標(biāo)題: Titlebook: Gas Turbine Design, Components and System Design Integration; Second Revised and E Meinhard T. Schobeiri Book 2019Latest edition Springer N [打印本頁(yè)] 作者: Corrugate 時(shí)間: 2025-3-21 16:39
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作者: 陪審團(tuán) 時(shí)間: 2025-3-21 23:58
Die Berufskrankheiten in der Schweiz,The energy transfer in turbomachinery is established by means of the stages. A . comprises a row of fixed, guide vanes called ., and a row of rotating blades termed ..作者: Morphine 時(shí)間: 2025-3-22 02:44 作者: 外表讀作 時(shí)間: 2025-3-22 08:07 作者: In-Situ 時(shí)間: 2025-3-22 09:51
Arbeitsmethoden der ThermodynamikUp to this point, the relationships developed for a turbomachinery stage have been strictly correct for given velocity diagrams with known inlet and exit flow angles. We assumed that the flow is fully congruent with the blade profile.作者: MERIT 時(shí)間: 2025-3-22 14:04
https://doi.org/10.1007/978-3-322-89473-1This chapter deals with the numerical modeling of the components pertaining to group 1 discussed in section 13.1.1. The components pertaining to this category are the connecting pipes, inlet and exhaust systems, as shown in Figure 13.1作者: MERIT 時(shí)間: 2025-3-22 19:41 作者: Tracheotomy 時(shí)間: 2025-3-22 23:32
Gas Turbine Thermodynamic Process,The first step toward designing a new gas turbine is to generate its thermodynamic cycle diagram. This diagram provides the essential information about the connection between the turbine inlet temperature TIT, the compressor pressure ratio . and the gas turbine thermal efficiency ..作者: 貝雷帽 時(shí)間: 2025-3-23 05:19
Theory of Turbomachinery Stages,The energy transfer in turbomachinery is established by means of the stages. A . comprises a row of fixed, guide vanes called ., and a row of rotating blades termed ..作者: Munificent 時(shí)間: 2025-3-23 06:57 作者: Contracture 時(shí)間: 2025-3-23 12:37 作者: ENACT 時(shí)間: 2025-3-23 17:55
Incidence and Deviation,Up to this point, the relationships developed for a turbomachinery stage have been strictly correct for given velocity diagrams with known inlet and exit flow angles. We assumed that the flow is fully congruent with the blade profile.作者: 喃喃而言 時(shí)間: 2025-3-23 21:08 作者: Expertise 時(shí)間: 2025-3-24 00:50
Gas Turbine Design, Preliminary Considerations,The objective of this chapter is to introduce novice engineers and students of turbomachinery design course to the fundamentals of gas turbine design.作者: 毗鄰 時(shí)間: 2025-3-24 02:47 作者: COWER 時(shí)間: 2025-3-24 09:57 作者: convulsion 時(shí)間: 2025-3-24 12:08 作者: 價(jià)值在貶值 時(shí)間: 2025-3-24 16:00
Arbeitsorientierte Arbeitslehreechanical energy (shaft work) with the surroundings takes place. In contrast to compressors, the total energy of the working medium is partially converted into shaft work, thus supplying necessary power to drive the compressor component, compensate for the bearing losses and provide the net power for driving the generator.作者: 綠州 時(shí)間: 2025-3-24 21:49
Thermo-Fluid Essentials for Gas Turbine Design, gas turbine engine with its components requires solid knowledge of aero-thermodynamic, heat transfer, combustion and solid mechanics design of these components. Aero-thermodynamics is the very basic tool for design, off-design and dynamic calculations of gas turbine components and hence the gas turbine system.作者: jaundiced 時(shí)間: 2025-3-24 23:52 作者: prosthesis 時(shí)間: 2025-3-25 05:38
Blade Design,The blade geometry is adjusted to the stage velocity diagram which is designed for specific turbine or compressor flow applications. Simple blade design methods are available in the open literature (see References).作者: 作嘔 時(shí)間: 2025-3-25 08:32
Turbine Aerodynamic Design and Off-Design Performance,echanical energy (shaft work) with the surroundings takes place. In contrast to compressors, the total energy of the working medium is partially converted into shaft work, thus supplying necessary power to drive the compressor component, compensate for the bearing losses and provide the net power for driving the generator.作者: excrete 時(shí)間: 2025-3-25 12:36
Springer Nature Switzerland AG 2019作者: Neonatal 時(shí)間: 2025-3-25 18:30 作者: Gleason-score 時(shí)間: 2025-3-25 22:49
Henriette Engelhardt,Alexia Prskawetzic energy. Gas turbines that produce shaft power are power .. Gas turbines that convert the fuel energy into kinetic energy are used for generation of thrust to propel aircrafts. The conversion of fuel energy into shaft power or propulsive force, requires interaction of several components of the eng作者: 使長(zhǎng)胖 時(shí)間: 2025-3-26 03:10 作者: 事先無(wú)準(zhǔn)備 時(shí)間: 2025-3-26 06:45 作者: 安慰 時(shí)間: 2025-3-26 08:40
Arbeitsmethoden der ThermodynamikThe blade geometry is adjusted to the stage velocity diagram which is designed for specific turbine or compressor flow applications. Simple blade design methods are available in the open literature (see References).作者: Dignant 時(shí)間: 2025-3-26 12:59 作者: 小樣他閑聊 時(shí)間: 2025-3-26 17:21
Arbeitsm?rkte und Sozialstrukturen in Europat of several . that we call . ([.,.,.,.]). Each component is an autonomous entity with a defined function within the system. Inlet nozzles, exit diffusers, combustion chambers, compressors, and turbines are a few component examples. A component may consist of several .. A turbine or a compressor sta作者: 搏斗 時(shí)間: 2025-3-26 21:31
