18473836. In-Tool Compaction for Composite Structures simplified abstract (THE BOEING COMPANY)
Contents
In-Tool Compaction for Composite Structures
Organization Name
Inventor(s)
Thomas Karl Tsotsis of Santa Ana CA (US)
In-Tool Compaction for Composite Structures - A simplified explanation of the abstract
This abstract first appeared for US patent application 18473836 titled 'In-Tool Compaction for Composite Structures
Simplified Explanation: The patent application describes an in-tool system for compacting an out-of-plane feature of a composite structure using a cavity, a stiffener preform, and an insert.
Key Features and Innovation:
- In-tool system for compacting out-of-plane features
- Cavity with an angled surface
- Stiffener preform with an out-of-plane feature
- Insert with complementary faces for the cavity and the out-of-plane feature
Potential Applications: This technology can be used in the aerospace industry for manufacturing composite structures with complex geometries.
Problems Solved: This system addresses the challenge of compacting out-of-plane features efficiently and accurately during the manufacturing process.
Benefits:
- Improved structural integrity of composite structures
- Enhanced manufacturing precision
- Cost-effective production of complex components
Commercial Applications: The in-tool system can be utilized in the production of aircraft components, automotive parts, and other industries requiring high-performance composite structures.
Prior Art: Readers can explore prior patents related to composite structure manufacturing processes and tooling systems.
Frequently Updated Research: Stay informed about the latest advancements in composite structure manufacturing techniques and tooling technologies.
Questions about the Technology: 1. How does the in-tool system improve the manufacturing process for composite structures? 2. What are the key components of the cavity in this system and how do they contribute to the compaction process?
Original Abstract Submitted
An in-tool system for compacting an out-of-plane feature of a composite structure. The in-tool system comprises a cavity formed in a tool, a stiffener preform, and an insert. The cavity has an angled surface. The stiffener preform includes an out-of-plane feature, where the out-of-plane feature has a compaction surface. The insert comprises a first face complementary to the angled surface of the cavity and a second face complementary to the compaction surface of the out-of-plane feature. The first face is opposite the second face.
