Results 21 to 30 of about 224,010 (356)

Wireless Communication Networks for Gas Turbine Engine Testing [PDF]

, 2011
A new trend in the field of Aeronautical Engine Health Monitoring is the implementation of wireless sensor networks (WSNs) for data acquisition and condition monitoring to partially replace heavy and complex wiring harnesses, which limit the versatility ...
Dutta, PS, Atkinson, Robert, Mingding, H, Sasloglou, Konstantinos, Xuewu Dai, Cai, Lim Yun, University College London, Han Mingding, Cai, LY, Dutta, Partha, Dutta, Partha S., John Strong, Ang Chee Wei, Lim Yun Cai, Partha S. Dutta, Cai, Yun L, Mitchell, John, Schiffers, Werner, Schiffers, W, Strong, J, Konstantinos Sasloglou, Sasloglou, K, Werner Schiffers, MITCHELL, J, Atkinson, R, Dai, Xuewu, John E. Mitchell, Wei, AC, Wei, Ang Chee, Rolls-Royce, Yun Cai, Lim, Dai, X, Wei, Chee Ang, Strong, John, Glover, Ian, Glover, I, Mitchell, John E., Isabella Panella, Mingding, Han, Ian Glover, Xuewu, Dai, Panella, Isabella, Robert Atkinson, Chee Wei, Ang, Panella, I   +44 more
core   +1 more source

EFFICIENT TRACTION AND EXTERNAL RESISTANCE OF AIRCRAFT POWER PLANT

Авіаційно-космічна техніка та технологія, 2020
Increasing the efficiency and effectiveness of a gas turbine engine can be achieved through a comprehensive review of all tasks that determine the parameters and characteristics of an aircraft power plant and aircraft.
Юрий Юрьевич Терещенко, Иван Алексеевич Ластивка, Павел Владимирович Гуменюк, Су Хунсян   +3 more
doaj   +1 more source

CONTROLLER DESIGN FOR A GAS TURBINE ENGINE

IFAC Proceedings Volumes, 1979
Abstract An aircraft gas turbine engine is modelled as a multivariable system of nonlinear dynamic equations which is subject to a number of operating restrictions. This paper considers the specific control problem of transferring the states of the engine from an operating point of low thrust to high thrust output in an optimal manner (transient mode)
C.W. Jones, P.J. Fleming
openaire   +1 more source

An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product project [PDF]

Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", 2022
The development of a new gas turbine engine requires a lot of time and money spent on the design and testing its compressor, which has been shown as the most complex and time-consuming assembly unit of the engine.
A. V. Grekhnev
doaj   +1 more source

Impact of Fuel Composition on Gas Turbine Engine Performance

Journal of Engineering For Gas Turbines and Power, 2019
An industrial gas turbine can run on a wide variety of fuels to produce power. Depending on the fuel composition and resulting properties, specifically the hydrogen–carbon ratio, the available output power, operability, and emissions of the engine can ...
Dan Burnes, Alejandro Camou
semanticscholar   +1 more source

Gas-turbine diagnostics using artificial neural-networks for a high bypass ratio military turbofan engine [PDF]

, 2004
The Tristar aircraft, operated by the Royal Air Force, fly many thousands of hours per year in the transport and air-to-air refuelling roles. A large amount of engine data is recorded for each of the Rolls-Royce RB211-524B4 engines: it is used to aid ...
Singh, Riti, Probert, Sydney D., Ogaji, Stephen O. T., Joly, R. B.   +3 more
core   +1 more source

CUDA-integration of the control loop of aviation gas turbine engine

Авіаційно-космічна техніка та технологія, 2022
The problem of accelerating the process of designing aircraft gas turbine engines and their control systems, the system "AIRCRAFT-AVIATION ENGINE-FUEL", and forming the technical type of an aircraft engine, adapting to new operating conditions within the
Serhii Tovkach
doaj   +1 more source

Research on the influence of fuel gas on energy characteristics of a gas turbine [PDF]

E3S Web of Conferences, 2019
The purpose of this paper is to study and analyze the gas turbine engine and the thermodynamic cycle of a gas turbine. The article describes the processes of influence of the working fluid composition on the parameters of the main energy gas turbines ...
Marin G.E., Osipov B.M., Mendeleev D.I.
doaj   +1 more source

Active radial clearance design method based on customized linear expansion coefficient

Hangkong gongcheng jinzhan
The active clearance control (ACC) technology for compressors in aero engines has slow deformation response, which is not suitable for military aero engines with drastic changes in throttle lever, and leads to the problem of excessive radial tip ...
ZHANG Shaoping, PANG Yanlong, CHEN Yanyan   +2 more
doaj   +1 more source

Gas turbine engine dynamic model based on variable-memory LSTM architecture

Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2020
The buildup of thermodynamic cycle parameters is the main way to increase gas turbine engine efficiency. However, the growth of engine pressure and temperature ratio leads to the increase in the turbine heat load, which reduces the engine lifetime ...
A. V. Kuznetsov, G. M. Makaryants
doaj   +1 more source