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Aerospace, Volume 8, Issue 4

2021 April - 30 articles

Cover Story: Aircraft maintenance is a relevant factor for the direct operating costs of an airline. Therefore, there is an increasing interest in planning maintenance more efficiently and increasing aircraft availability. This study presents a Reinforcement Learning approach to optimize the scheduling of long-term maintenance checks. This type of algorithms' learning potential and adaptability can be valuable for producing fast and efficient check schedules while dealing with operation disruptions or other unexpected events. Results show a reduction in the checks scheduled in the long term and a consequent increase in aircraft availability, which can have a significant financial impact on the airline. View this paper.
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Articles (30)

  • Article
  • Open Access
17 Citations
6,465 Views
27 Pages

A Breakdown of System of Systems Needs Using Architecture Frameworks, Ontologies and Description Logic Reasoning

  • Ludvig Knöös Franzén,
  • Ingo Staack,
  • Petter Krus,
  • Christopher Jouannet and
  • Kristian Amadori

Aerospace systems are connected with the operational environment and other systems in general. The focus in aerospace product development is consequently shifting from a singular system perspective to a System-of-Systems (SoS) perspective. This incre...

  • Article
  • Open Access
21 Citations
8,611 Views
17 Pages

Exemplification of Detecting Gas Turbine Blade Structure Defects Using the X-ray Computed Tomography Method

  • Józef Błachnio,
  • Marek Chalimoniuk,
  • Artur Kułaszka,
  • Henryk Borowczyk and
  • Dariusz Zasada

X-ray computed tomography is more often applied in non-destructive testing the quality of construction elements significantly crucial for reliability and safety of device elements, machines and complex industrial systems. This article describes the c...

  • Article
  • Open Access
68 Citations
10,922 Views
22 Pages

Aircraft trajectory prediction is the basis of approach and departure sequencing, conflict detection and resolution and other air traffic management technologies. Accurate trajectory prediction can help increase the airspace capacity and ensure the s...

  • Article
  • Open Access
26 Citations
9,882 Views
30 Pages

Risk assessment methods are widely used in aviation, but have not been demonstrated for visual inspection of aircraft engine components. The complexity in this field arises from the variety of defect types and the different manifestation thereof with...

(This article belongs to the Special Issue Digitalization and Decision Support in Aerospace Maintenance Applications)
  • Article
  • Open Access
9 Citations
3,966 Views
22 Pages

The film-cooling performance of a 2.5D braided ceramic matrix composite (CMC) plate with preformed holes was numerically studied. Four numerical models containing braided structures were established: one model with film-cooling holes preformed throug...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
53 Citations
11,184 Views
18 Pages

Aircraft Maintenance Check Scheduling Using Reinforcement Learning

  • Pedro Andrade,
  • Catarina Silva,
  • Bernardete Ribeiro and
  • Bruno F. Santos

This paper presents a Reinforcement Learning (RL) approach to optimize the long-term scheduling of maintenance for an aircraft fleet. The problem considers fleet status, maintenance capacity, and other maintenance constraints to schedule hangar check...

(This article belongs to the Special Issue Digitalization and Decision Support in Aerospace Maintenance Applications)
  • Article
  • Open Access
7 Citations
4,046 Views
16 Pages

Self-Oscillations of The Free Turbine Speed in Testing Turboshaft Engine with Hydraulic Dynamometer

  • Oleksandr Lytviak,
  • Vasyl Loginov,
  • Sergii Komar and
  • Yevhen Martseniuk

Self-oscillations are one of the common problems in the complex automatic system, that can occur due to the features of the workflow and the design of the governor. The development of digital control systems has made it possible to damp self-oscillat...

(This article belongs to the Special Issue Technologies for Future Distributed Engine Control Systems)
  • Article
  • Open Access
4 Citations
4,735 Views
9 Pages

Solar particle events (SPEs) can pose serious threats for future crewed missions to the Moon. Historically, there have been several extreme SPEs that could have been dangerous for astronauts, and thus analyzing their potential risk on humans is an im...

  • Article
  • Open Access
10 Citations
4,238 Views
18 Pages

Active fault-tolerant control systems perform fault diagnosis and reconfigurable control. There is a bidirectional uncertainty between them, and an integrated scheme is proposed here to account for that. The system considers both actuator and sensor...

(This article belongs to the Special Issue Fault Detection and Prognostics in Aerospace Engineering)
  • Article
  • Open Access
14 Citations
5,261 Views
20 Pages

Sol–Gel Waveguide-Based Sensor for Structural Health Monitoring on Large Surfaces in Aerospace Domain

  • Maxime Royon,
  • Damien Jamon,
  • Thomas Blanchet,
  • François Royer and ,
  • Francis Vocanson,
  • Emmanuel Marin,
  • Adriana Morana,
  • Aziz Boukenter,
  • Youcef Ouerdane and
  • Sylvain Girard
  • + 9 authors+ 4 authors

The potential of sol–gel-based optical sensors is investigated for applications in the aerospace domain. To this aim, a low-cost and non-intrusive sol–gel sensor based on waveguides, arranged as a 2D matrix structure, is fabricated by UV photolithogr...

