the internally fired, semi-closed cycle gas turbine were evaluated by the tests. Conventional gas turbine components are satisfactory for low sulfur fuel operation, and with additional precooler equipment development it is expected that high sulfur fuel operation will be achieved.


Author(s):  
Curt Keller

This paper is the author’s third progress report in the USA on the AK-closed cycle gas turbine.


Author(s):  
L. D. Stoughton ◽  
T. V. Sheehan

A nuclear power plant is proposed which combines the advantages of a liquid metal fueled reactor with those inherent in a closed cycle gas turbine. The reactor fuel is a solution of uranium in molten bismuth which allows for unlimited burn-up with continuous fuel make-up and processing. The fuel can either be contained in a graphite core structure or circulated through an external heat exchanger. The cycle working fluid is an inert gas which is heated by the reactor fuel before entering the turbine. A 15 MW closed cycle gas turbine system is shown to illustrate the application of this reactor.


Author(s):  
F. O. Hennig

This paper is a continuation of a previously presented paper, which described the over-all design of the major components of a mobile power unit. The present paper is concerned with the main power equipment only and offers a detailed description of the design features which were developed for this project and also provide the flexibility necessary to make this gas turbine suitable for other applications.


Author(s):  
W. E. Hammond ◽  
T. C. Evans

To exploit the regenerative gas-turbine cycle to the fullest possible extent requires an extremely high degree of heat exchange. Presently, the rotary heat exchanger is the only type which can be designed with the high thermal effectiveness necessary and yet remain practical from a size and cost standpoint. The mechanical nature of the rotary heat exchanger is such, however, that some leakage of high-pressure fluid to the low-pressure side will always occur. The fact that in the past this leakage could not be held to workable values has prevented commercial acceptance of this type unit. Consequently, The Air Preheater Corporation set up an intensive program aimed at developing an acceptable sealing means which would remove this one objection to an otherwise highly desirable piece of equipment. While this development program, at time of writing, is far from complete, results to-date have indicated that sealing of the rotary design can be accomplished, and based on quantity production, costs of a turbine plant equipped with a rotary heat exchanger would be attractive commercially. Included in the development program was the design and construction of a prototype unit for a 3000 hp turbine plant. While erection of the prototype unit is complete, no testing has been done at time of writing. The purpose of this paper is to emphasize the advantages of the regenerative cycle, generally, and more specifically, to show why the rotary type is most promising, particularly in the high effectiveness range. In addition, certain data pertaining to the design of the prototype unit are also presented. A future report will present results obtained from the prototype test program.


Author(s):  
W. M. M. Fowden ◽  
J. W. Sawyer

After some 33,000 hr of operating experience on marine gas turbines in naval vessels, it is believed that this prime mover has well demonstrated its reliability, its long-range economy, ease of operation, and quick replacement. Based on this experience, naval applications of marine gas turbine are expected to show a further increase in the immediate future. The gas turbine is now a strong contender in many fields and is being selected on the basis that it is able to do a better job than its nearest competitor.


Author(s):  
K. Leist

For several years past, the research staff of the Institute for Turbomachines of the Aachen Technical University has carried out measurements on rotating turbine blading. This program is part of a comprehensive effort directed toward the experimental investigation of the three-dimensional flow through axial-flow turbomachines.


Author(s):  
N. R. Balling ◽  
V. W. van Ornum

The objective of the research and development program reported by this paper was to decrease the specific fuel consumption of a small gas-turbine engine by means of an increase in pressure ratio alone. Development of a centrifugal compressor is presented, with a general description of equipment, methods, and special problems met during the tests. Results showed the required decrease in specific fuel consumption and pointed up the advantages of a straightforward development program.


Author(s):  
J. C. Miles ◽  
N. A. Parker ◽  
R. L. Smoot

Test performance of a rotary regenerator comprising the experimental evaluation of three lengths of flame-trap -type matrices is presented. Design parameters based on the experimental results are given. A compact structural design of a rotary regenerator is illustrated along with a configuration for a proposed application to small turbines. A seal design is suggested and the problem of matrix fouling is discussed.


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