Results 21 to 30 of about 21,160 (284)

Analysis of the Application and Benefits of Aircraft Electric Wheel Systems during Taxi and Take-Off

open access: yesInternational Transactions on Electrical Energy Systems, 2023
An electric wheel hybrid power system is designed for driving a large single-aisle passenger aircraft during the take-off and ground taxi phases, which consists of an APU, an energy storage system, and a motor.
Shuang Sun   +6 more
doaj   +1 more source

Advanced Materials and Technologies for Compressor Blades of Small Turbofan Engines

open access: yesAerospace, 2020
Manufacturing costs, along with operational performance, are among the major factors determining the selection of the propulsion system for unmanned aerial vehicles (UAVs), especially for aerial targets and cruise missiles.
Dmytro Pavlenko   +2 more
doaj   +1 more source

Large and Small Turbofans [PDF]

open access: yesMechanical Engineering, 2016
This article presents a study on common design challenges of large and small turbofans. Turbofan engines powering large transport aircraft have demonstrated much different design objectives than business-jet turbofans including thrust, range, mission type, development cost, unit price, maintainability standards, and production quantities.
openaire   +1 more source

Retrofitting of a High-Performance Aerospace Component via Topology Optimization and Additive Manufacturing

open access: yesMachines
This research presents a novel methodology for lightweighting and cost reduction of components with high structural demands by integrating advanced design and manufacturing techniques.
Jorge Crespo-Sánchez   +4 more
doaj   +1 more source

A New Robust Tracking Control Design for Turbofan Engines: H∞/Leitmann Approach

open access: yesApplied Sciences, 2017
In this paper, a H ∞ /Leitmann approach to the robust tracking control design is presented for an uncertain dynamic system. This new method is developed in the following two steps. Firstly, a tracking dynamic system with simultaneous consideration
Muxuan Pan   +3 more
doaj   +1 more source

Performance evaluation of aeroderivative gas turbine models derived from a high bypass turbofan for industrial power generation

open access: yesCogent Engineering, 2017
The paper presents the evaluation of the performance of various aeroderivative gas turbine models (AGTM) derived from a high bypass turbofan engine (HBTE).
Samuel O. Effiom   +2 more
doaj   +1 more source

Performance analysis of turbofan engine with afterburner with water injection at high-pressure compressor inlet

open access: yesАвіаційно-космічна техніка та технологія, 2022
Aircraft capabilities determine the performance of the engine that powers it, and therefore, the creation of the latest high-speed aircraft is directly related to the development level of aircraft engine building.
Yurii Ulitenko   +2 more
doaj   +1 more source

Selection of parameters for design of engine, turbofan and turbocompressor consisting of turbofan and turbofan mixed flow

open access: yesPerm National Research Polytechnic University Aerospace Engineering Bulletin
The article considers the features of the selection of the main parameters in the design of turbofan and turbofan-type turbofans, turbofans and turbocompressors of the gas generator in their composition. In addition to the known methods, new methods are proposed for using generalized statistical dependencies, such as the ratio of the diametrical ...
Nikolay Simonov   +2 more
openaire   +1 more source

The Future of Hydrogen‐Powered Aviation: Technologies, Challenges, and a Strategic Roadmap for Sustainable Decarbonization

open access: yesAdvanced Energy and Sustainability Research, EarlyView.
Hydrogen‐powered aviation offers a transformative pathway to zero‐emission flight by eliminating in‐flight CO2 emissions. Key considerations include propulsion systems (fuel cells and hydrogen combustion), cryogenic storage and insulation challenges, infrastructure and cost barriers, and supply‐chain constraints.
Mubasshira   +4 more
wiley   +1 more source

Research on analysis method of propulsive efficiency of prop-fan engine

open access: yesHangkong gongcheng jinzhan
It is of great significant for prop-fan engine under medium to high Mach number to evaluate the propulsive efficiency of turbofan, turboprop and prop-fan engines.
HUANG Xing   +3 more
doaj   +1 more source

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