Exergy Analysis of Sulfuric Acid Production: A Systematic Framework Using UniSim Design. [PDF]
Ferreira UG, Vaz da Costa T, Neiro SMDS.
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Deformation Monitoring Systems for Hydroturbine Head-Cover Fastening Bolts in Hydroelectric Power Plants. [PDF]
Yujra Rivas E +4 more
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Symmetrical Triboelectric In Situ Self-Powered Sensing and Fault Diagnosis for Double-Row Tapered Roller Bearings in Wind Turbines: An Integrated and Real-Time Approach. [PDF]
Wang S +5 more
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Will Wind Turbines Affect the Distribution of Alashan Ground Squirrel? Insights from Large-Scale Wind Farms in China. [PDF]
Wang Y +7 more
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A benchmark dataset of electrical signals from a permanent magnet synchronous generator for condition monitoring. [PDF]
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Compact gas turbine installation
Energy Conversion and Management, 2001Abstract A compact gas turbine installation is described in which, to be compact and easier, the blades of the gas turbine (GT) (void inside) are mounted at the periphery of the rotor of the centrifugal air compressor (AC) with a single compression stage. The air, partially compressed in the AC rotor, is passed and compressed further in the channels
Mircea Cârdu, Marian Dumitru
exaly +3 more sources
Gas Turbine Installation in Naviplane N500
Designed by SEDAM and built in 1975–1977, the Naviplane N500 hovercraft started the Boulogne-Dover cross-channel service in mid-’78. The craft is powered by five AVCO-Lycoming TF40 gas turbines driving the three propellers and two lift fans and two KHD T216 APU’s for the electric power supply.
G. Oberlaender, P. Guienne
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Nonlinear Model Predictive Control of a Laboratory Gas Turbine Installation
The feasibility of model predictive control (MPC) applied to a laboratory gas turbine installation is investigated. MPC explicitly incorporates (input and output) constraints in its optimizations, which explains the choice for this computationally demanding control strategy.
Vroemen, B.G. +3 more
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AVIATION GAS TURBINE INSTALLATION PROBLEMS
SAE Technical Paper Series, 1946<div class="htmlview paragraph"><b>THE author divides this discussion of the problems likely to be encountered in the installation of the turbo-jet engine to very high-speed aircraft as follows:</b></div> <div class="htmlview paragraph"> <ol class="list nostyle"> <li class="list-item"><span class="li-label ...
M. Benedict
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