SBIR/STTR Research Award

Fluid Temperature Determination from Surface Temperatures and Heat Fluxes

Award identifier ea017684c54f686ec1c23ab6a9b79620a360f57f2a95c5b3cb575fd5cfda02daAwarding agency National Aeronautics and Space Administration

Award amount

$69,640

Program and phase

SBIR · Phase I

Award year

1994

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Rdf Corp.
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Fluid temperature in a piping system can be accurately determined non-intrusively with pipe surface temperature and its correction factor. A new technique, called flux augmented surface temperature (FAST) method is proposed to determine the correction factor directly in real time, in situ. The correction factor is directly proportional to a heat flow through pipe wall. In FAST method, the proportional coefficient is directly calculated from 2 sets of surface temperature and heat flux measurements. Innovation in FAST method is a technique which creates 2 different thermal environments. These environments produce significantly different surface temperature and heat flow from each other, but they will leave no residual thermal disturbance to fluid or pipe. In FAST method, there are 2 heat flux sensors, both which can measure surface temperature and heat flux simultaneously. These sensors are equipped with heater and/or cooler, which are dynamically controlled in such a way that no heat will be generated or absorbed as net. FAST method is expected to produce response time and temperature accuracy comparable to a direct immersion method. FAST method and its heat flux sensor can be used many commercial applications as well as NASA rocket test facility, because of its easy installation.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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