James S Burgess

US Patent:

6622739, Sep 23, 2003

Filed:

Mar 12, 2001

Appl. No.:

09/803800

Inventors:

Robert M. Rice - Huntsville AL
James Fletcher Burgess - Huntsville AL
Kirk E. McLauchlin - Madison AL

Assignee:

Advanced Systems Technologies, Inc. - Huntsville AL

International Classification:

B08B 300

US Classification:

134184, 134134, 134116, 134119, 134123, 134129, 15302, 405 53

Abstract:

An oxide and coating removal system includes a mobile gantry or transport system supporting an end effector and high energy waterjet rotating nozzles judiciously located relative to the surface of the vehicle and includes positioning mechanism for locating the nozzle discretely relative to the vehicle. An environmentally safe system serves to re-claim the effluent by removing the contaminated particles and returning the re-claimed water to the pumping system.

US Patent:

H6572, Aug 1, 1989

Filed:

Sep 2, 1988

Appl. No.:

7/239814

Inventors:

Roy L. Cameron - Athens AL
James S. Burgess - Harvest AL

Assignee:

The United States of America as represented by the Secretary of the Army - Washington DC

International Classification:

G01C 1738

US Classification:

73 1C

Abstract:

A torque calibrator which has a pair of torque beams with hydraulic cylins for exerting forces on opposite ends of the torque beams and with load cells mounted at opposite ends of the beams for measuring the forces applied to the beams with the beams being designed for a torque cell to be mounted between the beams for having torque applied to the torque cell to calibrate the torque cell.

US Patent:

59644184, Oct 12, 1999

Filed:

Dec 13, 1997

Appl. No.:

8/990209

Inventors:

Jack G. Scarpa - Huntsville AL
James Fletcher Burgess - Huntsville AL
John D. Marlin - Tony AL
Matthew Kelly - Huntsville AL
Anthony Howard - Huntsville AL

Assignee:

USBI Co. - Kennedy Space Center FL

International Classification:

B05B 708

US Classification:

239424

Abstract:

A convergent spray gun which combines a liquid resin and dry metallic powder externally of the nozzle of the spray gun that utilizes a pair of diametrically opposing passages disposed at 0. degree. and 180. degree. relative to the central resin discharging orifice where the central orifice is approximately 0. 015 inch and the air for atomizing the fluids is approximately 0. 187 inch and the atomizing angle is approximately 90. degree. The metallic filler is added to the plume of the convergent spray at the low pressure section and the ratio of the fluids are controlled by a computerized system. The spray gun, controls and mixing chambers of the resin (two part) and powder fillers are housed in separate rooms and the dust where the powder fillers are metered is controlled.

US Patent:

61363790, Oct 24, 2000

Filed:

Jun 30, 1999

Appl. No.:

9/345151

Inventors:

Jack G. Scarpa - Huntsville AL
James Fletcher Burgess - Huntsville AL
John D. Marlin - Tony AL
Matthew Kelly - Huntsville AL
Anthony Howard - Huntsville AL

Assignee:

USBI Co. - Kennedy Space Center FL

International Classification:

B05D 134

US Classification:

427426

Abstract:

A convergent spray gun which combines a liquid resin and dry metallic powder externally of the nozzle of the spray gun that utilizes a pair of diametrically opposing passages disposed at 0. degree. and 90. degree. relative to the central resin discharging orifice where the central orifice is approximately 0. 015 inch and the air for atomizing the fluids is approximately 0. 187 inch and the atomizing angle is approximately 180. degree. The metallic filler is added to the plume of the convergent spray at the low pressure section and the ratio of the fluids are controlled by a computerized system. The spray gun, controls and mixing chambers of the resin (two part) and powder fillers are housed in separate rooms and the dust where the powder fillers are metered is controlled.

US Patent:

20210265643, Aug 26, 2021

Filed:

Feb 24, 2020

Appl. No.:

16/799470

Inventors:

- Morris Plains NJ, US
James Tory Burgess - Madison AL, US

International Classification:

H01M 8/04119
H01M 8/22
H01M 8/04082
B64C 39/02

Abstract:

An air system includes a fuselage, a motor supported by the fuselage, a propeller coupled to the motor, a fuel cell-based power generator supported by the fuselage and the motor, and a satellite communication system coupled to the fuel cell system. The generator includes a hydrogen generator, a fuel cell having an anode and a cathode, a cathode loop configured to provide oxygen to the cathode, an anode loop configured to provide hydrogen generated by the hydrogen generator to the anode, and an electrical connector coupled to the fuel cell to provide electricity generated by the fuel cell to the motor.