Manufacturing Demonstration of an All-Composite Selectively 3D Stitched Fuselage Section using HMZ-RTM

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Authors: Shuvam Saha, Brent Scheneman, Martin Tajiboy
Cited by: 0
References: 3

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