  • Editorial
  • Open Access
2,479 Views
2 Pages

This Special Issue contains selected papers from works presented at the 9th EASN International Conference on Innovation in Aviation & Space, which was successfully held in Athens, Greece, between the 3rd and 6th of September 2019 [...]

(This article belongs to the Special Issue 9th EASN International Conference on Innovation in Aviation & Space)
  • Editorial
  • Open Access
2,666 Views
3 Pages

This Special Issue contains selected papers from works presented at the 10th EASN International Conference on Innovation in Aviation & Space to the Satisfaction of the European Citizens, which was held successfully from the 2nd until the 4th of S...

(This article belongs to the Special Issue 10th EASN International Conference on Innovation in Aviation & Space to the Satisfaction of the European Citizens)
  • Article
  • Open Access
23 Citations
5,381 Views
15 Pages

A Text-Driven Aircraft Fault Diagnosis Model Based on a Word2vec and Priori-Knowledge Convolutional Neural Network

  • Zhenzhong Xu,
  • Bang Chen,
  • Shenghan Zhou,
  • Wenbing Chang and ,
  • Xinpeng Ji,
  • Chaofan Wei and
  • Wenkui Hou
  • + 2 authors+ 0 author

In the process of aircraft maintenance and support, a large amount of fault description text data is recorded. However, most of the existing fault diagnosis models are based on structured data, which means they are not suitable for unstructured data...

(This article belongs to the Special Issue Fault Detection and Prognostics in Aerospace Engineering)
  • Article
  • Open Access
7 Citations
3,608 Views
19 Pages

This study used pressure-sensitive paint (PSP) and determined the surface pressure distributions for a compressible swept convex-corner flow. The freestream Mach numbers were 0.64 and 0.83. The convex-corner angle and swept angle were, respectively,...

(This article belongs to the Special Issue Fluid Dynamic Measurement Technologies: Optical and Nanophotonic Methods)
  • Article
  • Open Access
14 Citations
6,790 Views
13 Pages

Bearing Strength and Failure Mechanisms of Riveted Woven Carbon Composite Joints

  • Mauricio Torres-Arellano,
  • Manuel de Jesus Bolom-Martínez,
  • Edgar Adrian Franco-Urquiza,
  • Ruben Pérez-Mora and ,
  • Omar A. Jiménez-Arévalo and
  • Philippe Olivier
  • + 1 author+ 0 author

This research aimed to determine riveted carbon/epoxy composites’ mechanical performance when fabricated by resin transfer molding (RTM). As this manufacturing process is gaining importance in the aeronautics and automotive industries, assembly metho...

  • Article
  • Open Access
52 Citations
21,126 Views
33 Pages

Aircraft Fleet Health Monitoring with Anomaly Detection Techniques

  • Luis Basora,
  • Paloma Bry,
  • Xavier Olive and
  • Floris Freeman

Predictive maintenance has received considerable attention in the aviation industry where costs, system availability and reliability are major concerns. In spite of recent advances, effective health monitoring and prognostics for the scheduling of co...

(This article belongs to the Special Issue Digitalization and Decision Support in Aerospace Maintenance Applications)
  • Article
  • Open Access
6 Citations
6,234 Views
14 Pages

Airworthiness standards of Korea recommend verifying structural safety by experimental tests and analytical methods, owing to the development of analysis technology. In this study, we propose a methodology to verify the structural safety of aircraft...

(This article belongs to the Special Issue Vibration Control for Space Application)
  • Article
  • Open Access
11 Citations
3,693 Views
14 Pages

Coupled Fluid–Solid Numerical Simulation for Flow Field Characteristics and Supporting Performance of Flexible Support Cylindrical Gas Film Seal

  • Junfeng Sun,
  • Meihong Liu,
  • Zhen Xu,
  • Taohong Liao and ,
  • Xiangping Hu,
  • Yuxian Li and
  • Juan Wang
  • + 2 authors+ 0 author

A new type of cylindrical gas film seal (CGFS) with a flexible support is proposed according to the working characteristics of the fluid dynamic seal in high-rotational-speed fluid machinery, such as aero-engines and centrifuges. Compared with the CG...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
24 Citations
5,973 Views
19 Pages

In order to study ice protection systems for rotating blades, a new experimental setup has been developed at the Anti-Icing Materials International Laboratory (AMIL). This system consists of two small-scale rotating blades in a refrigerated icing win...

