The aim of the COMBUSS project is to develop, design, manufacture and deliver to the Topic Manager (TM) facilities, all the prototype subcomponent manufacturing tooling needed to manufacture the stiffeners and panel of lower wing (including all auxiliary tools). COMBUSS project will design the tooling system which will incorporate self-heated capability with multiple heating zones and advanced thermal management.
For the COMBUSS project the major objective for the first reporting period (P1) was to design a prototype tooling system to produce the composite stiffened panel of the lower wing of a business jet. The design was on M9 of the project after a Critical Design Review (CDR) in collaboration with the TM. The tooling features the following key characteristics:
a. Full functionality for the processing in fewer steps of the integrated stiffened panel design.
b. Lightweight with long service life and flexibility.
c. Built-in quality assurance tools to guarantee reliable processing of the selected material systems according to technical specifications.
d. Tooling documentation for accurate dimensioning, modification protocols and health check during the tool service life.
In order to materialize this outcome, the COMBUSS Consortium has introduced, adapted and validated a set of innovative technologies covering materials, sensors, models, tools and devices. All these technologies will be physically integrated on the prototype tooling, which will acquire the required qualities in manufacturing.
Eventually, COMBUSS aims to develop and demonstrate an innovative tooling configuration for the manufacturing of all components of a composite stiffened panel, while considering sustainable production with integration of innovative modelling, monitoring, and optimization and control systems.