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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 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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Prognostics for Gas Turbine Engines
2017<div class="section abstract"> <div class="htmlview paragraph">This document applies to prognostics of gas turbine engines and its related auxiliary and subsystems. Its purpose is to define the meaning of prognostics with regard to gas turbine engines and related subsystems, explain its potential and limitations, and to provide guidelines
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Gas Turbines and Engine Simulations
2016Abstract Turbulent combustion is a complex phenomenon combining the random nature of turbulence with the nonlinearity of chemistry. As a major process for energy production, in particular in propulsion systems, turbulent combustion must be perfectly controlled to ensure maximum efficiency with minimum environmental impact in terms of both fuel ...
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Cracks in turbine disks of gas-turbine engines
Strength of Materials, 1972Ch. L. Svetlakov +2 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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Applications for Gas Turbine Engines
1981Gas turbine engines are most generally known for their use in aircraft (section 2.1)[9] but they are also used in surface transportation (section 2.2) and increasingly in stationary applications. The latter field encompasses the greatest variety of configurations and purposes and is still expanding, whereas the aviation field is consolidating.
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Efficiency of Gas Turbine Engines
The Kennesaw Journal of Undergraduate Research, 2020openaire +1 more source
Stoichiometric Gas Turbine Engines
Proceedings of Higher Educational Institutions. Маchine Building, 2018openaire +1 more source