fir+iaw Forschung für die Praxisrocess of heat exchange occurs between the high and low temperature sides. The working principle of these components is the same ([., ., .]). However, different working media are involved in the heat transfer process. More recently recuperators are applied to small and medium size gas turbine engine作者: Musculoskeletal 時(shí)間: 2025-3-27 04:15 作者: Employee 時(shí)間: 2025-3-27 07:27
Arbeitsorientierte Arbeitslehreechanical energy (shaft work) with the surroundings takes place. In contrast to compressors, the total energy of the working medium is partially converted into shaft work, thus supplying necessary power to drive the compressor component, compensate for the bearing losses and provide the net power fo作者: Accrue 時(shí)間: 2025-3-27 09:55
Simone Inversini,Eberhard Ulich,Marc Wülsersigns that are subject to extreme load conditions. Despite the enormous progress in the development of materials, at the design point, the engine components operate near their aerodynamic, thermal, and mechanical stress limits. Under these circumstances, any adverse dynamic operation causes excessiv作者: SLUMP 時(shí)間: 2025-3-27 15:50 作者: VOC 時(shí)間: 2025-3-27 17:48 作者: Formidable 時(shí)間: 2025-3-27 22:33
Arbeitsorganisation und Neue Technologiential kinetic energy difference . to the pressure buildup is marginal. In contrast, the above difference is substantial for a radial compressor stage, where it significantly contributes to increasing the total pressure as discussed in Chapter 4.作者: 新手 時(shí)間: 2025-3-28 05:53
Modeling the Compressor Component, Design and Off-Design,tial kinetic energy difference . to the pressure buildup is marginal. In contrast, the above difference is substantial for a radial compressor stage, where it significantly contributes to increasing the total pressure as discussed in Chapter 4.作者: 遺傳 時(shí)間: 2025-3-28 09:41 作者: Evolve 時(shí)間: 2025-3-28 14:16 作者: 必死 時(shí)間: 2025-3-28 17:29 作者: abduction 時(shí)間: 2025-3-28 20:23 作者: Priapism 時(shí)間: 2025-3-29 01:07
Special Topic: Reducing the Secondary Flow Losses By Endwall Contouring,se vortices induce drag forces that are the cause of the secondary flow losses. In addition, their interaction with the main flow causes angle deviation inside and outside the blade channel resulting in additional losses due to angle deviation. The nature of different flow losses is comprehensively treated in Chapter 6.作者: dry-eye 時(shí)間: 2025-3-29 05:16
omponent design, integration, off design and dynamic performThis is the second revised and enhanced edition of the book Gas Turbine Design, Components and System Integration written by a world-renowned expert with more than forty years of active gas turbine R&D experience. It comprehensively treats 作者: 捕鯨魚(yú)叉 時(shí)間: 2025-3-29 09:18
Henriette Engelhardt,Alexia Prskawetz thrust to propel aircrafts. The conversion of fuel energy into shaft power or propulsive force, requires interaction of several components of the engine, within each of them a chain of energy conversion takes place.作者: 悲觀 時(shí)間: 2025-3-29 12:20
https://doi.org/10.1007/978-3-663-13824-2nic flights, rocket propulsion systems and compression systems for transport of natural gas with a network of pipeline systems are a few examples of systems that heavily involve turbomachinery components.作者: 殘忍 時(shí)間: 2025-3-29 17:17 作者: 掃興 時(shí)間: 2025-3-29 23:47
Introduction, Gas Turbines, Applications, Types, thrust to propel aircrafts. The conversion of fuel energy into shaft power or propulsive force, requires interaction of several components of the engine, within each of them a chain of energy conversion takes place.作者: 巫婆 時(shí)間: 2025-3-30 02:17
Nonlinear Dynamic Simulation of Turbomachinery Components and Systems,nic flights, rocket propulsion systems and compression systems for transport of natural gas with a network of pipeline systems are a few examples of systems that heavily involve turbomachinery components.作者: abreast 時(shí)間: 2025-3-30 06:44
Generic Modeling of Turbomachinery Components and Systems,sers, combustion chambers, compressors, and turbines are a few component examples. A component may consist of several .. A turbine or a compressor stage exhibits such a sub-component. The numerical models of components are called 作者: Congruous 時(shí)間: 2025-3-30 12:16 作者: GET 時(shí)間: 2025-3-30 12:52 作者: semiskilled 時(shí)間: 2025-3-30 19:05
Gas Turbine Design, Components and System Design Integration978-3-030-23973-2作者: 聽(tīng)寫(xiě) 時(shí)間: 2025-3-30 23:21 作者: 領(lǐng)導(dǎo)權(quán) 時(shí)間: 2025-3-31 01:49 作者: 偏見(jiàn) 時(shí)間: 2025-3-31 07:31
idual modules that are integrated into a complete system. Quoting many statements by the gas turbine industry professionals, the young engineers graduated from the turbomachinery courses offered by the author, 978-3-030-23973-2作者: induct 時(shí)間: 2025-3-31 12:36 作者: Bucket 時(shí)間: 2025-3-31 17:11 作者: 大喘氣 時(shí)間: 2025-3-31 18:03
Efficiency of Multi-Stage Turbomachines,ses determines the stage efficiency which shows the capability of energy conversion within the stage. The stage efficiency, however, is not fully identical with the efficiency of the entire turbomachine.
