Manufacturing Demonstration of an All-Composite Selectively 3D Stitched Fuselage Section using HMZ-RTM
Abstract
The next generation of aerospace structures is increasingly reliant on multifunctional, unitized composite designs that reduce part count, weight, and manufacturing complexity. This study presents the manufacturing demonstration of a stiffened, highly-unitized fuselage panel using a novel Heated Mold Z-Flow Assisted Resin Transfer Molding (HMZ-RTM) process. The selected architecture features an all-composite construction with integrated hat-stiffeners and two oval window cutouts, mimicking transport-class fuselage sections while emphasizing manufacturability and structural efficiency. Selective through-thickness stitching is employed to improve delamination resistance. This work addresses long-standing challenges associated with resin infiltration in thick, unitized architectures by utilizing localized mold heating and 3D resin extraction pathways to promote through-thickness flow. A complete bag-side HMZ-RTM layup strategy was implemented to ensure full compaction and reliable permeability management during infusion. The resulting structure demonstrates the manufacturability, robustness, and scalability of HMZ-RTM for large, unitized, damage-tolerant airframe components and provides a path forward for certifiable, damage-tolerant fuselage components manufactured through a single-shot infusion strategy. The details of tool design, preform construction, stitching procedures, and infusion methodologies are described in the paper.
Fields of Study & Subjects
Mechanical Behavior of Composites
Material Properties and Applications
Fiber-reinforced polymer composites
Publication details
- Journal / source
- AIAA SciTech Forum
- Publication date
- 8 January 2026