Gas turbine or jet engineHRYNISZAK WALDEMAR DIPL.-ING.
A gas turbine by-pass type jet engine comprises a by-pass passage which is arranged to receive by-pass air and which communicates with the engine jet pipe, combustion equipment being mounted in the by-pass passage upstream of the region in which the latter communicates with the jet pipe, ...
Turbofan engines, commonly used to power aircraft, are a type of air-breathing jet engine that includes a fan and a core (turbine) engine that both ... TB Company 被引量: 0发表: 2017年 Theodorus spiral concept for pico-scale crossflow turbine nozzle design by computational method The implem...
文件:Gas Turbine_R_1.1.SLDASM 说明:SolidWorks工具内截图云检查是爱给网根据自动化脚本命令打开模型文件后自动截图生成,主要用于辅助判断预览图和实际模型的一致性。 提示:由于云检查并不是人工进行的,此项检查存在诸多因素(如视角设置不佳等)导致约有1%的模型还不能很好的展示,因此截图并不能完全代表模型的实际效...
This paper reviews the technical approach and reports on the results of ASPEN Plus; modeling of two patented approaches for integrating a gas turbine with reciprocating internal combustion engine for lower emissions and higher efficiency power generation. In one approach, a partial oxidation gas turbine...
Hybrid Fault Diagnosis: Application to a Gas Turbine Engine approach is employed to investigate faults in the fuel supply system and the nozzle actuator of a single-spool turbojet engine with an afterburner.doi... R Mohammadi,S Hashtrudi-Zad,K Khorasani - Asme Turbo Expo: Power for Land, ...
Turbine initializer gets 3 arguments as input:Gtengine::Simple::Turbine.new(burner, l_k, options) where:burner - is burner, as Gtengine::Simple::Burner class l_k - is l_k options - is a hash of options, defaults are:DEFAULTS = { eta: 0.9, eta_m: 0.985, g_ohl: 0.001, kpd: ...
Typical operating conditions of a jet engineFigure 1: Cross section of a turbojet and graph of typical operating conditions for its working fluid. The gas turbine operates on the Brayton cycle in which the working fluid is acontinuousflow of air ingested into the engine’s inlet. The air is...
However, it is well recognized that the lean combustors are prone to unstable operation and thermoacoustic pulsations [7,8], which results in reduced efficiency of the burning and leads to damage to the turbine. Therefore, it is important to study the contribution of different physical and ...
impingement; heat transfer; jet impingement; turbine cooling; jet orifice; crossflow1. Introduction The topic of jet impingement heat transfer has been widely researched, and details of such investigations can be found in [1,2,3]. Common parameters such as jet Reynolds numbers, jet-to-jet, ...