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Micro-Scale Regenerative Heat ExchangerA micro-scale regenerative heat exchanger has been designed, optimized and fabricated for use in a micro-Stirling device. Novel design and fabrication techniques enabled the minimization of axial heat conduction losses and pressure drop, while maximizing thermal regenerative performance. The fabricated prototype is comprised of ten separate assembled layers of alternating metal-dielectric composite. Each layer is offset to minimize conduction losses and maximize heat transfer by boundary layer disruption. A grating pattern of 100 micron square non-contiguous flow passages were formed with a nominal 20 micron wall thickness, and an overall assembled ten-layer thickness of 900 microns. Application of the micro heat exchanger is envisioned in the areas of micro-refrigerators/coolers, micropower devices, and micro-fluidic devices.
Document ID
20040171485
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Moran, Matthew E.
(NASA Glenn Research Center Cleveland, OH, United States)
Stelter, Stephan
(Polar Thermal Technologies Oak Creek, WI, United States)
Stelter, Manfred
(Polar Thermal Technologies Oak Creek, WI, United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2004
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
E-114821
NASA/TM-2004-213353
AIAA Paper 2004-6730
Meeting Information
Meeting: Canada-Europe-USA-Asia (CANEUS) 2004 Conferece on Micro-Nano-Technologies for Aerospace Applications
Location: Monterey, CA
Country: United States
Start Date: October 30, 2004
End Date: November 5, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 319-20-X1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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