Ques Tek Innovations, LLC

Apple Inc.

Motorola Corporation

Xtalic Corporation

Panduit Corporation

Horizon Systems Machining, Inc.

James A Wright

Abhijeet Misra

Jason T Sebastian

Herng-Jeng Jou

Jiadong Gong

David R Snyder

Stephen Brian Lynch

Matthew D Hill

Christopher S Graham

James A Curran

Brian S Tryon

Evgeniya Freydina

Karl Ruben F Larsson

William A Counts

Alan C Lund

Guangtao Zhang

Brian M Gable

Colin M Ely

Christopher Matthew Werner

Naoto Matsuyuki

Robert J Schwendeman

Gregory B Olson

James A Yurko

Daniel T McDonald

Leonard E Nelson

Ali Saidi

Jose Gutman

Zechariah D Feinberg

Charles J Kuehmann

Weiming Huang

Zechariah Feinberg

Raymund W M Kwok

Shiyun Ruan

Jason Reese

Joshua Garth Abbott

Robert Daniel Hilty

Lisa J Chan

Jeremy Hoishun Li

Jason Sebastian

Jeffrey Lee Mattlin

John Richard Kane

Hoishun Li

Lei Gao

Yoshihiko Yokoyama

Eric W Hamann

Brian P Demers

Wai Man Raymund Kwok

Casimir M Guzay

Darrell A Pfeffer

Thomas S Kozmel, Ii

Jin-Won Jung

Chune-Ching Young

Chun-Hsien Chiang

Dana J Frankel

Herng-Jen Jou

Weijia Tang

Ethan E Currens

Clay A Houser

William Arthur Counts

Walter Lee Davis

Angel J Kegg

Robert John Schwendeman

Weija Tang

Provided herein are titanium alloys that can achieve a combination of high strength and high toughness or elongation, and a method to produce the alloys. By tolerating iron, oxygen, and other incidental elements and impurities, the alloys enable the use of lower quality scrap as raw materials. The alloys are castable and can form &#x3b1;-phase laths in a basketweave morphology by a commercially feasible heat treatment that does not require hot-working or rapid cooling rates. The alloys comprise, by weight, about 3.0% to about 6.0% aluminum, 0% to about 1.5% tin, about 2.0% to about 4.0% vanadium, about 0.5% to about 4.5% molybdenum, about 1.0% to about 2.5% chromium, about 0.20% to about 0.55% iron, 0% to about 0.35% oxygen, 0% to about 0.007% boron, and 0% to about 0.60% other incidental elements and impurities, the balance of weight percent comprising titanium. There exists an unmet need to produce titanium alloys for use in aerospace applications which have a refined equiaxed grain structure. This can be beneficial for fatigue critical applications. The technology developed by QuesTek describes a titanium alloy and manufacturing methods thereof to obtain equiaxed grains on the order of 300 microns and corresponding UTS of approximately 170 ksi. In addition, various forms of the alloys are disclosed including ingots, billets, powders and wire in accord with the described microstructure and physical characteristics.

Titanium alloys

The disclosure provides an aluminized composite including a base material. The aluminized composite may also include a diffusion layer disposed over the base material. The aluminized composite may further include an aluminum material disposed over the diffusion layer.

Coloring of metallic materials coated with aluminum

A mold apparatus to form a ceramic (or glass) includes a first mold portion having a first coefficient of thermal expansion and a second mold portion having a second coefficient of thermal expansion. In some embodiments, the first mold portion and/or the second mold portion are substantially immiscible with the ceramic material, such as silicon oxide, at a temperature greater than 600&#xb0; C. In some embodiments, the first coefficient of thermal expansion and the second coefficient of thermal expansion are substantially similar to that of the glass or ceramic material. In some embodiments, the first coefficient of thermal expansion is different from the second coefficient of thermal expansion. In some embodiments, the first mold portion and the second mold portion contain a surface coating and a passivation layer.

Mold materials for formed ceramic

The disclosure provides methods of making iron-based alloys, as well as resulting alloys. An iron-based alloy containing a small amount of nickel (e.g., 0.5 to 2.0 wt %) is annealed and machined. The alloy is sufficiently ductile to reduce the likelihood of cracking, while not sufficiently high to result in a hardened alloy. After the alloy is shaped, the alloy is hardened by nitriding.

Steel compositions and solution nitriding of stainless steel thereof

A beryllium-free high-strength copper alloy includes, about 10-30 vol % of L1-(Ni,Cu)(Al,Sn), and substantially excludes cellular discontinuous precipitation around grain boundaries. The alloy may include at least one component selected from the group consisting of: Ag, Cr, Mn, Nb, Ti, and V, and the balance Cu.

Beryllium-free high-strength copper alloys

The disclosure provides an aluminum alloy including having varying ranges of alloying elements. In various aspects, the alloy has a wt % ratio of Zn to Mg ranging from 4:1 to 7:1. The disclosure further includes methods for producing an aluminum alloy and articles comprising the aluminum alloy.

