Horizon Inc.

David Adonis McFarlane

Matthew Scott Dunn

Ben Maples

Daniel Shane McFarlane

Cleaning reamer devices and methods for cleaning the interior of a valve guide are described. One cleaning reamer includes a straight shank, a body, and a piloted portion. The piloted portion is dimensionally sized and shaped to be substantially equivalent to the valve stem that is positioned within the valve guide to be cleared of deposits. The body of the cleaning reamer is fluted or straight.

Valve guide reamer for engines method and device

Wheel balancers and methods of their use are disclosed. One wheel balancer includes a cable and a base. The cable has a support end for being fastened to a support. The base is configured for receipt inside a wheel, and the base has proximal and distal ends and a hollow interior area for passing the cable therethrough. The cable passes through the base interior area and is operatively coupled to the base such that a distance between the cable support end and the base distal end is generally constant when the cable is extended. A pivot point for the cable is movable relative to the base between the base distal end and the cable support end.

Wheel balancer

Push-pull controls utilizing linear and rotational inputs to create linear output are disclosed. One control includes an elongate push rod and a roller pin. The rod has an outer surface, a generally circular cross-section perimeter, a center axis, a proximal end with a user input, and a distal end configured to directly or indirectly interact with an apparatus to be controlled. The rod is rotatable and slidable along the rod axis. The roller pin has a center axis and an outer surface that contacts the push rod outer surface. The roller pin center axis is angularly offset from and non-intersecting with the push rod center axis. The amount of angular offset is greater than zero degrees.

Push-pull control utilizing linear and rotational input

Aircraft systems having baffle seals with low coefficients of friction and methods of assembling aircraft systems are disclosed herein. In one embodiment, an aircraft system includes: (a) an aircraft baffle; (b) an aircraft cowl separated from the aircraft baffle by a gap, the aircraft cowl having a contact surface; and (c) a flexible aircraft baffle seal extending from the aircraft baffle to the aircraft cowl to seal the gap, the aircraft baffle seal having a contact side for contacting the contact surface of the aircraft cowl, the contact side having a kinetic coefficient of friction that is not more than 0.4, the aircraft baffle seal comprising an elastomer sheet and a laminate, the laminate being the contact side.

Growing community of inventors

Baldwin City, KS, United States of America

David Adonis McFarlane