18045257. SYSTEMS AND METHODS FOR SHAPING COMPOSITE STRUCTURES simplified abstract (The Boeing Company)
Contents
- 1 SYSTEMS AND METHODS FOR SHAPING COMPOSITE STRUCTURES
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 SYSTEMS AND METHODS FOR SHAPING COMPOSITE STRUCTURES - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Potential Applications
- 1.6 Problems Solved
- 1.7 Benefits
- 1.8 Potential Commercial Applications
- 1.9 Possible Prior Art
- 1.10 Unanswered Questions
- 1.11 Original Abstract Submitted
SYSTEMS AND METHODS FOR SHAPING COMPOSITE STRUCTURES
Organization Name
Inventor(s)
Luis F. Velasquez of Ladson SC (US)
Edward R. Duncan of Goose Creek SC (US)
SYSTEMS AND METHODS FOR SHAPING COMPOSITE STRUCTURES - A simplified explanation of the abstract
This abstract first appeared for US patent application 18045257 titled 'SYSTEMS AND METHODS FOR SHAPING COMPOSITE STRUCTURES
Simplified Explanation
The method described in the abstract involves shaping a composite structure by holding a composite member in an initial contour and then forming a final contour along the length of the member by sequentially shaping formed portions and unformed portions.
- Holding a composite member in an initial contour
- Forming a final contour by sequentially shaping formed portions and unformed portions
Potential Applications
The technology could be applied in industries such as aerospace, automotive, and construction for shaping composite structures with precision.
Problems Solved
This method solves the problem of efficiently shaping complex composite structures while maintaining structural integrity and accuracy.
Benefits
The benefits of this technology include improved efficiency in shaping composite structures, reduced material waste, and enhanced structural performance.
Potential Commercial Applications
"Precision Shaping Method for Composite Structures in Aerospace and Automotive Industries"
Possible Prior Art
There may be prior art related to methods for shaping composite structures, but specific examples are not provided in the abstract.
Unanswered Questions
How does this method compare to traditional methods of shaping composite structures?
Answer: This article does not provide a direct comparison to traditional methods, so it is unclear how this method differs in terms of efficiency, cost, and quality.
What are the limitations of this shaping method for composite structures?
Answer: The abstract does not mention any limitations or challenges that may arise when using this method, leaving room for further exploration into potential drawbacks or constraints.
Original Abstract Submitted
A method for shaping a composite structure includes steps of: (1) holding a composite member in an initial contour along a length of the composite member; and (2) forming a final contour along the length of the composite member by: (3) sequentially shaping formed portions of the composite member while holding unformed portions of the composite member in the initial contour to form portions of the final contour; and (4) sequentially shaping the unformed portions of the composite member to form other portions of the final contour.
