Eugene E Smith

Address:

5720 Goldmount Ave, Las Vegas, NV 89107

VIN:

1D8HN44H38B139469

Make:

DODGE

Model:

CARAVAN

Year:

2008

Address:

2115 Rockaway Pkwy, Brooklyn, NY 11236

VIN:

2FMDK46C57BA91081

Make:

FORD

Model:

EDGE

Year:

2007

US Patent:

D639696, Jun 14, 2011

Filed:

Mar 10, 2009

Appl. No.:

29/333446

Inventors:

Eugene Charles Smith - Hermosa Beach CA, US
Jeffrey James Flynn - Hermosa Beach CA, US

Assignee:

Dream Capsule, LLC - Stillwater MN

International Classification:

1102

US Classification:

D11 79, D11 1

US Patent:

40947742, Jun 13, 1978

Filed:

Mar 10, 1975

Appl. No.:

5/556918

Inventors:

Eugene J. Smith - Valley Cottage NY

International Classification:

C02B 134
C02C 102

US Classification:

210 12

Abstract:

Aerobically decomposable liquors are oxygenated by continuously extracting a portion thereof from an aeration tank and saturating the liquor portion with oxygen within a separate receiver tank, thereafter returning the oxygenated liquor portion to the aeration tank. The continuously flowing liquor portion is cooled prior to its oxygenation so that its oxygen-absorbing capability is increased. Cooling is effected by extracting therefrom the heat required to gasify the initially liquified gas being introduced into the receiver tank as the oxygenating medium. Secondary cooling of the liquor portion before its oxygenation can be effected by extracting therefrom an additional amount of heat as required to gasify a second liquified gas, such as nitrogen. Such heat exchange may be conducted in a separate heat exchanger, but is preferably conducted via parallel and adjacent heat-conductive sections of the liquified gas and liquor supply conduits which are disposed within the bottom portion of the receiver tank so that they are immersed in the collecting oxygenated liquor, which then serves as the heat-conducting medium between them. Oxygen absorption capability of the liquor is further increased by the above-atmospheric pressure maintained within the receiver tank.

US Patent:

40212688, May 3, 1977

Filed:

Oct 15, 1975

Appl. No.:

5/622556

Inventors:

Eugene G. Smith - Long Beach CA

Assignee:

Robertshaw Controls Company - Richmond VA

International Classification:

H01L 3504

US Classification:

136228

Abstract:

The thermocouple has a sheath attached to an outer thermocouple element of a pair of coaxial thermocouple elements between hot and cold junctions of the thermocouple elements with the sheath extending away from the hot junction.

US Patent:

41102070, Aug 29, 1978

Filed:

Jan 5, 1976

Appl. No.:

5/646450

Inventors:

Eugene L. Smith - Stamford CT

Assignee:

American Cyanamid Company - Stamford CT

International Classification:

B03D 102

US Classification:

209166

Abstract:

Process for flotation of non-sulfide ores using partial esters of polycarboxylic acids having the following structure ##STR1## wherein R is an alkyl group of about 4 to 12 carbon atoms, R" is hydrogen or an alkyl group of up to 12 carbon atoms, n is a number 0-3, and R' is a bivalent grouping of a selected class in combination with fuel oil and alkali.

US Patent:

46182241, Oct 21, 1986

Filed:

Feb 8, 1985

Appl. No.:

6/699704

Inventors:

Eugene A. Smith - Hawthorne CA

Assignee:

Northrop Corporation - Hawthorne CA

International Classification:

G02B 508
G02B 510

US Classification:

350618

Abstract:

An aircraft laser system in which a laser beam is generated in one location (e. g. the fuselage) and transmitted via a relay mirror through a window externally of the aircraft structure to a receiver window at another location (e. g. a wing-tip pod). At the receiver, the laser beam passes through the window and is directed by relay mirrors to a turret, the turret receiving and directing the laser beam to an external target.

US Patent:

46772880, Jun 30, 1987

Filed:

Feb 11, 1985

Appl. No.:

6/700788

Inventors:

Eugene A. Smith - Hawthorne CA

Assignee:

Northrop Corporation - Hawthorne CA

International Classification:

F41G 700

US Classification:

250216

Abstract:

An optical turret shaped for minimum aerodynamic and aero-optic impact at supersonic speeds. The turret optics includes a common optical element for scanning the optical tracking beam and the projected laser beam to provide for automatic alignment of both beams. Separate windows associated with the tracking beam and the laser output beam is provided for increased efficiency, the window material in each window being compatibel with the optical wavelengths passing therethrough.