C22C14/00

DUPLEX SURFACE TREATMENT FOR TITANIUM ALLOYS
20180010229 · 2018-01-11 ·

A surface treatment for a metal substrate includes a nitride layer and a diamond-like carbon coating on said nitride layer. The metal substrate can be a titanium-containing substrate. The nitride layer and diamond-like carbon coating serve to improve the tribological properties of the metal substrate.

DUPLEX SURFACE TREATMENT FOR TITANIUM ALLOYS
20180010229 · 2018-01-11 ·

A surface treatment for a metal substrate includes a nitride layer and a diamond-like carbon coating on said nitride layer. The metal substrate can be a titanium-containing substrate. The nitride layer and diamond-like carbon coating serve to improve the tribological properties of the metal substrate.

ENHANCED TEMPERATURE CAPABILITY GAMMA TITANIUM ALUMINUM ALLOYS
20180010468 · 2018-01-11 ·

An alloy composition including a γ-TiAl alloy with a sustained temperature capability of about 1500 F. An alloy composition including a γ-TiAl alloy with an oxygen level of about 100 wppm and between about 1500-3000 appm carbon. An alloy composition including a γ-TiAl alloy with an alpha stabilizer.

ENHANCED TEMPERATURE CAPABILITY GAMMA TITANIUM ALUMINUM ALLOYS
20180010468 · 2018-01-11 ·

An alloy composition including a γ-TiAl alloy with a sustained temperature capability of about 1500 F. An alloy composition including a γ-TiAl alloy with an oxygen level of about 100 wppm and between about 1500-3000 appm carbon. An alloy composition including a γ-TiAl alloy with an alpha stabilizer.

ENHANCE DUCTILITY OF GAMMA TITANIUM ALUMINUM ALLOYS BY REDUCING INTERSTITIAL CONTENTS
20180010213 · 2018-01-11 ·

A process to increase ductility includes utilizing γ-TiAl alloy as a base alloy and reducing at least one interstitial of the base alloy to create an alloy compositions with extremely low interstitials (Eli).

ENHANCE DUCTILITY OF GAMMA TITANIUM ALUMINUM ALLOYS BY REDUCING INTERSTITIAL CONTENTS
20180010213 · 2018-01-11 ·

A process to increase ductility includes utilizing γ-TiAl alloy as a base alloy and reducing at least one interstitial of the base alloy to create an alloy compositions with extremely low interstitials (Eli).

Method of manufacturing TiAl alloy impeller and TiAl alloy impeller

A method of manufacturing a TiAl alloy impeller includes a blank preparation step in which a blank of the TiAl alloy impeller is prepared, wherein the blank has a shaft portion and a plurality of blades, and a thickness of an outer edge of each of the blades of the blank is set so as to be larger than a thickness of an outer edge of a blade of the TiAl alloy impeller, and an additional work step in which an additional work is performed on each of the blades of the blank. In the additional work step, the additional work is performed on a first surface of a portion that includes at least the outer edge of each of the blades or the first surface and a second surface of the portion thereof.

MULTI-STAGE GAS ATOMIZATION PREPARATION METHOD OF TITANIUM ALLOY SPHERICAL POWDER FOR 3D PRINTING TECHNOLOGY

A multi-stage gas atomization preparation method of titanium alloy spherical powder for a 3D printing technology includes the following steps: bar preparation and machining step, multi-stage gas atomization powder preparation step through vacuum induction, and powder screening step. The collision probability of the metal droplets at the gas atomization stage is reduced by controlling the gas atomization pressure and the feeding speed of the titanium alloy electrode bar in a hierarchical manner, so that the collaborative control of the particle size and the surface quality of the titanium alloy 3D printing powder in the gas atomization preparation process is realized.

MULTI-STAGE GAS ATOMIZATION PREPARATION METHOD OF TITANIUM ALLOY SPHERICAL POWDER FOR 3D PRINTING TECHNOLOGY

A multi-stage gas atomization preparation method of titanium alloy spherical powder for a 3D printing technology includes the following steps: bar preparation and machining step, multi-stage gas atomization powder preparation step through vacuum induction, and powder screening step. The collision probability of the metal droplets at the gas atomization stage is reduced by controlling the gas atomization pressure and the feeding speed of the titanium alloy electrode bar in a hierarchical manner, so that the collaborative control of the particle size and the surface quality of the titanium alloy 3D printing powder in the gas atomization preparation process is realized.

COLLAPSING AND EXPANDING STRUCTURES WITH SHAPE MEMORY MATERIALS AT MULTIPLE TEMPERATURES
20230233834 · 2023-07-27 ·

Shape memory alloys are used in aerospace structures, orthodontics, cardiovascular prosthetic devices, sensors and controllers, and many other engineering, technology, science, and other fields. The methods are described in the case of a temporary heart assist pump to illustrate the concepts, but the method applies to many other fields. The properties of shape memory alloys are used to fold or collapse and implant in the human body a device without breaking the device as it reaches body temperature or without reaching permanent plastic deformation. The properties of nitinol are also used to describe intended explantation of the device, at body temperature, from the body without breaking it. Such planned explantation may be needed in cases where the device is designed for temporary use, such as mechanical circulatory support devices intended for temporary use and then removal of all components of the device from the body. The same method can be used for devices that have not been initially designed for removal, such as stents or valves, that must later be explanted for reasons unanticipated when they were installed. The methods ensure that the devices stay within stress-strain-temperature conditions so they remain elastic, or under the upper stress plateau, or remain plastic, but always under the breaking strain, of shape memory alloys at: room or environmental conditions; cooler than environmental conditions; and at a higher temperature, or body temperature. The methods described may also be applied to other industrial applications, where shape memory alloys may be installed and removed at different temperatures. Applications in other industries, include aerospace, civil structures, mechanical structures are contemplated.