Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1990-12-26
1992-05-19
Woodiel, Donald O.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
7386204, G01M 900
Patent
active
051136961
ABSTRACT:
An improved wind tunnel six component balance that is capable of accurately measuring low loads and high loads. The variable range balance has low load axial elements that will measure low loads precisely. When the load is increased over the low range capability of the measuring elements, in either the positive or negative load direction, pressure is applied to either the forward or aft bellows that are mounted in the inner tubular rod of the balance. This pressure applies a counter balance in force that reacts against the load applied. The results of this force is that the low loads links will always stay on range.
REFERENCES:
patent: 2918816 (1959-12-01), Ormond
patent: 3878713 (1975-04-01), Mole
patent: 4688421 (1987-08-01), Pzsolla
patent: 4845993 (1989-07-01), Horne
patent: 4938059 (1990-07-01), Fauche et al.
Duncan John R.
General Drawings Corporation, Convair Division
Gilliam Frank D.
Woodiel Donald O.
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