Aluminum alloys with high strength and cosmetic appeal

Alloys, processes for preparing the alloys, and articles including the alloys are provided. The alloys can include, by weight, about 0.01% to about 1% vanadium, 0% to about 0.04% carbon, 0% to about 8% niobium, 0% to about 1% titanium, 0% to about 0.04% boron, 0% to about 1% tungsten, 0% to about 1% tantalum, 0% to about 1% hafnium, and 0% to about 1% ruthenium, the balance essentially molybdenum and incidental elements and impurities.

Ductile high-temperature molybdenum-based alloys

Techniques for forming an enclosure comprised of an aluminum alloy are disclosed. In some embodiments, aluminum ions and metal element ions can be dissolved in a non-aqueous ionic liquid in an electrolytic plating bath. A reverse pulsed electric current can facilitate in co-depositing the aluminum ions and the metal element ions onto a metal substrate. The resulting aluminum alloy layer can include nanocrystalline structures, which can impart the alloy layer with increased hardness and increased resistance to scratching, corrosion, and abrasion. In some embodiments, the metal element ion is chromium and the aluminum alloy layer includes a chromium oxide passivation layer formed via a passivation process. Subsequent to the passivation process, the formation of the chromium oxide layer does not impart a change in color to the aluminum alloy layer. In some embodiments, hafnium ions are co-deposited with aluminum ions to form an aluminum hafnium alloy.

Nanostructured aluminum alloys for improved hardness

Techniques for forming an enclosure comprised of aluminum zirconium alloy layer are disclosed. In some embodiments, aluminum ions and zirconium ions can be dissolved in a non-aqueous ionic liquid in an electrolytic plating bath. A reverse pulsed electric current can facilitate in co-depositing the aluminum ions and the zirconium ions onto a metal substrate. The resulting aluminum zirconium alloy layer can include nanocrystalline grain structures, which can impart the alloy layer with increased hardness and increased resistance to scratching, denting, and abrasion. In some embodiments, the aluminum zirconium alloy layer can be anodized to form an aluminum oxide layer. Subsequent to the anodization operation, the oxidized layer is able to retain its substantially neutral color.

Nanostructured aluminum zirconium alloys for improved anodization

The disclosure provides aluminum alloys having varying ranges of alloying elements and properties. The aluminum alloys have a wt % ratio of Zn to Mg from 2.5 to 3.5.

An enclosure is formed by coupling an outer cover to a back enclosure piece. The enclosure defines an interior volume for receiving components of an electronic device. The back enclosure piece is formed from a metal frame component and a non-metal outer cover. A metal layer overlaps the metal frame component and the outer cover within the interior volume. The metal layer has a thickness that provides support and shatter resistance to the non-metal outer cover. The metal layer can form an inductor of a wireless power transfer circuit.

Enclosure with metal interior surface layer

An alloy includes, in weight percentage, about 20.0% to about 25.0% chromium, 0% to about 5.0% molybdenum, about 3.0% to about 15.0% cobalt, about 1.5% to about 6.0% niobium, about 1.0% to about 3.0% tantalum, about 1.0% to about 5.0% tungsten, 0% to about 1.0% aluminum, 0% to about 0.05% carbon, 0% to about 0.01% titanium, and the balance nickel and incidental elements and impurities, wherein the alloy includes L1and D0precipitates in a compact morphology.

Nickel-based alloys

An electroformed binary copper alloy comprising copper and X, where X is selected from the group consisting of Cr, Fe, W, Mo, B, Co, Ag, and P, having a yield strength of at least 600 MPa and an electrical conductivity of at least 20% IACS is disclosed.

High strength, high conductivity electroformed copper alloys and methods of making

Provided herein are titanium alloys that can achieve a combination of high strength and high toughness or elongation, and a method to produce the alloys. By tolerating iron, oxygen, and other incidental elements and impurities, the alloys enable the use of lower quality scrap as raw materials. The alloys are castable and can form &#x3b1;-phase laths in a basketweave morphology by a commercially feasible heat treatment that does not require hot-working or rapid cooling rates. The alloys comprise, by weight, about 3.0% to about 6.0% aluminum, 0% to about 1.5% tin, about 2.0% to about 4.0% vanadium, about 0.5% to about 4.5% molybdenum, about 1.0% to about 2.5% chromium, about 0.20% to about 0.55% iron, 0% to about 0.35% oxygen, 0% to about 0.007% boron, and 0% to about 0.60% other incidental elements and impurities, the balance of weight percent comprising titanium.

The methods including applying a corrosion resistant alloy to a metal substrate to create a bimetal blank. The bimetal blank can undergo a variety of shaping and machining operations to form the net shape and internal structures of the part. Further, the part can undergo a finishing operation (e.g. polishing) to create the desired cosmetic appearance on the exterior surfaces and remove any surface imperfections resulting from the shaping and machining operations.

Methods of manufacturing corrosion resistant bimetal parts and bimetal parts formed therefrom

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Los Gatos, CA, United States of America

James A Wright