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
Wind tunnel balanceA flow-through balance is provided which includes a non-metric portion and a metric portion which form a fluid-conducting passage in fluid communication with an internal bore in the sting. The non-metric and metric portions of the balance are integrally connected together by a plurality of flexure beams such that the non-metric portion, the metric portion and the flexure beams form a one-piece construction which eliminates mechanical hysteresis between the non-metric and the metric portion. The system includes structures for preventing the effects of temperature, pressure and pressurized fluid from producing asymmetric loads on the flexure beams. A temperature sensor and a pressure sensor are located within the fluid-conducting passage of the balance. The system includes a longitudinal bellows member connected at two ends to one of the non-metric portion and the metric portion and at an intermediate portion thereof to the other of (1) and (2). A plurality of strain gages are mounted on the flexure beams to measure strain forces on the flexure beams. The flexure beams are disposed so as to enable symmetric forces on the flexure beams to cancel out so that only asymmetric forces are measured as deviations by the strain gages.
Document ID
19910005044
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Horne, Warren L.
(NASA Ames Research Center Moffett Field, CA, United States)
Kunz, Nans
(NASA Ames Research Center Moffett Field, CA, United States)
Luna, Phillip M.
(NASA Ames Research Center Moffett Field, CA, United States)
Roberts, Andrew C.
(NASA Ames Research Center Moffett Field, CA, United States)
Smith, Kenneth M.
(NASA Ames Research Center Moffett Field, CA, United States)
Smith, Ronald C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
July 11, 1989
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
Patent Number: NASA-CASE-ARC-11877-1-SB
Patent Application Number: US-PATENT-APPL-SN-195563
Patent Number: US-PATENT-4,845,993
Accession Number
91N14357
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-ARC-11877-1-SB|US-PATENT-4,845,993
Patent Application
US-PATENT-APPL-SN-195563
No Preview Available