Synonyme wurden verwendet für: Aircraft
Suche ohne Synonyme: title: Smart Intelligent Aircraft Structures (SARISTU)

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    Smart intelligent aircraft structures (SARITSU) : proceedings of the Final Project Conference

    Final Project Conference Smart Intelligent Aircraft Structures (SARISTU) | TIBKAT | 2016

    Manufacturing and Testing of Smart Morphing SARISTU Trailing Edge

    Essa, Yasser / de la Escalera Cutillas, Federico Martin / Dimino, Ignazio et al. | Springer Verlag | 2015
    (Smart Intelligent Aircraft Structures) project. The main challenge is to design and manufacture the smart ATED structure able to support the ...

    Assessment of the SARISTU Enhanced Adaptive Droop Nose

    Kintscher, Markus / Kirn, Johannes / Storm, Stefan et al. | Springer Verlag | 2015

    For the application of laminar flow on commercial aircraft wings, the high-lift devices at the leading edge play

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    Schlagwörter: Aircraft Model

    SARISTU: Six Years of Project Management

    Wölcken, Piet Christof / Kötter, Andreas / Newman, Ben et al. | Springer Verlag | 2015

    SARISTUSmart Intelligent Aircraft Structures—is a large, integrated research and technology project funded by

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    Benefit Analysis Value and Risk Assessment of New SARISTU-Technologies

    Batal, Sevgi / du Rand, Stephne | Springer Verlag | 2015

    The value and risk assessment investigates whether the SARISTU aim of improving aircraft efficiency has been met

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    Seamless Morphing Concepts for Smart Aircraft Wing Tip

    Nagel, Christof / Fiedler, Arne / Schorsch, Oliver et al. | Springer Verlag | 2015

    Methodologies for Guided Wave-Based SHM System Implementation on Composite Wing Panels: Results and Perspectives from SARISTU Scenario 5

    Monaco, Ernesto / Boffa, Natalino Daniele / Memmolo, Vittorio et al. | Springer Verlag | 2015

    Within the SARISTU project, the Application Scenario 5 (AS05) was devoted primarily to the development of

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    Morphing Value Assessment on Overall Aircraft Level

    Peter, Fabian / Stumpf, Eike / Carossa, Giovanni Marco et al. | Springer Verlag | 2015

    In order to assess the benefit of the morphing devices developed in the framework of SARISTU, integration in an

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    Schlagwörter: Aircraft Model

    Manufacturing of Nano-treated Lower Panel Demonstrators for Aircraft Fuselage

    Sasal, Feride Nur / Dogangun Akın, Aysun / Kılıc, Ayhan et al. | Springer Verlag | 2015
    within the SARISTU project, is carbon nanotube (CNT)-integrated prepreg material M21/34%/UD194/T800S, which is treated by University of Patras ...

    Shape Sensing for Morphing Structures Using Fiber Bragg Grating Technology

    Evenblij, Rolf / Kong, Frank / Koimtzoglou, Christos et al. | Springer Verlag | 2015
    transmission, their high endurance, and chemically inertness allow successful implementations in harsh environments such as aerospace. In the SARISTU ...

    Damage Assessment in Composite Structures Based on Acousto-Ultrasonics—Evaluation of Performance

    Moix-Bonet, Maria / Wierach, Peter / Loendersloot, Richard et al. | Springer Verlag | 2015

    Dynamic Aircraft Model with Active Winglet, Effects of Flight Mechanics and Loads Analysis

    Kanakis, Toni / Prananta, Bimo / van Tongeren, Hans et al. | Springer Verlag | 2015
    aircraft sizing tool. With the completion of the winglet design, the SARISTU winglet and the winglet active trailing edge (WATE) model have also ...
    Schlagwörter: Aircraft Model

    Improvement of the Electrical Isotropy of Composite Structures—Overview

    Flórez, Sonia / Gaztelumendi, Idoia / Gayoso, Jorge | Springer Verlag | 2015

    The aim of SARISTU is to take forward to higher TRL level from previous research various technologies and methods

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    Multi-scale-Reinforced Prepregs for the Improvement of Damage Tolerance and Electrical Properties of Aeronautical Structures

    Vavouliotis, A. / Sotiriadis, G. / Kostopoulos, V. | Springer Verlag | 2015
    improvement in damage tolerance and electrical isotropy which in turn can produce a reduction in weight at the aircraft structure level. Nanoparticle ...

