People
Fioriti, Marco
in Cooperation with on an Cooperation-Score of 37%
Topics
- aircraft
- weight
- architecture
- flight
- actuator
- actuating system
- spoiler
- design method
- flight control system
- rudder
- airfoil
- system architecture
- hinge
- aileron
- case study
- engine
- optimization
- electrification
- control system
- family
- reliability
- assessment
- maintenance
- engineering
- fuel
- bottleneck
- constraint
- supporting
- safety analysis
- complex system
- system safety
- operating costs
- maintainability
- market
- costs
- streamlining
- wiring
- electrical wiring
- fuel consumption
- propulsion
- variance
- jet propelled aircraft
- engine performance
- regional jet
- turboprop aircraft
- electric power
- electrical system
- vehicle occupant
- behavior
- passenger
- supersonic aircraft
- fuzzy logic
- submarine
- drone
- safety
- machinery
- specification
- piston engine
- mechanical engineering
- gasoline
- layout
- base line
- small aircraft
- strut
- takeoff
- airplane
- stakeholder
- system design
- general aviation aircraft
- general aviation
- civil aircraft
- data
- male
- airframe
- combustion
- internal combustion engine
- motor
- warehousing
- energy storage system
- taxicab
- turbine
- aerospace engineering
- jet engine
- propeller
- nacelle
- crash
- interface
- pump
- generator
- explosion
- engineer
- locomotive engineer
- database
- bay
- graph
- high density
- electric generator
- graphical user interface
- design model
- turboprop engine
- engine starter
- automobile
- traffic congestion
- city
- beltway
- helicopter
- landing
- contaminant
- simulation
- evening
- airport
- parking
- weather condition
- occupation
- livability
- fuel cell
- show 86 more
Publications
- 2021New methodology for flight control system sizing and hinge moment estimation
- 2020Multidisciplinary aircraft integration within a collaborative and distributed design framework using the AGILE paradigmcitations
- 2020Environmental and Flight Control System Architecture Optimization from a Family Concept Design Perspective
- 2020A model-based RAMS estimation methodology for innovative aircraft on-board systems supporting MDO applications
- 2019Streamlining Cross-Organizational Aircraft Development: Results from the AGILE Projectcitations
- 2019Development of a new conceptual design methodology for parallel hybrid aircraftcitations
- 2019Method for estimation of electrical wiring interconnection systems in preliminary aircraft designcitations
- 2019Applying a distributed collaborative MDAO environment to study the power matching of the propulsion system and the on-board electrified systems for advanced regional and short- to medium-range jetlinerscitations
- 2018Comparative study of advanced turboprop aircraft with wing and rear mounted propulsion system in the AGILE EU project
- 2018Propulsion and On-Board System Integration for Advanced Regional Jet with Different Level of Electrification in the AGILE project
- 2018Integration of on-board Systems preliminary design discipline within a collaborative 3rd Generation MDO framework
- 2018Preliminary Study on OBS Electrification Efficiency for Advanced Supersonic Business and Medium Jet with Unified Engines
- 2018Innovative concepts of electric system architectures and hybrid propulsion system for regional turboprop aircraft
- 2018Trade off studies of hybrid-electric aircraft by Fuzzy Logic methodologycitations
- 2018The Effect of Sub-systems Design Parameters on Preliminary Aircraft Design in a Multidisciplinary Design Environmentcitations
- 2018Multiphase Drives for Hybrid-Electric Propulsion in Light Aircrafts: A Viable Solutioncitations
- 2018Cost-estimating model for aircraft maintenancecitations
- 2018Parametric approach to operating costs estimation for an innovative regional aircraft
- 2018Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU projectcitations
- 2018DESIGN OF THE STRUT BRACED WING AIRCRAFT IN THE AGILE COLLABORATIVE MDO FRAMEWORK
- 2017On-Board Systems Preliminary Sizing in an Overall Aircraft Design Environmentcitations
- 2017Collaborative system of systems multidisciplinary design optimization for civil aircraft: AGILE EU project
- 2017The educational experience at Politecnico di Torino to develop and increase the capability in aircraft layout comprehension and definition
- 2016Assessment of airframe-subsystems synergy on overall aircraft performance in a Collaborative Design Environment.
- 2016Possible hybrid propulsion configuration for transport jet aircraftcitations
- 2016Collaborative Systems Driven Aircraft Configuration Design Optimization
- 2015Guided procedure for the Zonal Safety Analysis in aircraft preliminary design
- 2015Contribution To R.A.M.S estimation in early design phases of unmanned aerial vehicles - UAVs
- 2014POSSIBLE HYBRID PROPULSION CONFIGURATION FOR TRANSPORT JET AIRCRAFT
- 2014Adaptable conceptual aircraft design modelcitations
- 2013Hybrid configuration – Advanced A.P.U. concept for future turboprop
- 2013SUPPORT AND MAINTENANCE STRATEGIES FOR FUTURE, INNOVATIVE AND LARGELY WIDESPREAD AIR PERSONAL TRANSPORTATION SYSTEMS
- 2013Zonal safety analysis in aircraft conceptual design: Application to SAvE aircraftcitations
- 2012Design of all electric secondary power system for future advanced medium altitude long endurance unmanned aerial vehiclescitations
- 2012Zonal safety analysis in aircraft conceptual design: application to SAvE aircraftcitations
- 2007Virtual and flying models for aircraft development
Places of action
conferencepaper
On-Board Systems Preliminary Sizing in an Overall Aircraft Design Environment
Abstract
An innovative aircraft preliminary design environment is presented, in particular highlighting the impacts of on-board systems design discipline on the Overall Aircraft Design, especially in terms of mass changes and fuel consumptions. The design environment has been conceived and set up during a collaboration between Politecnico di Torino and the German Aerospace Center (DLR – Hamburg). The entire design workflow is presented, focusing the attention on the subsystems design module, an in-house tool named ASTRID, developed at Politecnico di Torino. ASTRID is conceived to design both conventional and innovative systems, as hybrid-electric propulsion systems and More Electric and All Electric architectures. In particular, from the design modules of the proposed environment, system masses and secondary power levels are obtained, hence pointing out the system design effects on aircraft weights and fuel consumptions. Two case studies are presented. The first one refers to the preliminary design of a general aviation aircraft equipped with a hybrid-electric propulsion system. Several variants are designed varying the degree of hybridization, meant as the ratio between the electric power and the total propulsive power. The second case study is centered on four 90-passengers civil airplane designs with the same stakeholders’ requirements but different on-board systems technology levels – i.e. ranging from a conventional architecture to the All Electric Aircraft, passing through two More Electric configurations. Each design affects differently the aircraft empty weight and the required mission fuel. At the end of the designs, it is assessed that a high degree of hybridization, around 35%, entails a drastic fuel reduction, marking the significant benefits of this innovative technology. Concerning the second case study, the most innovative concept, the All Electric Aircraft, is characterized by a significant fuel reduction due to the more efficient power off-takes and a lower empty weight compared to the traditional architecture, hence returning a lower Maximum Takeoff Weight.
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