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Preston R Bates, 59Jacksonville, FL

Preston Bates Phones & Addresses

Jacksonville, FL   

6337 Inca Rd, Fort Worth, TX 76116    817-7639359   

Clarksville, TN   

1290 Gate Post Ct, Powder Springs, GA 30127    770-2228044   

Marietta, GA   

Atlanta, GA   

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Preston Bates resumes & CV records

Resumes

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Preston Bates

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Preston Bates

Education:
Orange Glen High School
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Preston Bates

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Preston Bates

Publications & IP owners

Us Patents

Method Of Determining A Maneuver Performed By An Aircraft

US Patent:
2011026, Oct 27, 2011
Filed:
Feb 18, 2011
Appl. No.:
13/030582
Inventors:
Preston R. Bates - Fort Worth TX, US
Mark W. Davis - Southbury CT, US
James Peter Cycon - Media PA, US
Payman Sadegh - Arlington VA, US
Assignee:
SIKORSKY AIRCRAFT CORPORATION - Stratford CT
International Classification:
G06F 19/00
G01M 17/00
US Classification:
701 14
Abstract:
A method of determining a maneuver performed by an aircraft having sensors for monitoring motion data, the method including periodically sampling the sensors to electronically determine segments of motion data of the aircraft; aggregating sequences of the segments of the motion data; comparing the aggregated segments of motion data to models of particular maneuvers; and determining the maneuver performed by the aircraft.

System And Method For Health Assessment Of Aircraft Structure

US Patent:
2017018, Jun 29, 2017
Filed:
Apr 1, 2015
Appl. No.:
15/300655
Inventors:
- Stratford CT, US
Preston R. Bates - Fort Worth TX, US
Mark W. Davis - Southbury CT, US
International Classification:
B64F 5/60
G07C 5/08
Abstract:
A method of health monitoring and assessment of an aircraft structure includes collecting data from a plurality of sensors located at one or more components of the aircraft. The sensors assess a physical condition of the components and are arrayed in one or more aircraft zones. The data is communicated to a health assessment module, which calculates one or more component structural condition indicators of each component. The component structural condition indicators are compiled and one or more component structural health indicators are calculated. The component structural health indicators are compiled by aircraft zone and a zone structural health indicator is calculated based on the component structural health indicators of components residing in the particular aircraft zone. An aircraft level health indicator is calculated based on the zone structural health indicators and one or more maintenance actions are recommended based on the structural condition and health indicators.

Damage Adaptive Control

US Patent:
2015030, Oct 22, 2015
Filed:
Jun 29, 2015
Appl. No.:
14/753318
Inventors:
- Stratford CT, US
Vineet Sahasrabudhe - Cheshire CT, US
Jonathan K. Garhart - Seymour CT, US
Preston R. Bates - Fort Worth TX, US
International Classification:
G05D 1/00
B64D 45/00
Abstract:
Embodiments of the disclosure are directed to measuring, via at least one sensor, at least one of a damage and a compromise associated with a vehicle, determining at least one of a region and a location of the at least one of a damage and a compromise and a level of the at least one of a damage and a compromise, and adapting an operational envelope for the vehicle based on the determined at least one of a region and a location of the at least one of a damage and a compromise and the level of the at least one of a damage and a compromise.

Damage Adaptive Control

US Patent:
2014024, Aug 28, 2014
Filed:
Feb 28, 2013
Appl. No.:
13/780987
Inventors:
- Stratford CT, US
Vineet Sahasrabudhe - Cheshire CT, US
Jonathan K. Garhart - Seymour CT, US
Preston R. Bates - Fort Worth TX, US
Assignee:
SIKORSKY AIRCRAFT CORPORATION - Stratford CT
International Classification:
B64C 19/00
US Classification:
701 3, 701 292, 701 99
Abstract:
Embodiments of the disclosure are directed to measuring, via at least one sensor, at least one of a damage and a compromise associated with a vehicle, determining at least one of a region and a location of the at least one of a damage and a compromise and a level of the at least one of a damage and a compromise, and adapting an operational envelope for the vehicle based on the determined at least one of a region and a location of the at least one of a damage and a compromise and the level of the at least one of a damage and a compromise.

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