Results 11 to 20 of about 294,503 (315)
Servitisation through structural adaptation
PurposeThe purpose of this study is to investigate the structural changes needed for project-based organisations (PBOs) to synthesise their project operations and services following the servitisation strategy. It addresses the question of how PBOs should change their organisational structure fitting with service provision strategy.Design/methodology ...
Saad Zighan +4 more
openaire +2 more sources
In the design of bonded aircraft structures, the type of failure is crucial. More specifically, the failure in case of overload should be limited to the surrounding fibre composite structure.
O. Völkerink, C. Hühne
doaj +1 more source
The present paper reports the outcomes of activities concerning a real-time SHM system for debonding flaw detection based on ground testing of an aircraft structural component as a basis for condition-based maintenance.
Monica Ciminello +10 more
doaj +1 more source
Delaminations are a concern for the structural integrity of fibre composite structures. The decisive material parameter for delaminations is fracture toughness. Structures usually have a multidirectional ply stacking.
O. Völkerink +3 more
doaj +1 more source
Car Soundproof Improvement through an SMA Adaptive System
The work at hand focuses on an adaptive system aimed at improving the soundproof performance of car door seals at specific regimes (cruise), without interfering with the conventional opening and closing operations.
Salvatore Ameduri +5 more
doaj +1 more source
The focus of the work is on the evaluation, development and integration of a robust actuator system for three-dimensional flow control of a blown Coanda flap to improve the high lift system of commercial aircraft.
Peter Wierach +2 more
doaj +1 more source
Manufacturing and Testing of a Variable Chord Extension for Helicopter Rotor Blades
Helicopters are still an indispensable addition to aviation in this day and age. They are characterized by their ability to master both forward flight and hover. These characteristics result in a wide range of possible operations.
Christoph Balzarek +3 more
doaj +1 more source
Integrated Shock Absorber With Both Tunable Inertance and Damping
Inerter is a two-terminal mass element, and the applied force is proportional to the relative acceleration between the terminals. According to the second class of mechanical–electrical analogy, the inerter corresponds exactly to the capacitor in the ...
Wei-Min Zhong +4 more
doaj +1 more source
Modelling of a SMA Blade Twist System Suited for Demonstration in Wind Tunnel and Whirl Tower Plants
In this work, the modeling of a demonstrator of a morphing system aimed at altering the twist of a rotorcraft blade is presented. The device was conceived for two different representative environments: the wind tunnel plant of the University of Bristol ...
Salvatore Ameduri +7 more
doaj +1 more source
Structure-Integrated Thin-Film Supercapacitor as a Sensor
Today, aircraft composite structures are generally over-dimensioned to avoid catastrophic failure by unseen damages. This leads to a higher system weight and therefore an unwanted increase in greenhouse gas emissions.
Jan Petersen +3 more
doaj +1 more source

