SBIR/STTR Research Award

Generating Autoclave-Level Mechanical Properties with Out-of-Autoclave Thermoplastic Placement of Large Composite Aerospace Structures

Award identifier 4d9572b0cb5ad31346c5c485f92b83bfc99b54759e50ee9a3402b46bd60be4d0Awarding agency National Aeronautics and Space Administration

Award amount

$599,487

Program and phase

STTR · Phase II

Award year

2009

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ACCUDYNE SYSTEMS, INC.
Proposal award date
2009-06-22
Contract end date
2011-06-21
UEI
QLJLWGE4MHD4
Solicitation number
Not reported
Topic code
T7.02

Research abstract

While in the 1970's and 1980's, composites were adopted for aerospace structure for increased performance and weight savings, the 1990's and 2000's witnessed the attention towards cost-effective fabrication. All thermoset processes that utilize such machines rely on autoclaves to consolidate the laminates, at significant acquisition and operational expense. Autoclaves to consolidate wings are hugely expensive. Autoclaves for fuselages are nearly cost-prohibitive (only one exists). Autoclaves for the Ares V do not exist. The marketplace would welcome a proven out-of-autoclave fabrication technology. The tasks in the ASI/UD-CCM STTR phase 1 was to assess the performance of the current TP-ATP heads, do a model based parametric study to determine possible head and process parameter changes and demonstrate an improved understanding of the head, with a goal of autoclave level properties. A set of models for the in situ Automated Tow/Tape Placement (ATP) processes that capture the important process phenomena were developed by UD-CCM. Accudyne then measured the laminate roughness, fabricated samples using a variety of conditions and tested the samples. Testing of the laminates indicate: placing with flat tape and using improved head chilling increases mechanical properties. Compacting with only a ¼ load reduces properties. Using a vacuum bag oven reconsolidation is ineffective, and even reduces mechanical properties. The phase 2 program innovation is to develop and deploy University of Delaware process models to Accudyne's thermoplastic tow and tape placement head to remedy the mechanical property shortfall between the two fabrication processes used to manufacture large composite aerospace structure important to NASA. An additional advantage that would accrue by adopting TP-ATP would be the use of novel thermoplastic materials with thermal stability and toughness far in excess of what thermosetting materials can achieve.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

11 SBIR/STTR records share this UEI (2000–2012). Reported award amounts total $3,483,155. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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