John R Kenyon

Address:

1045 Suwanee St, Safety Harbor, FL 34695

Phone:

7277918396

VIN:

1GCEC14X98Z309290

Make:

CHEVROLET

Model:

SILVERADO 1500

Year:

2008

US Patent:

20170186288, Jun 29, 2017

Filed:

Jul 11, 2016

Appl. No.:

15/207256

Inventors:

- Plymouth MN, US
Jonathan L. Carter - New Port Richey FL, US
John R. Kenyon - Safety Harbor FL, US
Jay B. Cleckler - Long Beach CA, US
Mark E. Walker - Fullerton CA, US

International Classification:

G08B 13/16
G08B 13/194
G08B 13/19

Abstract:

A multi-spectral detection device is provided that includes a housing, a bezel spacer, a microphone, an end cap and electro-optical sensors mounted to the end cap. The housing has an inner chamber that holds sensor components. The bezel spacer has a first end and an opposed, second end. The first end of the bezel spacer extends from a first end of the housing. The bezel spacer has a central bezel passage leading to the inner chamber of the housing. The bezel spacer further has at least four side walls. Each side wall is positioned 90 degrees away from an adjacent side wall. A microphone is coupled to each side wall of the bezel spacer in such a manner that each microphone is faced 90 degrees with respect to an adjacent microphone to form a compact acoustic array. The end cap is coupled to the second end of the bezel spacer and the electro-optical sensors are mounted to the end cap.

US Patent:

20160111008, Apr 21, 2016

Filed:

Nov 2, 2015

Appl. No.:

14/930376

Inventors:

- Dulles VA, US
John R. Kenyon - Safety Harbor FL, US

International Classification:

G08G 5/04
G06T 7/60
G06K 9/62

Abstract:

A method of operating a rotorcraft collision avoidance system is provided. The method includes determining a unique characteristic of a detected rotorcraft, determining the actual length of a first rotor based at least in part on the determined unique characteristic of the rotorcraft, locating a major axis of the first rotor of the rotorcraft from a perspective of a home unit, from the perspective of the home unit, determining an angular extent of the major axis of the first rotor, and determining the then current distance from the home unit to the rotorcraft based at least in part on the determined actual length of the first rotor and the corresponding angular extent.

US Patent:

20150355350, Dec 10, 2015

Filed:

Mar 13, 2013

Appl. No.:

13/799519

Inventors:

- Dulles VA, US
Jonathan L. Carter - New Port Richey FL, US
John R. Kenyon - Safety Harbor FL, US
Jay B. Cleckler - Long Beach CA, US
Mark E. Walker - Fullerton CA, US

International Classification:

G01V 1/00
G01V 8/10

Abstract:

A multi-spectral detection device is provided that includes a housing, a bezel spacer, a microphone, an end cap and electro-optical sensors mounted to the end cap. The housing has an inner chamber that holds sensor components. The bezel spacer has a first end and an opposed, second end. The first end of the bezel spacer extends from a first end of the housing. The bezel spacer has a central bezel passage leading to the inner chamber of the housing. The bezel spacer further has at least four side walls. Each side wall is positioned 90 degrees away from an adjacent side wall. A microphone is coupled to each side wall of the bezel spacer in such a manner that each microphone is faced 90 degrees with respect to an adjacent microphone to form a compact acoustic array. The end cap is coupled to the second end of the bezel spacer and the electro-optical sensors are mounted to the end cap.