Kenneth Martin Gardner

US Patent:

8328147, Dec 11, 2012

Filed:

Jun 10, 2009

Appl. No.:

12/481574

Inventors:

Kenneth R. Gardner - Phoenix AZ, US
Jonathan L. Gardner - Glendale AZ, US

International Classification:

F16M 11/00

US Classification:

2481761, 248121, 248156, 124 86, 124 88

Abstract:

The present invention relates generally to devices and methods for assisting archery bow hunters in making accurate shots while hunting in dynamic terrain. Generally, in accordance with various exemplary embodiments of the present invention, the present invention discloses various universal mounting brackets and integrated archery bow systems configured for coupling a support element to an archery bow. Most preferably, the universal mounting brackets and integrated archery bow systems are configured to give the bow hunter maximum stability and range of motion when aiming and/or firing the bow. In accordance with the various exemplary embodiments of the present invention, various universal mounting brackets and integrated archery bow systems configured for coupling a collapsible monopod support element to an archery bow is disclosed. Additionally, various universal mounting brackets configured for coupling an extendable bipod support element to an archery bow is disclosed.

US Patent:

8353484, Jan 15, 2013

Filed:

Nov 10, 2009

Appl. No.:

12/615895

Inventors:

Kenneth D. Gardner - Wichita KS, US

Assignee:

Textron Innovations, Inc. - Providence RI

International Classification:

B64C 19/02

US Classification:

244235

Abstract:

A cockpit rudder control mechanism is described for accepting aircraft control input utilizing rudder pedals depending from a movable carriage to rotate a shaft. The mechanism may be removed from the aircraft for maintenance and the position of the mechanism within the aircraft may be adjusted for a particular user. Movement of the rudder pedals is conveyed by linkages to a collar which rotates a shaft. The rotation of the shaft is measured for control input to the aircraft or is transferred to the mechanical control systems for the aircraft.

US Patent:

20130233292, Sep 12, 2013

Filed:

Oct 26, 2012

Appl. No.:

13/694096

Inventors:

Kenneth R. Gardner - Phoenix AZ, US

International Classification:

F41B 5/14

US Classification:

124 256

Abstract:

A portable archery bow apparatus can be transported to any of a plurality of locations to contact the ground and to provide support and stability while firing an arrow from the bow apparatus. The apparatus includes a bow and includes a support pole attached to a side of the bow. The bottom of the pole rests on the ground while the bow is utilized to fire an arrow. The pole permits the bow to be tilted fore and aft, and from side to side while the bow is positioned to fire an arrow from the bow.

US Patent:

55929583, Jan 14, 1997

Filed:

Feb 1, 1995

Appl. No.:

8/382077

Inventors:

Kenneth D. Gardner - Apache Junction AZ

Assignee:

Coates, Asi, Inc. - Phoenix AZ

International Classification:

B08B 304

US Classification:

134122R

Abstract:

Apparatus for processing a thin circuit board substrate includes upper and lower input roller assemblies and upper and lower output roller assemblies. A liquid reservoir extends between the input roller assemblies and the output roller assemblies. The thin substrate travels from the input roller assemblies, through the reservoir, and exits the reservoir via the output roller assemblies. The lower input roller assembly includes alternating rollers of different diameter which permit the interleaving of disks with the lower input roller assembly.

US Patent:

20200023936, Jan 23, 2020

Filed:

Jul 19, 2018

Appl. No.:

16/039968

Inventors:

- Mobile AL, US
Kenneth D. GARDNER - Wichita KS, US

International Classification:

B64C 1/18

Abstract:

A method and apparatus for installing an aircraft cabin floor module inside an aircraft fuselage is disclosed. The cabin floor module is attached to the fuselage with a plurality of linkages having a spherical bearing at each end to allow for the alignment and adjustment of the cabin floor module, and a second joint which includes a lug having a double eccentric bushing which will allow the fastening apertures at the second interface point to line up with precision.