Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery 1982
DOI: 10.1115/82-gt-306
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Regenerated Marine Gas Turbines: Part I — Cycle Selection and Performance Estimation

Abstract: Analytical studies are currently being conducted by the David Taylor Naval Ship R&D Center to assess the suitability of regenerative-cycle and intercooled, regenerative-cycle gas turbines for naval applications. This paper, which is presented in two parts, discusses results of initial investigations to identify attractive engine concepts based on existing turbomachinery and to consider the regenerator technology required to develop these engine concepts. Part I of the paper deals with the attractive engine… Show more

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Cited by 4 publications
(6 citation statements)
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“…The design point performance of both the simple-cycle and ICR 50,000 HP marine gas turbines are estimated using a thermodynamic cycle analysis computer model which uses basic thermodynamic relationships to compute the work across each component of the gas turbine. Cycle parameters for the analysis are based on current marine gas turbines [3] and on actual capabilities of in-production 50,000 HP engines [4]. Table 1 shows the input values used for the 50,000 HP simple cycle and ICR marine engines.…”
Section: Performancementioning
confidence: 99%
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“…The design point performance of both the simple-cycle and ICR 50,000 HP marine gas turbines are estimated using a thermodynamic cycle analysis computer model which uses basic thermodynamic relationships to compute the work across each component of the gas turbine. Cycle parameters for the analysis are based on current marine gas turbines [3] and on actual capabilities of in-production 50,000 HP engines [4]. Table 1 shows the input values used for the 50,000 HP simple cycle and ICR marine engines.…”
Section: Performancementioning
confidence: 99%
“…The generated SFC versus HP curve is shown in Figure 2. For the 50,000 HP ICR gas turbine, an intercooler and recuperator are added to the 50,000 HP simple cycle base engine using the effectiveness and pressure losses assumed in reference [3]. Heat exchanger relationships are added to the 50,000 HP simple cycle thermodynamic computer program to compute the performance of the ICR cycle at the design point.…”
Section: Performancementioning
confidence: 99%
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“…Figure 10 compares the performance of intercooled/ recuperated gas turbines and their simple cycle counterparts as a function of pressure ratio. The data of Figure 10 were taken (partially) from Reference (9), and apply to power systems in the 10,000-20,000 hp nominal range. These curves illustrate the substantial efficiency improvement resulting from using an intercooled and recuperated system, compared with a simple gas turbine unit.…”
Section: Gas Turbine System Enhancementsmentioning
confidence: 99%
“…An alternate approach to the far term engine is to pursue modifications to the simple cycle which include both intercooling and recuperation. Engines of this type are described by Bowen [25] as having significant performance advantages over the simple cycle and even greater advantages over a recuperated advanced cycle. Figure 3 shows a diagram of an intercooled regenerative cycle with a dual spool gas generator and free power turbine.…”
Section: Far Term Enginesmentioning
confidence: 99%