    Design, Optimization, Testing, Verification, and Validation of the Wingtip Active Trailing Edge

    Wildschek, Andreas / Storm, Stefan / Herring, Martin et al. | Springer Verlag | 2015

    Within the scope of the SARISTU project (smart intelligent aircraft structures), a wingtip active trailing edge

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    Load Monitoring by Means of Optical Fibres and Strain Gages

    Airoldi, Alessandro / Sala, Giuseppe / Evenblij, Rolf et al. | Springer Verlag | 2015

    This chapter describes the development of load monitoring systems integrated in the demonstrator of a smart wing

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    Adaptive Trailing Edge: Specifications, Aerodynamics, and Exploitation

    Carossa, Giovanni Marco / Ricci, Sergio / De Gaspari, Alessandro et al. | Springer Verlag | 2015

    Damage Identification in Composite Panels—Methodologies and Visualisation

    Loendersloot, Richard / Buethe, Inka / Michaelides, Pavlos et al. | Springer Verlag | 2015

    Development of a Door Surround Structure with Integrated Structural Health Monitoring System

    Schmidt, Daniel / Kolbe, Andreas / Kaps, Robert et al. | Springer Verlag | 2015
    for in-service inspection of composite structures. Lamb waves can be excited and received using a network of actuators and sensors, which are ...

    Distributed Actuation and Control of a Morphing Wing Trailing Edge

    Dimino, Ignazio / Ciminello, Monica / Concilio, Antonio et al. | Springer Verlag | 2015

    Winglet Design, Manufacturing, and Testing

    Drezga, Danijel / Korian, Viken / Roock, Olaf et al. | Springer Verlag | 2015

    With respect to the SARISTU project (Smart Intelligent Aircraft Structures), a wingtip active trailing edge (WATE

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    Structural Design of an Adaptive Wing Trailing Edge for Large Aeroplanes

    Pecora, Rosario / Magnifico, Marco / Amoroso, Francesco et al. | Springer Verlag | 2015

    Development and Validation of a Bird Strike Protection System for an Enhanced Adaptive Droop Nose

    Chary, Charles | Springer Verlag | 2015

    In the frame of IS12 wing integration scenario of the SARISTU project, SONACA was incharge of the development and

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    Use of Carbon Nanotubes in Structural Composites

    Bonduel, Daniel / Kchit, Nadir / Claes, Michael | Springer Verlag | 2015
    conductive properties which make them the prime candidate to reinforce high-performance composite structures. However, location and dispersion state ...

    Elastomer-Based Skin for Seamless Morphing of Adaptive Wings

    Schorsch, Oliver / Lühring, Andreas / Nagel, Christof | Springer Verlag | 2015

    Ribbon Tapes, Shape Sensors, and Hardware

    Bosboom, Matthijs / van Wijngaarden, Martijn / Evenblij, Rolf et al. | Springer Verlag | 2015

    For fiber optic sensors to be integrated in aerospace structures and for these sensors to provide data that can

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    Compression After Multiple Impacts: Modelling and Experimental Validation on Composite Curved Stiffened Panels

    Psarras, Spyridon / Muñoz, Raul / Ghajari, Mazdak et al. | Springer Verlag | 2015

    Path-Based MAPOD Using Numerical Simulations

    Buethe, Inka / Dominguez, Nicolas / Jung, Henning et al. | Springer Verlag | 2015
    the industrial implementation. Due to the fixed mounting of SHM systems on structures, experimentally based investigation is particularly ...

    Morphing Wing Integrated Safety Approach and Results

    Verrastro, Maurizio / Metge, Sylvain | Springer Verlag | 2015

    SARISTU morphing wing is mainly based on three devices: enhanced adaptive droop nose (EADN), adaptive trailing

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    Damage Introduction, Detection, and Assessment at CFRP Door Surrounding Panel

    Bach, Martin / Dobmann, Nicolas / Moix-Bonet, Maria | Springer Verlag | 2015
    methodology, which has been integrated into a Graphical User Interface (GUI) in the SARISTU project. In this paper, the methodology is verified ...

    Methodologies for the Damage Detection Based on Fiber-Optic Sensors. Applications to the Fuselage Panel and Lower Wing Panel

    Güemes, Alfredo / Sierra, Julian / Grooteman, Frank et al. | Springer Verlag | 2015
    hypothesis testing-based method. These developments were put together on two realistic full-size aircraft structures, to validate the methodologies ...

    Coating for Detecting Damage with a Manifest Color Change

    Monier, Laura / Le Jeune, Karel / Kondolff, Isabelle et al. | Springer Verlag | 2015

    Carbon fiber-reinforced plastic (CFRP) structures are used in modern airliner. An impact may damage the inner

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    Implementation of a Structural Health Monitoring System for a Composite Wing Box Skin

    Marzani, Alessandro / Testoni, Nicola / De Marchi, Luca et al. | Springer Verlag | 2015

    Flat and Curved Panel Manufacturing

    van Wijngaarden, Martijn | Springer Verlag | 2015
    damage assessment of CFRP structures. Unidirectional carbon fibre prepreg has been used to laminate and autoclave the test panels. The flat ...

