NASA SBIR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- H7.02-2933
SUBTOPIC TITLE:
 In-situ monitoring and development of in-process quality control for in-space manufacturing (ISM) applications
PROPOSAL TITLE:
 Feedback Sensors for Closed Loop Additive In-Space Manufacturing
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Cybernet Systems Corporation
3741 Plaza Drive
Ann Arbor , MI 48108-1655
(734) 668-2567

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Mr. Glenn Beach
proposals@cybernet.com
3741 Plaza Drive Ann Arbor, MI 48108 - 1655
(734) 668-2567

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Margaret Press
proposals@cybernet.com
3741 Plaza Drive Ann Arbor, MI 48108 - 1655
(734) 668-2567
Estimated Technology Readiness Level (TRL) :
Begin: 4
End: 5
Technical Abstract

This solicitation calls for online quality control to be applied to In-Space Manufactured (ISM) additive manufactured parts.  Our proposed approach is integrated precision scanning of the additive manufactured (AM) parts and feedback of that data back into AM layer by layer process control.  The goal is to augment Space Manufacturing AM process controls with verifiable feedback enabling improved process stability and part quality to significantly reduce the risk associated with complex AM parts, especially those with critical hidden internal geometries or other features not readily measured with non-destructive tests/measurements.

The proposed approach proposes to leverage and productize technology disclosed by the Marshall Space Flight Center in reference number MFS-TOPS-70 case number MFS-33013-2, a method that determines geometric differences (flaws) between the designed model and the printed part/component by employing IR cameras to collect accurate temperature data that can be validated against valid thermal models.  We will add to that approach by also employing mature but improved NIR optical measurement to implement an additional function on the moving AM extrusion head.  We then will employ the 3D data acquired by this embedded scanning sensor to (a) provide dimensional verification of part geometry after each deposition pass, and (b) when employed real time to modify machine control – likely requiring modification of the AM machine’s X, Y, Z, and feed rate controlling mechanisms that have to be different depending on ambient conditions (temp, humidity, and gravity) and deposited materials (plastic and plastic emulsion material differences).

Potential NASA Applications

The goal is to develop a real-time system active feedback control and process characterization applied to multiple materials, specifically in Phase I to FDM parts, and in Phase II to support in-space manufacturing employing the ISS AMF.  This will show how closed-loop AM manufacturing is feasible and changes the quality and consistency of AM manufactured parts for aerospace parts fabrication in support of rapid development and in-situ manufacturing for long-distance space missions.

Potential Non-NASA Applications

Key potential customers will be the military for out-of-production spares, industry for low quantity high quality parts manufacturing, and more specialized makers of other products like prostheses of 3D art.  We will also partner with interested AM machine OEMs.


Form Generated on 05/25/2018 11:30:03