A Comprehensive Commercialization Framework for Nanocomposites Utilizing a Model-Based Systems Engineering Approach
Abstract
:1. Introduction
1.1. The Complexity of Commercializing Nanocomposites
1.2. The ZT-CFRP Technology and the National NSF I-Corps Teams Program
2. Methodology
2.1. Market Analysis Overview (i.e., the Lean LaunchPad Approach)
2.2. Systems Analysis Overview (i.e., a Model-Based Systems Engineering Methodology)
- Defining requirements.
- From requirements, requirements diagrams are created.
- Requirements are further described by use cases.
- Each Use Case is further specified using activity diagrams.
- Requirements, use cases and activity diagrams are used to build block definition diagrams (bdds).
- Moving from black-box to white-box views, blocks from bdds are decomposed to internal block diagrams (ibds).
- Requirement diagrams, bdds and ibds can be used to define constraints/performance parametric diagrams.
- Bdds, ibds, and use case models are used as the basis of Scenario Sequence Diagrams.
- Ibds and activity diagrams can be used as the basis of Interaction State Diagrams.
- In summary, this MBSE methodology helps to determine the stakeholders and their requirements, the system domain, the system requirements, as well as behavioral, structural (e.g., logical and physical) and parametrical information of the technology.
2.3. Engineering Analysis Overview
3. Results
3.1. The Proposed Commercialization Framework
3.2. Framework Validation
- A team lead that coordinates and overlooks the different analyses.
- A market analyst with background knowledge of the Lean LaunchPad approach that performs the market analysis (note that during the interviews, it is important that at least two people are present: one as the interview lead and question-asker, and one to take notes).
- A systems analyst with background knowledge in MBSE that performs the system analysis and develops the system architecture/model. A test engineer with deep background knowledge of the technology to develop a prototype and perform necessary tests.
4. Discussion
4.1. Compariosn between Lean LaunchPad Approach and the Proposed Framework
4.2. Comparison to Other High Technology Commercialization Frameworks
4.3. Limitations of the Proposed Framework
4.4. A MBSE Model for the Proposed Framework
5. Conclusions
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
Disclosure
Appendix A
Interview Question | Answer/Notes |
---|---|
What is your name, job title and affiliation? | |
How long have you been working in your current position? | |
Do you have direct decision power over the integration of new materials in a product? | |
What kind of products does your company produce? | |
What challenges do you have with your current materials? | |
How does the general ecosystem look within your industry and where is your organization positioned within the value chain? | |
What properties are you usually looking for in a new material? | |
What kinds of properties would the ideal material have? | |
How do you become informed about new technology invention and how do you evaluate them? | |
How critical is the price point of a new material? | |
Have you had any kind of experience with nanotechnologies/-materials? | |
Are you using prepreg materials? | |
How much prepreg/material are you generally using for your products? | |
What is your production speed? | |
Do you or your suppliers have to comply to any regulations? | |
How long is your product development time? | |
How conservative is your industry for new inventions? | |
What are general quality control requirements for your suppliers? |
Appendix B
- Increased material strength and toughness will enable the use of lower-grade carbon fiber while achieving equivalent performance to that of high-grade carbon fiber, which results in a significant cost reduction and less export control limitations associated with some high-grade carbon fiber.
- Increased material strength will enable the manufacturing of ultra-lightweight, high-performing golf shafts for increased swing speed, hitting distance, and control.
- Structural weight savings of 20% reduce operational costs by ~10%.
- Improvements of 50% in ILSS reduce repair costs of structural composites by ~20%.
- Removing metal mesh reduces airplane weight by 454 kg (1000 lbs.).
- Currently, metal meshes are used for composite parts for lightning strike protection, which adds additional weight to the aircraft.
- There is a large need for weight reduction in aircraft for competitive advantages.
- The repair cost for composite parts on aircraft is very high due to the long repair time, which results in long downtimes for the aircraft.