    Metallic Strip Details for Validation of ESN Technologies

    Perraud, Richard / Urrea, Olivier / Pelegrin, Thierry et al. | Springer Verlag | 2015

    The aim of AS10 is to evaluate technologies that can be integrated directly into structures with the target of

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    Installation of Metallic Strip on CRFP Frames: Assessment of IS13 Mechanical and Electrical Performance

    Perraud, Richard / Urrea, Olivier / Pelegrin, Thierry et al. | Springer Verlag | 2015

    The extended use of CFRP material in airframes led to a loss of the ability to use the aircraft superstructure

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    Testing Overview of the EADN Samples

    Snop, Vladimir / Horak, Vaclav | Springer Verlag | 2015
    SARISTU project. VZLU manufactured kinematic parts for wind tunnel model including auxiliary spar and assembled this test article. The functional ...

    An Electromechanical Impedance-Based Mobile System for Structural Health Monitoring and Reliability Check of Bonded Piezoelectric Sensors

    Lilov, Mihail / Siebel, Thomas | Springer Verlag | 2015
    structures for bonded transducers can degrade, monitoring of the reliability of these transducers is crucial to guarantee proper system operation ...

    Enhancement of Primary Structure Robustness by Improved Damage Tolerance

    Flórez, Sonia / Gayoso, Jorge | Springer Verlag | 2015

    The aim of SARISTU is to take forward to higher TRL level from previous research of various technologies and

     ...

    Enhanced Adaptive Droop Nose—from Computer Model to Multi-functional Integrated Part

    Heintze, Olaf / Steeger, Stefan / Falken, Alexander et al. | Springer Verlag | 2015

    The INVENT GmbH rises in the EU project SARISTU under the lead of Airbus and in cooperation with project partners

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    Fabrication of Carbon Nanotubes-Doped Veils

    Latko, Paulina / Boczkowska, Anna | Springer Verlag | 2015
    lighting strike protection instead of presently used metallic meshes or tapes. Due to their low weight, the total mass of the aircraft could be ...

    Enhancement of Infused CFRP Primary Structure Mechanical Properties Using Interleaving Thermoplastic Veils

    Breen, Daniel | Springer Verlag | 2015

    Damage tolerance of aircraft primary structures is important to prolong the life of the structure and reduce

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    Sensitive Coating Solutions to Lower BVID Threshold on Composite Structure

    Barut, Silvere | Springer Verlag | 2015

    The objectives of the 8th Application Scenario in SARISTU project is to develop sensitive coating for impact

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    Piezochromic Compounds Able to be Used in Shock Detecting Paints

    Gaudon, Manuel / Demourgues, Alain / Blanco-Gutierrez, Veronica et al. | Springer Verlag | 2015
    piezochromic behavior of the pigments. This point is very important for SARISTU project in order to get a palette of morphologies fitting ...

    Compression After Multiple Impacts: Modelling and Experimental Validation on Composite Coupon Specimens

    Psarras, Spyridon / Muñoz, Raul / Ghajari, Mazdak et al. | Springer Verlag | 2015

    Design and Manufacturing of WP135 Side Panel for Validation of Electrical Structure Network (ESN) Technologies

    Altkvist, Christina / Wahlbäck, Jonas / Tauchner, Juergen et al. | Springer Verlag | 2015

    Design and manufacturing of a curved stiffened panel has been carried out within WP135 in SARISTU Integration

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    Value at Risk for a Guided Waves-Based System Devoted to Damage Detection in Composite Aerostructures

    De Marchi, Luca / Marzani, Alessandro / Testoni, Nicola et al. | Springer Verlag | 2015
    influence on the maintenance portfolio. In this paper, a reliability-based optimization of the life cycle cost of a smart aircraft component is ...

    Toward the Upscaling of Guided Waves-Based NDE and SHM in Aeronautics

    Testoni, Nicola / De Marchi, Luca / Marzani, Alessandro | Springer Verlag | 2015
    -shaped piezoelectric sensor sensitive to the wave direction of arrival (WDA) of guided waves propagating in plate-like structures is described ...

    PAMELA SHM System Implementation on Composite Wing Panels

    Alcaide, Angel / Martin, Federico / Barrera, Eduardo et al. | Springer Verlag | 2015
    responses of several types of damages on different materials as metallic or composite structures is utmost importance for efficient and reliable SHM ...