scholarly journals Operating Experience With Gas-Turbine Ships of the Maritime Administration

Author(s):  
C. C. Tangerini ◽  
D. H. Specht

The two year operating results of the open cycle-gas turbine propulsion plant in the John Sergeant are given with reference to the actual performance, economy, and durability of the components of this marine drive. The operational records show that this type engine can compete favorably with conventional propulsion systems. Similarly, the operating results of the free piston gas-turbine propulsion plant in the William Patterson are given with limited operational experience at this time. The free-piston-installation operating record is submitted as preliminary.

Author(s):  
F. K. Konig

The author states the basic philosophy for the installation of gas turbines burning blast-furnace gas in the power-generating systems of an iron and steel works. A description is given of the two gas-turbine generators at the Huttenwerk Rheinhausen, A.G. and their operating experience.


1959 ◽  
Vol 81 (3) ◽  
pp. 311-339
Author(s):  
John W. Sawyer ◽  
Harry M. Simpson

This is a progress report on the marine gas turbine and free-piston gas turbine during the 5-yr period, 1953–1957. Since the merchant and naval services encompass many similar operating conditions—in spite of many differing requirements—the entire marine field will be reviewed in a single paper. In the first report [18], separate papers appeared on marine, merchant, and naval applications. Open and closed-cycle gas-turbine, nuclear gas-turbine, and free-piston gas-turbine prime movers will be discussed along the following lines: Applications, operating experience, development, advantages, disadvantages, economics, and the future potential in the marine field.


Author(s):  
Massimo Maggini ◽  
Roberto Tonelli

The LM2500 gas turbine has been used in Italian Navy (ITN) ships for more than twenty years, as the first engines were installed on board the “Lupo” class Frigates during the second half of the 1970s. The LM2500 during its service has proven to be reliable in both the “Combined Diesel or Gas” (CODOG) and the “Combined Gas and Gas” (COGAG) propulsion plant, with Controllable Pitch Propeller (CPP) and Fixed Pitch Propeller (FPP) as the ITN marine operational experience demonstrates. The last application was in the DURAND DE LA PENNE Class DDG with a CODOG arrangement and two shaft lines with Feathered Controllable Pitch Propellers (FCPP), produced by FINCANTIERI shipyard, which may range from a forward to an astern direction till the blades reach a flag position. This type of propeller allows a considerable drop in the absorbed power and therefore in fuel consumption and noise when using a single shaft. Based on the ITN experience with the DDG class, the use of FCPP achieves remarkable fuel savings with the gas turbine since, due to the high specific consumption of the engine at low speeds, it is cheaper to have a single shaft running. The maintenance approach to the engines installed on board ITN ships, based on the “on condition” concept, has been developed by the ITN and Fiat Avio to maximise the availability of the vessels. This covers both on-board corrective maintenance (inspection, special maintenance and / or introduction of improvements) and the substitution maintenance, with successive overhaul and application of decided updating of gas generators and power turbines.


1975 ◽  
Author(s):  
K. Davies ◽  
I. Brannam ◽  
G. L. Amundrud

The four destroyers of the Canadian Armed Forces DDH 280 Class have, since commissioning, accumulated a diverse spectrum of operational experience in widely varied geographical theatres ranging from the Tropics to the Arctic and from the Western Atlantic to the Mediterranean. A technical narrative is presented that confirms the original decision to opt for gas turbine propulsion and discusses some of the more significant problems encountered. Areas are highlighted where further system and component development is necessary in the DDH 280 Class in order to maximize the advantages of the aero-derivative gas turbines as a prime mover in our Naval Ships.


Author(s):  
Federico Bonzani ◽  
Andrea Silingardi ◽  
Laura Traversone ◽  
Luigi Di Pasquale

The growth of power markets stresses the importance of optimizing power plant performance and boosts the need to improve and upgrade the existing power generation plants. In this framework, Gas Turbine with medium power output are regarded as strategic asset to gain competitiveness in energy business. In such a challenging scenario, the current version of the 50/60 cycles AE64.3A Gas Turbine has been upgraded by Ansaldo Energia, enhancing performances, operational and dynamic features. Therefore the unit is rated now 75 Mwe power output and 35.9% efficiency. The upgraded AE64.3A along with the relevant generator and auxiliary systems in single shaft configuration, has been installed in the combined cycle generation plant of Vlore, on the Adriatic coast of Albania. The gas turbine has been supplied in accordance to the standard and proven design of the manufacturer, optimizing the need for burning fuel oil in continuous operation. The paper will report the main feature of the engine highlighting the upgrade and present the operational experience gained during the commissioning phase.


Author(s):  
S. Comassar ◽  
F. B. Lash

The Spruance (DD-963) Class destroyers are the first all-gas turbine powered combatant ships in the US Navy. The first of the 30-ship class entered Navy operational service in September 1975. This paper presents the operational experience of the LM2500 Gas Turbines and the propulsion system from that time to the present. It includes experience obtained from all Spruance class destroyers now and soon-to-be commissioned.


Author(s):  
Ennio Macchi ◽  
Aurelio Poggio

The idea of re-injecting into a gas turbine cycle the steam generated by the heat recovery steam generator (HRSG) is a well-established practice, especially in small-medium size cogeneration plants operating under variable heat demand. Power augmentation, electrical efficiency increase, NOx reduction and operating flexibility are the most obvious advantages brought about by steam injection. On the other hand, the discharge to the ambient of the injected steam has two major drawbacks: (i) a relevant water consumption and (ii) the large thermal loss related to the latent heat of steam. The addition of a recuperator downstream of the HRSG, whereby steam condensation takes place, can solve both problems, by achieving very high first-law efficiencies (over 100%, if reference is made to the lower heating value) and the integral recovery of water. The present paper describes the design philosophy and the operational experience of a cogeneration plant where such a condensation is accomplished. To the Authors’s knowledge, it is the first time in the world that this is achieved with gas turbine exhausts. The plant is located inside the “CARROZZERIA BERTONE”, a car manufacturing factory near Turin, Italy. It was designed to fulfill all the energy needs of the factory: it supplies all the electricity, steam and hot water required by the industrial process and during peaking hours, sells excess electricity to the national grid, at special increased tariffs offered to energy-saving plants in Italy. The plant erection (including the recuperator/condenser) was completed in December 1992; commercial operation began in February 1993.


2020 ◽  
Vol 11 (1) ◽  
pp. 28
Author(s):  
Emmanuel O. Osigwe ◽  
Arnold Gad-Briggs ◽  
Theoklis Nikolaidis

When selecting a design for an unmanned aerial vehicle, the choice of the propulsion system is vital in terms of mission requirements, sustainability, usability, noise, controllability, reliability and technology readiness level (TRL). This study analyses the various propulsion systems used in unmanned aerial vehicles (UAVs), paying particular focus on the closed-cycle propulsion systems. The study also investigates the feasibility of using helium closed-cycle gas turbines for UAV propulsion, highlighting the merits and demerits of helium closed-cycle gas turbines. Some of the advantages mentioned include high payload, low noise and high altitude mission ability; while the major drawbacks include a heat sink, nuclear hazard radiation and the shield weight. A preliminary assessment of the cycle showed that a pressure ratio of 4, turbine entry temperature (TET) of 800 °C and mass flow of 50 kg/s could be used to achieve a lightweight helium closed-cycle gas turbine design for UAV mission considering component design constraints.


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