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Gas Turbine Engines: Fundamentals
2012The gas turbine engine and its conventional variants (turbojet, turbofan, turboprop, and turboshaft) provide an effective means for thrust and power delivery for a wide number of atmospheric flight applications. In this chapter, the design and performance analysis of gas turbine engines will be introduced, with the turbojet engine as the primary focus (
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Stochastic Gas Turbine Engine Models
2004Previous chapters gave an overview of conventional methods for modelling of gas turbines for control purposes. This chapter provides basics of stochastic modelling using controllable Markov chain techniques. Accounting for stochastic properties is essential for engine modelling at system test facilities, where the real-life environment is simulated. In
Gennady G. Kulikov, Haydn A. Thompson
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Cogeneration with gas turbine engines
Heat Recovery Systems and CHP, 1993Abstract Cogeneration, simply, is the generation of energy for one process from the excess energy supplied to another process. Cogeneration, then, is nothing more than an economically sound method for the conservation of resources [1]. Thus, the benefits from the use of cogeneration may be cited as energy conservation, environmental improvement and ...
Y.S.H. Najjar +3 more
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Gas Turbine Engine Application
Gas turbine engines are critical to the aviation industry, yet their intricate design, operation, and maintenance pose significant challenges for engineers and technicians to master. Traditional educational approaches often fall short in effectively conveying the dynamic principles and components of these complex machines.Amaluddin Muhamad +5 more
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1981
The performance parameters of a running gas turbine are determined at any time by a unique set of curves, such as those in figure 4.2. Of all the parameters shown, it is the fuel flow which is the input and which controls the operation.
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The performance parameters of a running gas turbine are determined at any time by a unique set of curves, such as those in figure 4.2. Of all the parameters shown, it is the fuel flow which is the input and which controls the operation.
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Gas Turbine Engine Corrosion Control
SAE Technical Paper Series, 1964<div class="htmlview paragraph">The challenge of preventing corrosion of gas turbine engines, with emphasis on military aircraft engines in marine atmospheres, is discussed. Differences between lower temperature corrosion and accelerated oxidation at high temperatures are described.
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Gas Turbine Engine Noise Reduction
1981Noise is unwanted sound, generated by a vibrating surface or a turbulent flow; transmitted by synchronised pressure fluctuations through a medium (section G.1); and received by the listener’s ear or, indirectly, via a microphone and a recording and playback system.
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2019
A gas turbine engine for an aircraft, comprising: an engine core; a covering configured to cover at least part of the engine core; and an engine accessory that interacts with the engine core or a component of the engine core; wherein the engine accessory is outside the covering.
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A gas turbine engine for an aircraft, comprising: an engine core; a covering configured to cover at least part of the engine core; and an engine accessory that interacts with the engine core or a component of the engine core; wherein the engine accessory is outside the covering.
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Gas Turbine Engine Development Partnerships
SAE Technical Paper Series, 1987<div class="htmlview paragraph">The development of gas turbine engines can benefit from the synergistic aspects gained by-partnership agreements. Development cost and risk are minimized by careful selection and application of modern technology.
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Gas turbine engines and propulsion
1993To compare the thermal efficiency for an industrial gas turbine engine with that for the air-standard cycle. To introduce the open-cycle with friction for an industrial gas turbine engine. To compare the performance of the cycle with friction with the air-standard cycle.
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