The Boeing Company

Gary Robert Weber

Daniel James Kane

Matthew Leroy Anderson

David Howard Gane

Terry C Tomt

Ricole Allison Johnson

Ryan J Glamm

Frederick John Feiertag

Tyre Glenn Boss

Ronald Hitzeman

Simon R Walter

Genji Mizushima

Kelly William Meloy

Michael J Reberg

Takeshi Kawase

Peter D Verge

Pradip K Saha

Mark E Bice

Azzréal Pugh

Clinton J Campbell

A method for forming a structure using an interim temper process is provided. A metal material is partially-aged to a stable temper that does not require cold storage. The partially-aging step is completed at a supplier facility prior to the metal material being received by the manufacturer. Once received by the manufacturer, the partially-aged metal material is heated to a first temperature to perform retrogression. A structure is formed from the partially-aged metal material after performing the retrogression. The structure is shaped and inspected. The structure is then heated to a second temperature in an age oven to reach its final aged state. The final aged state may be close to, meet, or exceed a T6 temper.

Interim temper process

A method, system, and apparatus for a part forming system. The part forming system comprises a field shaper having a cavity configured to receive a workpiece and a die. The field shaper has a number of dimensions based on being inserted into a main coil. The workpiece is bent to form a part with a desired shape when an electromagnetic field from the main coil is applied to the field shaper while the field shaper is located within the main coil.

Electromagnetic field shaping system and method

A method for manufacturing a part including steps of (1) casting an ingot, (2) scalping the ingot to yield a scalped ingot, (3) homogenizing the scalped ingot to yield a homogenized ingot, (4) breakdown of the homogenized ingot to yield a slab, (5) rolling the slab to yield a rolled aluminum material, (6) annealing the rolled aluminum material to yield an aluminum starting material, (7) cold working the aluminum starting material to obtain an aluminum cold worked material, and (8) forming the part from the aluminum cold worked material.

Method for manufacturing anodized aluminum alloy parts without surface discoloration

An interpenetrating polymer network (IPN) adhesive comprises an acrylated polymer system curable by radiation, and a flexible epoxy system thermally curable after the acrylated polymer system is cured.

Bonding composite structures using interpenetrating polymer network adhesives

A method for manufacturing a part including steps of providing an aluminum starting material, wherein the aluminum starting material is in an anneal temper, cold working the aluminum starting material to obtain an aluminum cold worked material, and forming the part from the aluminum cold worked material.

A composition is provided that consists essentially of a first polymer system and a second polymer system. The first polymer system has a first modulus of about 180 ksi to about 335 ksi. The first polymer system consists essentially of a thermosetting acrylate. The second polymer system consists essentially of a thermosetting epoxy system and an epoxy curing agent. The thermosetting epoxy system comprises a first epoxy.

Composite structures using interpenetrating polymer network adhesives

A monolithic structure for use as a pressure bulkhead for an aircraft includes a first web, a redundant second web spaced from the first web, stiffeners disposed between and connecting the webs to each other, and first and second outer attachment rings respectively provided on the outer peripheries of the first and second webs for attaching the bulkhead to fuselage structure. One of the webs comprises a pressure web for supporting pressure loading, and the other web defines at least one aperture therethrough. The stiffeners are integrally fabricated along with at least one of the webs and associated attachment ring as a one-piece monolithic part.

Growing community of inventors

Kent, WA, United States of America

Gary Robert Weber