Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1989-10-03
1990-07-03
Woodiel, Donald O.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
G01M 900
Patent
active
049380591
ABSTRACT:
A strain gauge balance consisting of an outer longitudinal shell and a monopiece inner center core; the outer shell having a open end and a closed end with a frustoconical bore extending towards the closed end, and the inner core having frusto conical shaped ends, one end being sized to fit within the frusto conical core and the other end being sized to fit into a sting; four radially extending, equally spaced, webs formed within the core and at each end of the core inboard of the frusto conical ends, and a central region of two longitudinally separated, semicircular cross-section parts each being formed within the part, with tensioning rings, one disposed diagonally to the other, and a number of strain gauges secured to the webs and the rings to determine induced strain in 6 degrees of freedom.
REFERENCES:
patent: 2785569 (1957-03-01), Miller
patent: 2885890 (1959-05-01), Liccini et al.
patent: 3019643 (1962-02-01), Curry
patent: 3159027 (1964-12-01), Curry
patent: 3412604 (1968-11-01), Iandolo
patent: 4074567 (1978-02-01), Horanoff
patent: 4688421 (1987-08-01), Pzsolla
Faucher Gilles
Girard Bertrand
Paradis Marc-Andre
Her Majesty the Queen in right of Canada as represented by the
Hinds William R.
Woodiel Donald O.
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