Zephyros, Inc.

Jason Walker

David K Carlson

Matthew Harthcock

Brandon Madaus

Charles L Taylor

Kearney Barton

Michael J Czaplicki

David Kosal

Kevin Hicks

Blake Synnestvedt

Yuan Lu

Eric A Franzoi

Ken Mazich

Austin O'Connor

Manish Taxak

Sajesh Madhavan

Austin O'connor

C L Taylor

An insert for structurally reinforcing a cavity of a structural member, wherein the insert includes a ballistic material to prevent penetration of the structural member by flying debris, fragmentation, or both.

Inserts having ballistic protection layer

The present teachings contemplate a method comprising providing a first and second substrate, locating an initiator onto a surface of the first or second substrate, the initiator including a substance for initiating polymerization of a polymerizable adhesive, locating the polymerizable adhesive onto a surface of the first and second substrate, the adhesive including a monofunctional, difunctional, or multifunctional methylene malonate, or cyanoacrylate, and contacting first and second substrate.

Malonate and cyanoacrylate adhesives for joining dissimilar materials

An adhesive material which comprises an epoxy component including a first flame retardant and a curing component which includes an adhesion promoter and a second flame retardant The epoxy component and curing component are present in a ratio of about 1:1 and the adhesive is formed when the epoxy component is combined with the curing component.

Adhesive material, and method of use thereof

The present teachings relate generally to a one part room temperature curable composition. e.g., a one-part epoxy-based adhesive precursor composition. The composition may include an epoxy resin, and a filler. The composition may include a flame retardant sufficient so that when the adhesive precursor composition is cored, it meets applicable requirements for flame retardancy of 14 C.F.R. &#xa7; 25.853 for aircraft inferior cabins. An amount of a curing agent may be included. The selection of the epoxy resin, curing agent, or both, may afford curing with or without the need for an application of heat. The epoxy resin, the filler, any flame retardant and the curing agent are admixed to define a substantially homogenous admixture, thereby defining a mass of adhesive precursor.

One part epoxy-based composition

An insert () comprising a core () and one or more extensions () extending from the core. The insert is adapted to be inserted into a cavity of a hollow tube-shaped member (). The hollow member can be a motorcycle handlebar or footrest. The insert can be made of metal or a polymer and can be an extrusion product.

Vibration damping insert

A panel structure and a method of forming the panel structure are disclosed. The panel structure typically includes at least one panel associated with a material. The panel structure has been found particularly advantageous for use as an interior panel of an airplane.

Panel structure

A panel assembly and method of making the same, whereby the panel assembly includes an adhesive located onto one or more edges of a layered honeycomb structure and a mesh material adhered in between the layered honeycomb structure by the adhesive.

Growing community of inventors

Lenox, MI, United States of America

Jason Walker