Illinois Tool Works Inc.

Other

Jacuzzi Inc.

Oldcastle Precast, Inc.

Sca Tissue North America LLC

J. S. Land Management Corporation

Aalba Dent Inc.

Sca Hygiene Products Ab

Bio-plas, Inc.

Toolz, Ltd.

Bescal, Inc.

Wolfgang Ott

Folkert Fred Koch

Brian Michael Piety

Mark David Resendes

Eric C Freeman

Mark J Jurich

Jon R Reed

Alan J Janis

Paul A Jurich

Paul H Appelblom

Rickey G Swartz

Christopher Robin Drake

Christopher Tacklind

Russell G Wieser

Scott Takayuki Koizumi

Vince Benetti

Anatoly I Gosis

Garo J Paroonagian

Mark Brosius

Mark Swanson

Wilfrido Barajas

Utku Aksu

Donald H DeVaughn

David Adam

Donald H De Vaughn

Aragon Burlingham

Jonathan Carver

Thomas Zimmerman

Dale Arnold Miller

Steven Jones

Denise Marie Frazier

Raymond Dickinson

Michael Giddens

A pulley in a housing designed for use with a flexible flat strap in which low friction movable guides in the pulley housing allow the flexible flat strap to enter, pass through and exit the housing through windows in the housing without the flexible flat strap jamming the pulley or being worn by contact with an edge of a housing window.

Flat strap pulley

A method and system for producing, marking, and packaging ingots for use in fabricating dental prosthetics.

System and method for packaging dental ingots

A concrete lid for an in-ground utilities box includes a plastic reinforcement structure filled with concrete. The plastic reinforcement structure includes one or more plastic sidewalls that protect the edges of the lid from damage. The upper and lower surfaces of the lid are exposed concrete (with the exception of the upper and lower edges of the one or more plastic sidewalls). The one or more plastic sidewalls laterally surround a plastic reinforcement grid, which is centrally located between the upper and lower edges of the one or more plastic sidewalls. The one or more plastic sidewalls can be integrally formed with the plastic reinforcement grid. The plastic reinforcement grid reinforces the concrete lid, eliminating the need for separate reinforcement material. Support struts can be used to support the plastic reinforcement grid while wet concrete is being poured into the plastic reinforcing structure.

Utilities access closure

A preconditioned air connector (PCA) may be provided with a hollow body configured to pass a fluid flow, and a first mount assembly coupled to the hollow body. The first mount assembly may include a first cam joint with a first arcuate path of motion in a first plane generally tangential to the hollow body, a first mount coupled to the first cam joint, and a first lever coupled to the first cam joint. The first lever may be configured to actuate the first mount via a first transfer of motion through the first cam joint to draw the first mount inwardly toward the hollow body. In addition, the first mount may be configured to draw the hollow body and a mating component inwardly toward one another to pass the fluid flow between the hollow body and the mating component.

Preconditioned air connector assembly for aircraft

In certain embodiments, a preconditioned air connector has a hollow body configured to route a fluid therethrough and a hook member configured to mate with a cooperating element to draw the hollow body into fluid communication with a mating component. The preconditioned air connector also has a pivotable member actuatable along an arc tangential to the hollow body to direct axial translation of the hook member from a first position to a second position to draw the hollow body into fluid communication with the mating component. The pivotable member has an arcuate camming surface having a locking portion that secures the connector in a fully engaged position with respect to the mating component.

In certain embodiments, a PCA connector has a polyethylene body, wherein the polyethylene is durable, corrosion resistant, and exhibits excellent strength over a large range of temperature and moisture conditions. The polyethylene body may be described as a single structure with integral features, such as a bearing portion, a latch housing portion, a latch guide portion, and so forth. Thus, the number of parts is significantly reduced by the one-piece design of the body. In addition, the PCA connector may include a latching mechanism configured to secure the PCA connector to an aircraft. For example, the latching mechanism may include a pair of levers, which engage a pair of latches on opposite sides of the polyethylene body. In some embodiments, the levers may be rotated in opposite directions relative to one another to impart movement of the latches in the same direction, e.g., an axial direction. Also, some embodiments of the latching mechanism include a cam between the levers and the latches, respectively.

An aircraft powering system is provided which includes an aircraft electrical connector is provided with features to allow facile engagement with an aircraft and strong retention forces. The aircraft powering system may include the aircraft electrical connector having a unique biasing mechanism and modular construction, wherein the biasing mechanism is configured to place differential forces onto mating electrical connectors from an aircraft. The biasing mechanism may be operatively coupled to a handle or trigger, which may be easily engageable by an operator.

Aircraft electrical connector with differential engagement and operational retention forces

In certain embodiments, a PCA connector has a nylon body, wherein the nylon is durable, corrosion resistant, and exhibits excellent strength over a large range of temperature and moisture conditions. The nylon body may be described as a single structure with integral features, such as a bearing portion, a latch housing portion, a latch guide portion, and so forth. Thus, the number of parts is significantly reduced by the one-piece design of the body. In addition, the PCA connector may include a latching mechanism configured to secure the PCA connector to an aircraft. For example, the latching mechanism may include a pair of levers, which engage a pair of latches on opposite sides of the nylon body. In some embodiments, the levers may be rotated in opposite directions relative to one another to impart movement of the latches in the same direction, e.g., an axial direction. Also, some embodiments of the latching mechanism include a cam between the levers and the latches, respectively.

An aircraft electrical connector is provided with features to allow facile engagement with an aircraft and strong retention forces. The aircraft electrical system may include the aircraft electrical connector having a unique biasing mechanism and modular construction, wherein the biasing mechanism is configured to place differential forces onto mating electrical connectors from an aircraft. The biasing mechanism may be operatively coupled to a handle or trigger, which may be easily engageable by an operator. In one embodiment, an electrical connector may include a cam plate disposed between electrical connectors. The cam plate is configured to place differential forces on mating connectors inserted into the electrical connectors. In another embodiment, an electrical connector includes a moveable shaft that is disposed between electrical connectors. The shaft is configured to bias the position of the electrical connectors to place differential engagement and retention forces on mating connectors inserted into the electrical connectors.

Support tray

Water jet

Growing community of inventors

Antioch, CA, United States of America

Wolfgang Ott