SBIR/STTR Research Award

Asymmetric Conductance Thermoelectric Cooling Modules for Cryogenic Applications

Award identifier 8b51076c4fe0d5e26e7973f8194ee2e6ad9136b962a0935b614799d1e5145b23Awarding agency National Aeronautics and Space Administration

Award amount

$124,785

Program and phase

SBIR · Phase I

Award year

2017

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
MICROVECTION, INC.
Proposal award date
2017-06-09
Contract end date
2017-12-08
UEI
DL3FC1SALR38
Solicitation number
Not reported
Topic code
S3.06

Research abstract

Thermoelectric coolers (TECs) have long been noted for their compact construction, high reliability, and clean, quiet operation, and they are now widely used in consumer products. However, TECs are inefficient devices requiring large electrical currents to provide a refrigerant effect. Even modest improvements in TEC performance would vastly increase the market potential of thermoelectric cooling, expanding its role into maintaining space science instrument components at cryogenic temperatures (<90K), as well as increasing adoption in consumer appliances such as refrigerators and air conditioners. microVection has identified a means of improving the efficiencies of TECs with minor design and fabrication changes. This involves shifting the peak temperature location through modification of the conductance in a simple and controlled manner. This was demonstrated first analytically and then by using a small cell of 3 couples (6 legs), and the results showed a significant (~30%) increase in the temperature differential of the cell at no heat load. The simplicity of the concept suggests that it offers a near-term, affordable cooling solution that can take advantage of both advanced materials and reductions in scale to improve temperature differentials by as much as 30%. Conversely, the same temperature differential can be achieved at lower input power levels, or at higher cold-side heat fluxes, with input power being reduced by as much as 60%. The overarching goal of the proposed effort is to bring high-performance thermoelectric cooling technology to a maturity suitable for the space science and commercial marketplaces, and to demonstrate analytically and experimentally that asymmetric conductance TEC designs offer significant advantages over conventional thermoelectric devices. The specific objective of the Phase I is to show that asymmetric conductance thermoelectric devices offer near-term improvements to thermoelectric coolers in high current design scenarios.

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

5 SBIR/STTR records share this UEI (2002–2017). Reported award amounts total $418,080. Reported amounts are not federal obligations.

Phases: Phase I

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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