Method for creating a structure for calibration or verification for non-destructive evaluation inspection

Patent metadata

Field	Value
Publication number	US-10488369-B2
Application number	US-201715480977-A
Country	US
Kind code	B2
Filing date	Apr 6, 2017
Priority date	Apr 6, 2017
Publication date	Nov 26, 2019
Grant date	Nov 26, 2019

Abstract

Various embodiment methods to reliably and repeatedly replicate delaminations/disbonds and/or porosity defects in specimens/structures may include constructing the specimens/structures such that aerogel sheets and/or aerogel powders are placed or deposited in selected delamination/disbonding and/or porosity locations in the specimen/structure before the specimen/structure is cured. In various embodiments, the specimens/structures may be composites and/or bonded structures and the structures may be flat or curved. The aerogel sheets and/or aerogel powders may mimic delamination/disbonding and/or porosity defects in the cured specimens/structures. The cured specimens/structures including the replicated aerogel sheets and/or aerogel powders may be used for nondestructive inspection or other measurements, such as POD studies.

First claim

What is claimed is:

1. A method of fabricating a composite or bonded structure having at least one representative defect, comprising:
selecting one or more defect locations in a structure to be fabricated, wherein the defect locations are selected prior to completing fabrication of the structure;
fabricating the structure from one or more materials including at least one curable material, wherein fabricating the structure includes placing aerogel at one or more of the selected defect locations followed by curing the curable material of the structure whereby the aerogel forms a representative defect in the structure.

2. The method of claim 1 , wherein fabricating the structure includes laying up a plurality of ply layers to form a composite structure, and wherein the aerogel is configured to replicate a delamination defect in the composite structure.

3. The method of claim 2 , wherein fabricating the composite structure includes placing at least one aerogel sheet between at least two ply layers.

4. The method of claim 3 , wherein the at least one aerogel sheet includes a hydrophobic coating.

5. The method of claim 3 , wherein at least one of the ply layers has a ply thickness, and wherein a thickness of the least one aerogel sheet is less than the ply thickness.

6. The method of claim 2 , wherein fabricating the composite structure includes depositing aerogel powder to replicate a delamination defect in the composite structure.

7. The method of claim 1 , wherein the structure is a bonded structure that is fabricated by adhesively bonding a first member to a second member with curable adhesive material.

8. The method of claim 1 , wherein the aerogel is configured to replicate porosity defect.

9. The method of claim 8 , including depositing aerogel powder to replicate a porosity defect.

10. The method of claim 9 , wherein the structure is fabricate from a plurality of ply layers, and wherein aerogel powder is deposited on one or more ply layers during layup of the structure.

11. The method of claim 7 , wherein the aerogel powder is mixed with the curable adhesive prior to curing the adhesive material.

12. The method of claim 8 , wherein the structure is a bonded structure that is fabricated by adhesively bonding a first member to a second member with curable adhesive material.

13. The method of claim 1 , further comprising performing a non-destructive measurement on the structure after the curable material is cured to detect the representative defect formed by the aerogel.

14. A method of fabricating a measurement structure, comprising:
fabricating the measurement structure from one or more layers and a curable material;
wherein fabricating the measurements structure includes disposing aerogel in the measurement structure at a selected location relative to the one or more layers prior to curing the curable material followed by curing the curable material such that the aerogel replicates a defect in the measurement structure.

15. The method of claim 14 , wherein the aerogel is configured to replicate at least one of a porosity defect and a delamination defect.

16. The method of claim 15 , wherein the aerogel comprises one or more aerogel sheets or aerogel powder.

17. The method of claim 15 , wherein fabricating the measurements structure comprises at least one of a) laying up a plurality of ply layers to form a composite measurement structure, or b) adhesively bonding first and second layers together using a curable adhesive to form a bonded measurement structure.

18. The method of claim 14 , including adhering the one or more layers together with an adhesive layer.

Assignees

• Nasa

Inventors

• Juarez Peter D
• Leckey Cara A C

Classifications

• G01N2001/2893

  Preparing calibration standards · CPC title

• G01N15/088

  Investigating volume, surface area, size or distribution of pores; Porosimetry · CPC title

• G01N19/08

  Detecting presence of flaws or irregularities · CPC title

• G01N2291/2694

  Wings or other aircraft parts · CPC title

• B32B7/12

  using interposed adhesives or interposed materials with bonding properties · CPC title