NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Electronically scanned pressure sensor module with in SITU calibration capabilityThis high data rate pressure sensor module helps reduce energy consumption in wind tunnel facilities without loss of measurement accuracy. The sensor module allows for nearly a two order of magnitude increase in data rates over conventional electromechanically scanned pressure sampling techniques. The module consists of 16 solid state pressure sensor chips and signal multiplexing electronics integrally mounted to a four position pressure selector switch. One of the four positions of the pressure selector switch allows the in situ calibration of the 16 pressure sensors; the three other positions allow 48 channels (three sets of 16) pressure inputs to be measured by the sensors. The small size of the sensor module will allow mounting within many wind tunnel models, thus eliminating long tube lengths and their corresponding slow pressure response.
Document ID
19790006176
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Gross, C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 5, 1978
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Number: US-PATENT-4,111,058
Patent Application Number: US-PATENT-APPL-SN-835628
Patent Number: NASA-CASE-LAR-12230-1
Accession Number
79N14347
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,111,058|NASA-CASE-LAR-12230-1
Patent Application
US-PATENT-APPL-SN-835628
No Preview Available