曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

the customization and the management of the whole aircraft engineering process, involving any commercial
software and in-house skill tools. This environment manages the Product Lifecycle at the simulation level and the
Knowledge Based Engineering (KBE) by encapsulating the customer skills and knowledge into Analysis Processes
and Analysis Methods that ensure the reusability and sharing of knowledge in the context of the Extended
Enterprise. CÆSAM can also be linked to the customer Simulation Data Management system and lastly, thanks
to its graphical interface, data sharing is provided within and across CAE analysis disciplines.
The analyst experts of the company can autonomously build and document their own simulation processes,
involving commercial software, in-house codes, but also re-engineered algorithms with the CAESAM development
toolkit. This includes any kind of simulation, from simple analytic formulas to complex Finite Element
models, for whom advanced capabilities (pre- and post- processing, exchange...) are provided.
Application- The CAE centric application framework CAESAM developed by SAMTECH was chosen by
Airbus for its new harmonised trans-national Structure Analysis environment ISAMI. The main objectives of
ISAMI (which stands for „Improved Structure Analysis Multidisciplinary Integration“) are to rationalize processes,
methods and tools, and to have one common environment for structure analysis disciplines at an Extended
Enterprise level. ISAMI integrates the AIRBUS aircraft structure analyses in one single CAE framework where all
the computation processes, methods, software tools and data are fully embedded.
Since July 2008, this new platform ISAMI is deployed at an Extended Enterprise level and will be used by
AIRBUS for the composite and metallic structural sizing of the A350 XWB to secure the sizing by fully validated/
efficient processes methods and tools, with also advanced capabilities (like NASTRAN or SAMCEF Finite
Element models…) when needed.
Title: Simulation Research Center for Mobile Platforms
Authors: Prof. M. Zasuwa, Prof. J. Narkiewicz
Warsaw University of Technology
Time: November 4, 2009 4:40 pm
Room: Lumen
The paper presents the Simulation Research Center (SRC) that is under development at the Department of Automation
and Aeronautical Systems (DAAS), Institute of Aeronautics and Applied Mechanics (IAAM), Warsaw
University of Technology (WUT).
The objective of the Centre is to provide support for design and development of several mobile platforms by
operating several innovative, reconfigurable simulators. The moving platforms are: UGV robot supporting various
operations for security and anti-disaster operations, helicopter simulator as training device class for flight
and navigation procedures and the platform for fixed-wing aircraft basic instrument training.
The novelty of the approach in the Centre development is the high level of reconfigurability, which allows to
implement simulation models of other, various mobile platforms.
The reconfiguration level is important for simulating operations of very different mobile platforms, which may
operate in ground and air in various environment conditions and scenarios. The software has an open, modular
architecture allowing for the modification, extension and enrichment. Due to their flexibility the simulators
may be used to verify the design of mobile platforms (at the design process and after), and they may be used
for training of the operators both of robots, helicopters and fixed-wings as well as for the validation of the
system elements.
In the paper the requirements, architecture and usability of the simulators are described,
showing the novelty of the solution (both in hardware and software).
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Title: Flow and Cure Simulation for the Production of Large and
Thick Walled Composite Structures
Authors: F. Klunker, S. Aranda, Prof. G. Ziegmann
TU Claustal
Time: November 4, 2009 5:00 pm
Room: Lumen
Fibre reinforced polymer composites offer desirable properties for the design of lightweight structures and
thus are becoming more and more the materials of choice in the aircraft and aerospace industry. The further
reduction of costs while maintaining the quality is a major challenge to be faced in the production of this kind
of composite parts. A well accepted technology for the manufacturing of structural and semi-structural components
is Liquid Composite Moulding. The production costs reduction in these technologies requires the optimisation
of the impregnation and curing phases. Simulation is a valuable tool for the reduction of the whole cycle
and in consequence, for the rise of the maximum affordable production rate. Especially in the case of complex
　
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