Multidisciplinary Methodology For Control Surface Simulation. Mechanical Systems Installation Department - Alenia Aeronautica. Speaker: Luigi MORRONE
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1 Multidisciplinary Methodology For Control Surface Simulation Speaker: Luigi MORRONE Mechanical Systems Installation Department - Alenia Aeronautica MSC Software Italian User s s Conference Turin, October 6 th 7 th 2010
2 Multidisciplinary Methodology For Control Surface Simulation ALENET ( Alenia Networked Enterprise Trasformation) Developed by: Luigi MORRONE Mechanical Systems Installation Department - Alenia Aeronautica Massimiliano PICCIRILLO Structure Department Alenia Aeronautica Mauro Camillo MAROTTA Flight Controls Systems Department Alenia Aeronautica Pasquale MASTROMAURO Flight Engineering Department Alenia Aeronautica
3 Summary SDM-TCE Workflow Concept Data Flow & Management Introduction Aircraft C-27J Flight Controls Systems High Level Work Flow Model definition:system Model Structural Model- Aero Force Dataset Assembly Model Solver Phase - PostProcessor Conclusions
4 SDM-TCE Workflow Concept Dept.1 Dept.2 1 Dept.3 2 Team Center Dept Dept.5 Dept.6 Link SDM Environment YES NO SDM Process Link Common Data Model (library/view)
5 Data Flow & Management SimXpert environment ICS. Structural On Board Systems. System ICS. Assembly, analysis set-up FIPER-Isight environment TCAA. Aero-loads mapping on structural mesh SimManager environment CAD Model (link to) File CI File Manouver Initial MB structural Structural FE Aero-Forces loads on MB Structural Control system System Assembled Specific results Aero-Force data set ICS Results view Initial MB system MB results
6 Flight Controls Systems C-27J C GEARED TRIM TAB AILERON GEARED TRIM TAB TAB OUTBOARD FLAP SPRING TAB INBOARD FLAP SPOILER ELEVATOR TRIM TAB RUDDER GEARED TAB
7 CAD Model High Level Process Flow Mechanical Systems Installation/On Board Systems. Surface Control System definition On Board Systems. System SimXpert Environment ICS. Structural ICS. Assembly, analysis set-up ICS Results view ICS. Flap FE structural TCAA. Flap FE CFD TCAA. Aero-loads mapping on structural mesh
8 System Model Rigid components: command line, shaft, screws, bearings, actuators, power distribution unit Kinematics joints Dynamic connections (spring, dampers, bushings, etc.) Forces and moments Surface control definition System CAD Model Structural Assembly Flap FE structual Flap FE CFD Aero-loads mapping on structural mesh Results view
9 Structural Model Rigid components: tracks, rollers, flap inboard Surface control definition Kinematics joints Elastic connections Forces and moments Contacts btw parts Flexibility of the flap outboard CAD Model Aerodynamic forces on the flexible flap Clearance measures btw flexible flap and other rigid components Flap FE structual Flap FE CFD System Structural Assembly Aero-loads mapping on structural mesh Results view
10 Aereo Force Dataset: Nodal Force (VFOSUB) Modal Force (MFOSUB) Modal Force (MFOSUB) Aero Force Dataset Surface control definition CAD Model Flap FE structual Flap FE CFD System Structural Aero-loads mapping on structural mesh Assembly Results view
11 Assembly Model The customized buttons are into the Tool Ribbon region of the Motion SimXpert Workspace: Surface control definition System CAD Model Structural Assembly Results view Flap FE structual Flap FE CFD Aero-loads mapping on structural mesh Assembly Button: permits to load and connect the System Model and the Structure Model Maneuver Button: permits to prepare the solver (ADAMS/Solver) data for the maneuvers selected.
12 Solver Phase Manual run: The Read_Excel_Manouver action, prepares the ADAMS/Solver command files (.acf) for all the analysis defined into the Excel file. Then is possible to run, for each analysis, the standard ADAMS/Solver command. All runs: Example: C:/MSC.Software/MSC_Adams/20 10/common/mdi.bat ru-st Analisi1 Use solver.bat to run all the analysis in one time.
13 PostProcessor Import results: SimXpert standard command: File-> Import -> XML Results File, then select the proper.res file. Post processing: SimXpert standard Results tools
14 Conclusions Main benefits: Process automation, related efficiency increase and time saving Parametrization Multidisciplinary Approach Multi run capability Flow data sharing using SDM capability (Simanager)
15 THANK YOU FOR YOUR ATTENTION
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