Results 41 to 50 of about 3,568 (253)

Review of Small Gas Turbine Engines and Their Adaptation for Automotive Waste Heat Recovery Systems

open access: yesInternational Journal of Turbomachinery, Propulsion and Power, 2020
Current commercial and heavy-duty powertrains are geared towards emissions reduction. Energy recovery from exhaust gases has great potential, considering the mechanical work to be transferred back to the engine.
Dariusz Kozak, Paweł Mazuro
doaj   +1 more source

Variable-speed rotor helicopters: Performance comparison between continuously variable and fixed-ratio transmissions [PDF]

open access: yes, 2016
Variable speed rotor studies represent a promising research field for rotorcraft performance improvement and fuel consumption reduction. The problems related to employing a main rotor variable speed are numerous and require an interdisciplinary approach.
Benini, Ernesto   +1 more
core   +1 more source

Analytical Calculation Model of the TV3-117 Turboshaft Working Regimes Based on Experimental Data

open access: yesApplied Sciences, 2023
The paper presents a practical and relevant analytical calculation model for free turbine turboshaft working regimes and engine performance. The analytical calculation model is based on a post-processing method that analyzes a series of experimental data,
Razvan Marius Catana, Gabriel Dediu
doaj   +1 more source

Examination of Applicability of Engine Condition Trend Monitoring to Bell 2068 Ill Helicopter

open access: yesPromet (Zagreb), 2002
Because of the advantages of turboshaft engine conditiontrend monitoring, it is in the interest of the Croatian Air Forceto examine its applicability in Bell 206B Ill helicopter maintenancesystem.The paper deals with the basic of turboshaft engine ...
Davor Mistrić   +2 more
doaj   +1 more source

Multi-Parameter Quadratic Programming Explicit Model Predictive Based Real Time Turboshaft Engine Control

open access: yesEnergies, 2021
The traditional model predictive control (tMPC) algorithms have a large amount of online calculation, which makes it difficult to apply them directly to turboshaft engine–rotor systems because of real time requirements.
Nannan Gu, Xi Wang, Meiyin Zhu
doaj   +1 more source

Model-Based Fault Diagnosis for Turboshaft Engines [PDF]

open access: yesIFAC Proceedings Volumes, 1997
Tests are described which, when used to augment the existing periodic maintenance and pre-flight checks of T700 engines, can greatly improve the chances of uncovering a problem compared to the current practice. These test signals can be used to expose and differentiate between faults in various components by comparing the responses of particular engine
Michael D. Green   +2 more
openaire   +1 more source

Design and additive manufacturing of Ti-6Al-4V test-piece for use in aeronautical turboshaft engine heat exchanger [PDF]

open access: yesMATEC Web of Conferences
While post-compression intercooling is commonly used to modify the performance characteristics of traditional turbocharged internal combustion engine layouts, there may be benefits to installing similar modifications in aeronautical turboshaft engines ...
Bester Paul.   +2 more
doaj   +1 more source

Thermal cycling performances of multilayered yttria‐stabilized zirconia/gadolinium zirconate thermal barrier coatings

open access: yesJournal of the American Ceramic Society, Volume 103, Issue 3, Page 2048-2061, March 2020., 2020
Abstract Gadolinium zirconate (Gd2Zr2O7, GZO) as an advanced thermal barrier coating (TBC) material, has lower thermal conductivity, better phase stability, sintering resistance, and calcium‐magnesium‐alumino‐silicates (CMAS) attack resistance than yttria‐stabilized zirconia (YSZ, 6‐8 wt%) at temperatures above 1200°C.
Dapeng Zhou   +6 more
wiley   +1 more source

Neural Nonlinear Autoregressive Model with Exogenous Input (NARX) for Turboshaft Aeroengine Fuel Control Unit Model

open access: yesAerospace, 2021
One of the most important parts of a turboshaft engine, which has a direct impact on the performance of the engine and, as a result, on the performance of the propulsion system, is the engine fuel control system.
Maria Grazia De Giorgi   +2 more
doaj   +1 more source

Investigation on the Optimal Design and Flow Mechanism of High Pressure Ratio Impeller with Machine Learning Method

open access: yesInternational Journal of Aerospace Engineering, Volume 2020, Issue 1, 2020., 2020
The optimization of high‐pressure ratio impeller with splitter blades is difficult because of large‐scale design parameters, high time cost, and complex flow field. So few relative works are published. In this paper, an engineering‐applied centrifugal impeller with ultrahigh pressure ratio 9 was selected as datum geometry.
Weilin Yi   +2 more
wiley   +1 more source

Home - About - Disclaimer - Privacy