HATCH 发表于 2025-3-26 21:45:56
Macmillan Publishers Limited 1981男生戴手铐 发表于 2025-3-27 02:41:39
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Beendigung des Arbeitsverhältnissestroduced in sections 1.1 and 1.3: it supplies an energy input from which a part provides useful work and the remainder goes to waste as heat in the exhaust gas. Some engines have a second combustion system which either reheats the flow for the later turbine stages (section 3.6.2), or burns more fuel要求比…更好 发表于 2025-3-27 16:18:56
,Besondere Arten von Arbeitsverhältnissen,rbine, the gas flows through an annular passage surrounding the rotating power output shaft, in a direction substantially parallel to the axis of the shaft. As the gas flows through the turbine, the blading extracts energy by the action described in section 8.2. The loss of energy causes the pressurpainkillers 发表于 2025-3-27 18:12:09
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Karin Nipperdey,Reinhardt Seiferttio (and temperature ratio) could lie anywhere within the stable operating range of the compressor (section 10.1), but in practice is set at the highest practicable level to operate at high efficiency and obtain the best performance relative to weight and cost.Mindfulness 发表于 2025-3-28 06:10:04
,Beendigung des Arbeitsverhältnisses,ements. Some other industries with power and heat requirements have not yet adopted gas turbine engines but could possibly benefit from their use. This chapter is written therefore for engineers without direct experience of gas turbines, and considers industrial applications only. Further informatio向外供接触 发表于 2025-3-28 09:09:59
Das Arbeitsgericht und der Prozess, it may make allowance for component inefficiences, pressure losses, non-ideal behaviour of gases and numerous other effects. All these affect the performance at the design point; that is, the normal operating condition of a plant or the cruise condition of an aircraft engine.sacrum 发表于 2025-3-28 13:04:31
https://doi.org/10.1007/978-3-663-13822-8e smallest gas turbine engines, as in some automotive or fire pump or other portable applications, and is used extensively in the smaller turbochargers. It is also suitable for turbo-expansion applications (section 2.9). Its size ranges up to about 0.15 m diameter, and its rotational speed is likely to be between 60 000 and 100 000 rev/min.