Invention Grant
- Patent Title: Method for test data reduction of composite intralaminar failure mode
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Application No.: US15009777Application Date: 2016-01-28
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Publication No.: US10775286B2Publication Date: 2020-09-15
- Inventor: Haozhong Gu
- Applicant: The Boeing Company
- Applicant Address: US IL Chicago
- Assignee: THE BOEING COMPANY
- Current Assignee: THE BOEING COMPANY
- Current Assignee Address: US IL Chicago
- Agency: MH2 Technology Law Group LLP
- Main IPC: G01N3/08
- IPC: G01N3/08 ; G06F30/15 ; G06F30/23 ; B32B41/00 ; G01N3/00 ; B32B7/02 ; G06F111/10 ; G06F113/26

Abstract:
A method to utilize the results from a series of FEM models to develop a master derivative of compliance curve. The use of the unique master curve resolves the test data variability issue caused by fitting the compliance curve individually. The analytically derived derivative of compliance curve eliminates the needs to take the derivative of compliance and therefore the derivative computation error no longer exists. By applying the existing solution and the solution as disclosed and claimed herein to the same set of the raw test data, it is found that data scatter is significantly reduced.
Public/Granted literature
- US20170219469A1 METHOD FOR TEST DATA REDUCTION OF COMPOSITE INTRALAMINAR FAILURE MODE Public/Granted day:2017-08-03
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