G - Physics – 06 – F
Patent
G - Physics
06
F
G06F 17/00 (2006.01) G05B 19/409 (2006.01) G05B 19/4097 (2006.01) G06F 17/50 (2006.01)
Patent
CA 2355666
A method of automatically defining the spatial arrangement of structural components and optimizing the functional positions and/or quantities thereof is useful for design and production of an aircraft cabin. The basic aircraft type is input into a configuration tool of a data processing system. The aircraft- specific geometry is stored in, loaded from and represented by a drawing module of the system. The required components are geometrically defined by stored data and position rules, and are combined with the aircraft-specific geometry in the drawing module. The components and the aircraft-specific geometry are spatially optimally configured relative to each other according to a rule set which accounts for specific customer requirements, in the configuration tool. Production documents such as drawings and parts lists are automatically generated by a document gener- ating tool of the system after inputting project-related data.
Lohmann Hans-Juergen
Muehlmeister Werner
Rasch Carsten
Gowling Lafleur Henderson Llp
Lohmann Hans-Juergen
Muehlmeister Werner
Rasch Carsten
LandOfFree
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