(This article belongs to the Special Issue Deicing and Anti-Icing of Aircraft (Volume II))
  • Article
  • Open Access
5 Citations
4,074 Views
13 Pages

Online Identification-Verification-Prediction Method for Parallel System Control of UAVs

  • Yixin Huang,
  • Xiaojia Xiang,
  • Han Zhou,
  • Dengqing Tang and
  • Yihao Sun

In order to solve the problem of how to efficiently control a large-scale swarm Unmanned Aerial Vehicle (UAV) system, which performs complex tasks with limited manpower in a non-ideal environment, this paper proposes a parallel UAV swarm control meth...

(This article belongs to the Collection Unmanned Aerial Systems)
  • Article
  • Open Access
21 Citations
6,276 Views
12 Pages

Aeroelastic Stability Analysis of Electric Aircraft Wings with Distributed Electric Propulsors

  • Mohammadreza Amoozgar,
  • Michael I. Friswell,
  • Seyed Ahmad Fazelzadeh,
  • Hamed Haddad Khodaparast and ,
  • Abbas Mazidi and
  • Jonathan E. Cooper
  • + 1 author+ 0 author

In this paper, the effect of distributed electric propulsion on the aeroelastic stability of an electric aircraft wing was investigated. All the electric propulsors, which are of different properties, are attached to the wing of the aircraft in diffe...

(This article belongs to the Special Issue Advances in Aerospace Sciences and Technology)
  • Article
  • Open Access
30 Citations
7,396 Views
16 Pages

Wing Structure of the Next-Generation Civil Tiltrotor: From Concept to Preliminary Design

  • Marika Belardo,
  • Aniello Daniele Marano,
  • Jacopo Beretta,
  • Gianluca Diodati and ,
  • Mario Graziano,
  • Mariacarmela Capasso,
  • Pierpaolo Ariola,
  • Salvatore Orlando,
  • Francesco Di Caprio and
  • Luigi Di Palma
  • + 6 authors+ 1 author

The main objective of this paper is to describe a methodology to be applied in the preliminary design of a tiltrotor wing based on previously developed conceptual design methods. The reference vehicle is the Next-Generation Civil Tiltrotor Technology...

  • Article
  • Open Access
32 Citations
6,558 Views
11 Pages

To reduce gas leakage, shape optimization of a straight labyrinth seal was carried out. The six design parameters included seal clearance, fin width, fin height, fin pitch, fin backward, and forward expansion angle. The CFD (Computational Fluid Dynam...

  • Article
  • Open Access
21 Citations
4,829 Views
32 Pages

Current investigations into urban aerial mobility, as well as the continuing growth of global air transportation, have renewed interest in conflict detection and resolution (CD&R) methods. The use of drones for applications such as package delive...

(This article belongs to the Special Issue Application of Data Science to Aviation)
  • Article
  • Open Access
17 Citations
4,664 Views
20 Pages

The assembly quality of an aero-engine directly determines its stability in high-speed operation. The coaxiality and unbalance out of tolerance caused by improper assembly may give rise to complicated vibration faults. To meet the requirements of the...

  • Article
  • Open Access
18 Citations
3,266 Views
14 Pages

Pulse phase is the basic measurements of X-ray pulsar-based navigation, and thus how to estimate a pulse phase for an orbiting spacecraft is important. The current methods for on-orbit pulse phase estimation could provide an accurate estimation perfo...

  • Article
  • Open Access
32 Citations
6,926 Views
24 Pages

An Experimental Investigation of the Convective Heat Transfer on a Small Helicopter Rotor with Anti-Icing and De-Icing Test Setups

  • Abdallah Samad,
  • Eric Villeneuve,
  • Caroline Blackburn,
  • François Morency and
  • Christophe Volat

Successful icing/de-icing simulations for rotorcraft require a good prediction of the convective heat transfer on the blade’s surface. Rotorcraft icing is an unwanted phenomenon that is known to cause flight cancelations, loss of rotor performance an...

(This article belongs to the Special Issue Deicing and Anti-Icing of Aircraft (Volume II))
  • Article
  • Open Access
7 Citations
3,692 Views
27 Pages

Dynamic stall is a phenomenon on the retreating blade of a helicopter which can lead to excessive control loads. In order to understand dynamic stall and fill the gap between the investigations on pitching wings and full helicopter rotor blades, a nu...

  • Article
  • Open Access
4 Citations
4,402 Views
15 Pages

Two-phase flow in gas turbine compressors occurs, for example, at heavy rain flight condition or at high-fogging in stationary gas turbines. The liquid dynamic processes are independent of the application. An overview on the processes and their appro...

(This article belongs to the Section Aeronautics)
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Aerospace - ISSN 2226-4310