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Shape Memory Alloy Heat Engine

Award Information
Agency: Department of Defense
Branch: Army
Contract: W911W6-19-C-0043
Agency Tracking Number: A183-137-0268
Amount: $99,923.11
Phase: Phase I
Program: SBIR
Solicitation Topic Code: A18-137
Solicitation Number: 18.3
Timeline
Solicitation Year: 2018
Award Year: 2019
Award Start Date (Proposal Award Date): 2019-02-06
Award End Date (Contract End Date): 2020-03-15
Small Business Information
4030 Spencer St, Suite 108
Torrance, CA 90503
United States
DUNS: 106823607
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: Yes
Principal Investigator
 Scott Bland
 PRINCIPAL INVESTIGATOR
 (310) 626-8660
 sbland@nextgenaero.com
Business Contact
 Zoltan Feher
Phone: (310) 626-8384
Email: zfeher@nextgenaero.com
Research Institution
N/A
Abstract

The primary objective of this program is to design, model and demonstrate a shape memory alloy (SMA) heat engine with high efficiency utilizing improvements in material composition, processing and heat engine design developed by the NextGen Aeronautics/Penn State team. The proposed SMA engine design will provide high power density and efficiency at low temperature gradients and improved fatigue lifetimes over the current state-of-the-art. The proposed SMA heat engine will provide a practical, cost efficient method for powering structural and system health monitoring sensor networks. To achieve these objectives, during the Phase I effort we will focus development and evaluation of specific SMA compositions to meet phase transition and fatigue life requirements and processing of thin-film SMA belts. We will also perform further refinement of our proposed SMA heat engine architecture and develop system level models for simulation and optimization of the SMA heat engine. Successful completion of Phase I will result in feasibility assessment and proof-of-concept demonstration of the proposed SMA heat engine. We expect to achieve a TRL = 3 during the Phase I effort and with further technology maturation and evaluation during the Phase II effort we anticipate achieving TRL = 7 for the proposed technology.

* Information listed above is at the time of submission. *

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