Robert Lee Parks

Address:

3531 Upfield Dr, Houston, TX 77082

Phone:

(713)6959195

VIN:

3VWDX7AJ3CM458613

Make:

VOLKSWAGEN

Model:

JETTA

Year:

2012

Address:

3531 Upfield Dr, Houston, TX 77082

VIN:

2GCEC19J271547302

Make:

CHEVROLET

Model:

SILVERADO 1500

Year:

2007

US Patent:

6735809, May 18, 2004

Filed:

May 9, 2002

Appl. No.:

10/141734

Inventors:

Robert T. Parks - Houston TX

Assignee:

XStreamline Products, Inc. - Houston TX

International Classification:

A47L 1312

US Classification:

15118, 152091, 152441, 152444

Abstract:

A hand-held pad is disclosed for cleaning, waxing, rubbing, polishing and applying liquid or semi-liquid to surfaces. The pad has at least four faces that are in non-parallel planes to every other face. Each face has a wide end tapered to a narrow end. Each face may have different texture, absorbency and/or abrasiveness than each other face. The hand-held pad provides ergonomic advantages and may be used on a variety of surfaces and/or materials.

US Patent:

8061646, Nov 22, 2011

Filed:

Sep 15, 2008

Appl. No.:

12/210711

Inventors:

Martin L. Gomez - Fairfax VA, US
Robert Parks - San Jose CA, US
Adam J. Woodworth - Melrose MA, US

Assignee:

Aurora Flight Sciences Corporation - Manassas VA

International Classification:

B64C 37/02
B64C 23/06
B64D 5/00

US Classification:

244 2, 244 1 TD, 2441993

Abstract:

A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure.

US Patent:

8172172, May 8, 2012

Filed:

Nov 18, 2011

Appl. No.:

13/299924

Inventors:

Martin L. Gomez - Fairfax VA, US
Robert Parks - San Jose CA, US
Adam J. Woodworth - Melrose MA, US

Assignee:

Aurora Flight Sciences Corporation - Manassas VA

International Classification:

B64C 37/02
B64C 23/06

US Classification:

244 2, 2441993, 244 3, 244 1 TD

Abstract:

A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure.

US Patent:

8226025, Jul 24, 2012

Filed:

Nov 18, 2011

Appl. No.:

13/299883

Inventors:

Martin L. Gomez - Fairfax VA, US
Robert Parks - San Jose CA, US
Adam J. Woodworth - Melrose MA, US

Assignee:

Aurora Flight Sciences Corporation - Manassas VA

International Classification:

B64C 37/02
B64C 23/06
B64D 5/00

US Classification:

244 2, 244 3, 2441992, 2441993, 244 1 TD

Abstract:

A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure.

US Patent:

20090314886, Dec 24, 2009

Filed:

Jun 12, 2008

Appl. No.:

12/137901

Inventors:

Tom Clancy - Washington DC, US
Robert Parks - San Jose CA, US

Assignee:

Aurora Flight Sciences Corporation - Manassas VA

International Classification:

B64C 1/00
B64C 3/56
B64C 25/10

US Classification:

244 1TD, 244 49, 244102 R, 24115 R

Abstract:

A system for deploying a deployable structure in an aircraft, comprising a drogue parachute, at least one deployable structure, a riser line attached to the drogue parachute and the at least one deployable structure, wherein when the drogue parachute is deployed, a tension is applied to the riser line, and a parachute deployment system, wherein the parachute deployment system is configured to utilize the applied tension to deploy the at least one deployable structure.

US Patent:

20130319727, Dec 5, 2013

Filed:

Jul 30, 2012

Appl. No.:

13/561598

Inventors:

ED WEN - BRISTOW VA, US
ADAM SCOTT EHRMANTRAUT - DUMFRIES VA, US
ROBERT PARKS - SAN JOSE CA, US

Assignee:

AURORA FLIGHT SCIENCES CORPORATION - Manassas VA

International Classification:

H01B 7/08
B32B 37/14

US Classification:

174117FF, 156 60, 1563071, 174117 R

Abstract:

An aircraft conductor sandwich assembly configured to be embedded in a composite aircraft structure. The conductor sandwich assembly comprises a plurality of carbon conductors disposed between two sheets of insulating layers and an adhesive resin bonding the plurality of carbon conductors and the two sheets of insulating layers into a carbon sandwich assembly such that (i) the conductors are electrically isolated and (ii) structural loads can be passed through said conductor sandwich assembly.

US Patent:

RE346683, Jul 19, 1994

Filed:

May 31, 1991

Appl. No.:

7/708810

Inventors:

Robert E. Parks - Houston TX
Robert L. Marietta - Needville TX

Assignee:

Nitec, Inc. - Houston TX

International Classification:

G01N 2176
G01N 3112

US Classification:

436114

Abstract:

In one exemplar embodiment, a chemiluminescent nitrogen detector for detecting chemically-bound nitrogen in an organic compound is provided in which a discrete sample of the organic compound containing the chemically-bound nitrogen is injected into a high temperature furnace where the sample is pyrolyzed at extremely high temperatures in an oxygen rich atmosphere to form nitric oxide. The pyrolysis gases, including nitric oxide is then applied to a drying means for eliminating a substantial quantity of water vapor from the carried pyrolysis gases to insure that the dew point of the gases is below the operating temperature of a nitric oxide and ozone reaction chamber. The nitric oxide and ozone are mixed in a reaction chamber to form metastable nitrogen dioxide which instantaneously relaxes to its ground state with a resulting photo-emission of light energy. The chemiluminescent detection is based on this photo-emission of light energy, and emitted light is detected by a photo-multiplier tube whose output is an electrical potential proportional to the intensity of the light detected. Appropriate electronic circuitry may be provided to convert the electrical potential output of the photo-multiplier tube to an analog electrical signal for driving a chart recorder and for application to an integrator for deriving and displaying a digital count that is proportional to the quantitative value of the chemically-bound nitrogen contained in the sample.

US Patent:

40185621, Apr 19, 1977

Filed:

Oct 24, 1975

Appl. No.:

5/625510

Inventors:

Robert E. Parks - Houston TX
Robert L. Marietta - Richmond TX

Assignee:

Antek Instruments, Inc. - Houston TX

International Classification:

G01N 2124
G01N 3112
G01N 3108

US Classification:

23230PC

Abstract:

In one exemplar embodiment, a chemiluminescent nitrogen detector for detecting chemically-bound nitrogen in an organic compound is provided in which a discrete sample of the organic compound containing the chemically-bound nitrogen is injected into a high temperature furnace where the sample is pyrolyzed at extremely high temperatures in an oxygen rich atmosphere to form nitric oxide. The pyrolysis gases, including nitric oxide is then applied to a drying means for eliminating a substantial quantity of water vapor from the carried pyrolysis gases to insure that the dew point of the gases is below the operating temperature of a nitric oxide and ozone reaction chamber. The nitric oxide and ozone are mixed in a reaction chamber to form metastable nitrogen dioxide which instantaneously relaxes to its ground state with a resulting photo-emission of light energy. The chemiluminescent detection is based on this photo-emission of light energy, and emitted light is detected by a photo-multiplier tube whose output is an electrical potential proportional to the intensity of the light detected. Appropriate electronic circuitry may be provided to convert the electrical potential output of the photo-multiplier tube to an analog electrical signal for driving a chart recorder and for application to an integrator for deriving and displaying a digital count that is proportional to the quantitative value of the chemically-bound nitrogen contained in the sample.