- Being able to eliminate the metal mesh (454 kg) for an A320 aircraft could save ~ USD 430,000 in fuel savings per service life (30 years) of an aircraft at a jet fuel cost of USD 1.91/gallon, with the assumption that “100 kg of excess weight requires an additional 5000 kg of fuel per year per aircraft” (p.13) [42]. Based on a list price of USD 101.0 million [43], this would be a saving of over 4%.
- Increased material strength together with improved electrical and thermal conductivity will enable improved applications that result in lower vehicle weight and, therefore, lower fuel/energy consumption.
Appendix C
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Description | Initial Commercialization Status | Commercialization Status after Framework Utilization | |
---|---|---|---|
Tested Material Properties | |||
Tested CNF Concentration |
|
| P-ZT-CFRP:
|
Testing Focus | All material properties | Matrix-dominated properties (e.g., ILSS and compressive strength) based on needs of the sporting goods industry | |
Models | |||
Understanding of Failure Behavior | Low | High | |
Production Capabilities | Low Production Volume: 10 × 10 in./(2 days) of prepreg Prepreg Size: 10 × 10 in. | Medium Production Volume: 20 × 20 in./day of prepreg Prepreg Size: 20 × 20 in. | |
Potential Customer’s Willingness to Try This Technology | Low Reason: Not enough material data available; low production volume; prepreg size too small. | High Reason: Potential customers see great potential due to data for material property improvements. | |
Market Analysis | N/A | Yes | |
Systems Analysis | N/A | Yes | |
TRL | 4 | ~5 | |
Market Focus and Confidence Level | Focus: Aerospace Industry; Confidence Level: High; Support for Confidence Level: Initial aerospace funding | Focus: Golf Shaft Industry; Confidence Level: High; Support for Confidence Level: Material data and interviews with potential customers | |
Commercialization Strategy | N/A | Yes | |
Funding Opportunities | Low Reason: Not fundamental research anymore, but not mature enough for PFI or STTR/SBIR funding. | High Reason: Ideal level of maturity for PFI or STTR/SBIR funding. | |
Commercialization Risk | High | Medium/Low | |
Customer Acquisition Strategy | N/A | Publications, white papers, presentations, and material testing | |
Supply Chain | N/A | Yes Based on potential customers in the sporting goods industry | |
IP Security | Pending:
| Granted:
|
Propositions | Validation Criteria |
---|---|
A framework in which MBSE plays an important role when trying to overcome the many market and especially technological uncertainties that arise during the commercialization of nanocomposites |
|
The proposed framework is a combination of the Lean LaunchPad approach, a Model-Based Systems Engineering methodology and a thorough engineering analysis, which would tremendously support the commercialization process of nanocomposites such as the ZT-CFRP technology and, therefore, shorten the time to market, reduce costs and limit the risks. |
|
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Kirmse, S.; Cloutier, R.J.; Hsiao, K.-T. A Comprehensive Commercialization Framework for Nanocomposites Utilizing a Model-Based Systems Engineering Approach. Systems 2021, 9, 84. https://doi.org/10.3390/systems9040084
Kirmse S, Cloutier RJ, Hsiao K-T. A Comprehensive Commercialization Framework for Nanocomposites Utilizing a Model-Based Systems Engineering Approach. Systems. 2021; 9(4):84. https://doi.org/10.3390/systems9040084
Chicago/Turabian StyleKirmse, Sebastian, Robert J. Cloutier, and Kuang-Ting Hsiao. 2021. "A Comprehensive Commercialization Framework for Nanocomposites Utilizing a Model-Based Systems Engineering Approach" Systems 9, no. 4: 84. https://doi.org/10.3390/systems9040084
APA StyleKirmse, S., Cloutier, R. J., & Hsiao, K. -T. (2021). A Comprehensive Commercialization Framework for Nanocomposites Utilizing a Model-Based Systems Engineering Approach. Systems, 9(4), 84. https://doi.org/10.3390/systems9040084