Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: An overview

N Rath, RK Mishra, A Kushari - International Journal of Turbo & Jet …, 2024 - degruyter.com
Aero engine performance deterioration highly influences its reliability, availability and life
cycle. Predictive maintenance is therefore a key figure within Industry 4.0, which guarantees …

[HTML][HTML] Real-time gas turbine model for performance simulations

H Gazzetta, C Bringhenti, JR Barbosa… - Journal of Aerospace …, 2017 - SciELO Brasil
Industry and universities around the world invest time and money to develop digital
computer programs to predict gas turbine performance. This study aims to demonstrate a …

[图书][B] Fundamentals of heat engines: Reciprocating and gas turbine internal combustion engines

J Ghojel - 2020 - books.google.com
Summarizes the analysis and design of today's gas heat engine cycles This book offers
readers comprehensive coverage of heat engine cycles. From ideal (theoretical) cycles to …

Detection and localization of fouling in a gas turbine compressor from aerothermodynamic measurements

KT Millsaps, J Baker… - … Expo: Power for …, 2004 - asmedigitalcollection.asme.org
This paper presents a new method for condition assessment of axial flow compressors that
provides a tool for specifying the magnitude and location of degradation due to fouling. A …

Performance of a turbojet engine with fluidic thrust vectoring

TC Sekar, RH Sundararaj, R Arora… - The Aeronautical …, 2022 - cambridge.org
The objective of the present work is to estimate the performance of a turbojet engine during
Fluidic Thrust Vectoring (FTV) employed by injecting the secondary-jet at the throat of a …

Performance analysis and dynamic modeling of a single-spool turbojet engine

IC Andrei, A Toader, G Stroe… - AIP Conference …, 2017 - pubs.aip.org
The purposes of modeling and simulation of a turbojet engine are the steady state analysis
and transient analysis. From the steady state analysis, which consists in the investigation of …

[PDF][PDF] Analysis of the sensitivity of multi-stage axial compressors to fouling at various stages

JD Baker - 2002 - core.ac.uk
This thesis presents a simple, meanline analysis of the impact of blade roughness on the
mass flow, work coefficient, and efficiency of a three-stage axial compressor as a function of …

Digital simulation of propulsion system performance for cycle optimization studies

V Sanghi, SK Sane - International Journal of Turbo and Jet Engines, 1999 - degruyter.com
The propulsion system has a high cost of ownership, long development period, and bears a
dominant influence on aircraft mission performance. Thus identification of an optimum …

[PDF][PDF] COMPARATIVE ANALYSIS FOR PERFORMANCE PREDICTION IN CASE OF IAR 99 AIRCRAFT PROPULSION SYSTEMS

IC ANDREI, MV PRICOP, ML NICULESCU… - Scientific Research & …, 2024 - ns.afahc.ro
This paper presents a comparative analysis regarding Performance Prediction at Design
and Off-Design Regimes, applied for two distinct constructions of Jet Engines as Propulsion …

[PDF][PDF] The completion of the mathematical model by parameter identification for simulating a turbofan engine

IC Andrei, MV Pricop, ML Niculescu, A Cernat - INCAS Bulletin, 2015 - researchgate.net
The purpose of this paper is to set up a method to determine the missing engine design
parameters (turbine inlet temperature T3T, airflow rate) which significantly influence the jet …