Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1986-03-31
1987-03-10
Woodiel, Donald O.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
239426, 239434, 239545, B05B 704, G01M 900
Patent
active
046482679
ABSTRACT:
An atomizer (10) for a liquid has an air supply tube (20). Liquid supply tubes (26, 28) extend longitudinally along the air supply tube (20). The air supply tube (b 20) has at least one air orifice (22) extending from an inner surface (24) of the tube (20) through the tube. The liquid supply tubes (26, 28) are positioned on either side of the air orifices (22) and the liquid tubes are sealed to the air supply tube. The liquid supply tubes (26, 28) with facing liquid orifices (30) are positioned adjacent each of the air orifices 22. The liquid supply tubes (26, 28) are laterally spaced apart at the liquid orifices (30) a distance less than the diameter of the air orifices (22) to enable a beneficial venturi effect when the atomizer is in operation.
REFERENCES:
patent: 2515069 (1950-07-01), Zola
patent: 3606159 (1971-09-01), Sutton
patent: 3774842 (1973-11-01), Howell
patent: 3896666 (1975-07-01), Johnson et al.
patent: 4221339 (1980-09-01), Yoshikawa
Brekke Darrell G.
Manning John R.
Marchant Robert D.
The United States Government as represented by the Administrator
Woodiel Donald O.
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