Micro Cooling Concepts
- View government funding actions
- Huntington Beach, CA 92647
- Phone: 714-847-9945
- Corporate URL: www.microcoolingconcepts.com
- Estimated Number of Employees: 3
- Estimated Annual Receipts: $750,000
- Business Start Date: 2000
- Contact Person: Jack Fryer
- Contact Phone: 714-847-9945
- Contact Email: jayfryer@microcoolingconcepts.com
- Business Structure:
- Corporate Entity (Not Tax Exempt)
- Business Type:
- For Profit Organization
- Veteran Owned Business
- Subchapter S Corporation
- Industries Served: Power Boiler and Heat Exchanger Manufacturing
- Product Areas: R&D- ENVIRONMENTAL PROTECTION: OTHER (MANAGEMENT/SUPPORT), R&D-OTHER ENVIRONMENT-MGMT SUP
Sampling of Federal Government Funding Actions/Set Asides
In order by amount of set aside monies.
- $746,314 - Thursday the 27th of October 2016
National Aeronautics And Space Administration
NASA SHARED SERVICES CENTER
IGF::OT::IGF OTHER FUNCTION - GAS TURBINE ENGINE TECHNOLOGY IS CONSTANTLY CHALLENGED TO OPERATE AT HIGHER COMBUSTOR OUTLET TEMPERATURES. IN A MODERN GAS TURBINE ENGINE, THESE TEMPERATURES CAN EXCEED THE BLADE AND DISK MATERIAL LIMITS BY 600 ?F OR MORE, NECESSITATING BOTH INTERNAL AND FILM COOLING SCHEMES IN ADDITION TO THE USE OF THERMAL BARRIER COATINGS. INTERNAL CONVECTIVE COOLING IS INADEQUATE IN MANY BLADE LOCATIONS, AND BOTH INTERNAL AND FILM COOLING APPROACHES CAN LEAD TO SIGNIFICANT PERFORMANCE PENALTIES IN THE ENGINE. MICRO COOLING CONCEPTS HAS DEVELOPED A TURBINE BLADE COOLING CONCEPT THAT PROVIDES ENHANCED INTERNAL IMPINGEMENT COOLING EFFECTIVENESS VIA THE USE OF MICRO-STRUCTURED IMPINGEMENT SURFACES. THESE SURFACES SIGNIFICANTLY INCREASE THE COOLING CAPABILITY OF THE IMPINGING FLOW, AS COMPARED TO A CONVENTIONAL UNTEXTURED SURFACE. THIS APPROACH CAN BE COMBINED WITH MICROCHANNEL COOLING AND EXTERNAL FILM COOLING TO TAILOR THE COOLING CAPABILITY PER THE EXTERNAL HEATING PROFILE. THE COOLING SYSTEM CAN THEN BE OPTIMIZED TO MINIMIZE IMPACT ON ENGINE PERFORMANCE.
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