20   Artículos

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en línea
Giovanna Barigozzi, Hamed Abdeh, Samaneh Rouina and Nicoletta Franchina    
Design of cooling systems for rotor platforms is critical due to the complex flow field and heat transfer phenomena related to the secondary flow structures originating at the blade leading edge. Horseshoe vortex and passage vortex are the fluid-dynamic ... ver más

 
en línea
Shucong Liu, Hongjun Wang and Xiang Zhang    
In gas turbine rotor systems, an intelligent data-driven fault diagnosis method is an important means to monitor the health status of the gas turbine, and it is necessary to obtain sufficient fault data to train the intelligent diagnosis model. In the ac... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Paolo Gaetani and Giacomo Persico    
In stator?rotor interaction studies on axial turbines, the attention is commonly focused on the unsteady rotor aerodynamics resulting from the periodic perturbations induced by the stator flow structures. Conversely, less interest has been historically a... ver más

 
en línea
Petro Kachanov,Oleksandr Lytviak,Oleksandr Derevyanko,Sergii Komar     Pág. 52 - 57
To absorb the power generated by a free turbine, hydraulic brake systems of various designs are used in ground tests of aircraft turboshaft gas turbine engines. Ground tests of aircraft turboshaft gas turbine engines with the use of such hydraulic brakes... ver más
Revista: Eastern-European Journal of Enterprise Technologies    Formato: Electrónico

 
en línea
Yipeng Zhang, Lidong He, Jianjiang Yang, Fangteng Wan and Jinji Gao    
The proposed integral squeeze film bearing damper can effectively decrease the vibration of an unbalanced single-side cantilevered rotor system such as a flue gas turbine and pump.
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Marios Patinios, James A. Scobie, Carl M. Sangan and Gary D. Lock    
This paper presents measurements of CO2 concentration and pressure in a new, highly instrumented and versatile, 1.5-stage gas turbine facility. The rig, which has been specifically designed for investigations related to hot gas ingestion, features interc... ver más

 
en línea
Hamed Abdeh, Giovanna Barigozzi and Nicoletta Franchina    
Off-design condition of a rotor blade cascade with and without platform cooling was experimentally investigated. The ability of the gas turbine to operate down to 50% to 20% of its nominal intake air flow rate has an important consequence in the change i... ver más

 
en línea
Artur Kulaszka, Józef Blachnio and Henryk Borowczyk    
The reliability and operational safety of an aircraft engine gas turbine are extremely important in terms of its operation. In the course of operation, these turbines undergo complex thermal, mechanical, aerodynamic, and chemical exhaust gas loads. Due t... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Qingcai Zhang, Qinqin Wang, Xiaoming Tan and Jingzhou Zhang    
A rim seal is often used to prevent the ingress of high-temperature gas into the turbine disk cavity and protect the turbine disk from damage. Based on the overlapping rim seal (Seal-A), this paper proposes two more composite sealing structures (Seal-B a... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Roberta Masci and Enrico Sciubba    
Modern gas turbine firing temperatures (1500?2000 K) are well beyond the maximum allowable blade material temperatures. Continuous safe operation is made possible by cooling the HP turbine first stages, nozzle vanes and rotor blades, with a portion of th... ver más

 
en línea
Paolo Gaetani and Giacomo Persico    
This paper presents the results of an experimental study on the evolution of hot streaks generated by gas turbine burners in an un-cooled high-pressure turbine stage. The prescribed hot streaks were directed streamwise and characterized by a 20% over-tem... ver más

 
en línea
Filippo Merli, Nicolas Krajnc, Asim Hafizovic, Marios Patinios and Emil Göttlich    
The purpose of the paper is to characterize the aerodynamic behavior of a rotor-downstream hub cavity rim seal in a high-pressure turbine (HPT) stage. The experimental data are acquired in the Transonic Test Turbine Facility at the Graz University of Tec... ver más

 
en línea
Anitha Kumari Azmeera, Prakash Jadhav and Chhaya Lande    
Upgrading abradable or wearable coatings in the high-temperature zone of aero engines is advised to increase the efficiency and high-density power in gas turbine engines for military or commercial fixed-wing and rotary-wing aircraft. The development of t... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Jörg R. Riccius and Evgeny B. Zametaev    
A numerical turbine-blade fatigue-life analysis method is suggested. This method comprises a stationary thermal 3D finite element (FE) analysis of the hot run for the combined high-cycle fatigue (HCF) and creep analysis, and a follow-on (one-way coupled)... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Gang Zhao, Tian Qiu and Peng Liu    
The pre-swirl stator-rotor system is a common and important structure in gas turbines, and its main function is to provide cold air to the turbine blades with a low relative total temperature. Under normal conditions, the boundaries of the system are sym... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Lahouari Mammar, Yahiaoui Tayeb, Omar Ladjedel, Ondrej ?ikula     Pág. 31 - 42
This paper is divided into two parts; the first describes a CFD analysis of a gland packing labyrinth seals in 20 MW steam turbine in LNG plant using ANSYS CFX code as an isothermal simulation in fluid domain. The results of two turbulence models k-e and... ver más
Revista: Periodica Polytechnica: Mechanical Engineering    Formato: Electrónico

 
en línea
Hui Tang, GeonHwan Cho, Mario Patinios, James A. Scobie, Carl M. Sangan, J. Michael Owen and Gary D. Lock    
Ingress is the penetration of a hot mainstream gas in a turbine annulus through the rim seal into the wheel-space between the rotating turbine disc (the rotor) and the adjacent stationary casing (the stator). Purge flow is used to prevent or reduce ingre... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Katrina Calautit, Angelo Aquino, John Kaiser Calautit, Payam Nejat, Fatemeh Jomehzadeh and Ben Richard Hughes    
Global demand for energy continues to increase rapidly, due to economic and population growth, especially for increasing market economies. These lead to challenges and worries about energy security that can increase as more users need more energy resourc... ver más
Revista: Computation    Formato: Electrónico

 
en línea
Samuel P. Lee, Simon M. Barrans, Martyn L. Jupp and Ambrose K. Nickson    
Current trends in the automotive industry towards engine downsizing mean turbocharging now plays a vital role in engine performance. A turbocharger increases charge air density using a turbine to extract waste energy from the exhaust gas to drive a compr... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Samuel P. Lee, Simon M. Barrans, Martyn L. Jupp and Ambrose K. Nickson    
Current trends in the automotive industry towards engine downsizing mean turbocharging now plays a vital role in engine performance. A turbocharger increases charge air density using a turbine to extract waste energy from the exhaust gas to drive a compr... ver más
Revista: Aerospace    Formato: Electrónico

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