Off-Design Analysis Method for Compressor Fouling Fault Diagnosis of Helicopter Turboshaft Engine [PDF]
Farshid Bazmi, Afshin Rahimi
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Data‐Driven Sliding Mode Control for Partially Unknown Nonlinear Systems
ABSTRACT This paper presents a novel data‐driven control framework for multi‐input multi‐output (MIMO) nonlinear systems with partially unknown dynamics and bounded disturbances. In practical scenarios, exact cancellation of system nonlinearities is often infeasible due to limited model information and unpredictable disturbances.
Jianglin Lan +2 more
wiley +1 more source
This article presents a vibration signal analysis method to diagnose helicopter turboshaft engine defects such as bearing imbalance and wear. The scientific novelty of the article lies in the development of a comprehensive approach to diagnosing ...
Serhii Vladov +6 more
doaj +1 more source
One‐Dimensional Finite Elements With Arbitrary Cross‐Sectional Displacement Fields
ABSTRACT This paper introduces an unprecedented unified approach for developing structural theories with an arbitrary kinematic variable over the beam cross‐section. Each of the three displacement variables can be analyzed using an independent expansion function. Both the order of the expansion and the number of terms in each field can be any. That is,
E. Carrera, D. Scano, E. Zappino
wiley +1 more source
IMPROVING THE QUALITY OF DIAGNOSTICS OF AN AXIAL COMPRESSOR OF A HELICOPTER GAS TURBINE ENGINE
V. A. Potapov, А. А. Sanko
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Conceptual design and optimization of a sustainable and environmentally friendly archetypal helicopter within the selection criteria and limitations. [PDF]
Gunaltili E +6 more
europepmc +1 more source
Numerical Analysis of Bird Strike on Engine Cowling of AW139 Helicopter using Sandwich Composite Material with Lattice Core Structure [PDF]
Budi Aji Warsiyanto +3 more
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Onboard Neuro-Fuzzy Adaptive Helicopter Turboshaft Engine Automatic Control System
A modified onboard neuro-fuzzy adaptive (NFA) helicopter turboshaft engine (HTE) automatic control system (ACS) is proposed, which is based on a circuit consisting of a research object, a regulator, an emulator, a compensator, and an observer unit.
Serhii Vladov +3 more
doaj +1 more source
Helicopters Turboshaft Engines Neural Network Modeling under Sensor Failure [PDF]
Serhii Vladov +4 more
openalex +1 more source

