Patent classifications
C22F3/00
Method for producing high-strength magnesium alloy material and magnesium alloy rod
A method for producing a high-strength magnesium alloy material includes (a) a step of preparing a magnesium alloy workpiece having a top face and a side face; and (b) a step of applying a compressive load p (MPa) from the top face side of the workpiece and performing a uniaxial forging process on the workpiece. Step (b) is performed while suppressing deformation of the workpiece widening outward and under conditions including (i) p>f (where f is the compressive breaking stress (MPa) of the workpiece); (ii) a plastic deformation rate is less than or equal to 10%, and (iii) a strain rate is less than or equal to 0.1/sec.
Method for producing high-strength magnesium alloy material and magnesium alloy rod
A method for producing a high-strength magnesium alloy material includes (a) a step of preparing a magnesium alloy workpiece having a top face and a side face; and (b) a step of applying a compressive load p (MPa) from the top face side of the workpiece and performing a uniaxial forging process on the workpiece. Step (b) is performed while suppressing deformation of the workpiece widening outward and under conditions including (i) p>f (where f is the compressive breaking stress (MPa) of the workpiece); (ii) a plastic deformation rate is less than or equal to 10%, and (iii) a strain rate is less than or equal to 0.1/sec.
Article comprising a metal substrate and a channel in the metal substrate and method for producing same
An article having a metal substrate and a channel in the metal substrate which is partly or completely open to the surface, wherein the cross section of the channel has a local width maximum (5) between the channel base (7) and the contact plane (1), measured parallel to the contact plane and at right angles to the longitudinal channel axis in the section perpendicular to the surface. (FIG. 1a).
Article comprising a metal substrate and a channel in the metal substrate and method for producing same
An article having a metal substrate and a channel in the metal substrate which is partly or completely open to the surface, wherein the cross section of the channel has a local width maximum (5) between the channel base (7) and the contact plane (1), measured parallel to the contact plane and at right angles to the longitudinal channel axis in the section perpendicular to the surface. (FIG. 1a).
SURFACE TREATING COMPONENT WITH VIBRATION ASSISTED ROLLING TOOL
A method of operation is provided during which a tool is arranged with a surface of a component. The tool includes a roller contacting the surface. A rolling operation is performed on the surface using the roller. A vibration operation is performed on the surface through the roller concurrently with the performing of the rolling operation.
Robot machining system and control method for ultrasonic surface rolling process of aircraft engine blade
The application relates to a robot machining system and control method for ultrasonic surface rolling process of an aircraft engine blade. The robot machining system includes: a robot, to which an ultrasonic surface rolling process device is fixed, the robot drives the ultrasonic surface rolling process device to move; a base provided with a spindle turntable and a three-dimensional mobile lifting device, the spindle turntable being provided with a rotatable blade clamp, and a flexible follow-up support head being fixed to the three-dimensional mobile lifting device; and a control system, which is in electrical connection or communication connection with the robot, the spindle turntable and the three-dimensional mobile lifting device, respectively. According to the application, the robot assists in clamping ultrasonic rolling device and cooperates with the three-dimensional mobile lifting device and the flexible follow-up support head, such that the accurate ultrasonic surface rolling process of blade is realized.
Robot machining system and control method for ultrasonic surface rolling process of aircraft engine blade
The application relates to a robot machining system and control method for ultrasonic surface rolling process of an aircraft engine blade. The robot machining system includes: a robot, to which an ultrasonic surface rolling process device is fixed, the robot drives the ultrasonic surface rolling process device to move; a base provided with a spindle turntable and a three-dimensional mobile lifting device, the spindle turntable being provided with a rotatable blade clamp, and a flexible follow-up support head being fixed to the three-dimensional mobile lifting device; and a control system, which is in electrical connection or communication connection with the robot, the spindle turntable and the three-dimensional mobile lifting device, respectively. According to the application, the robot assists in clamping ultrasonic rolling device and cooperates with the three-dimensional mobile lifting device and the flexible follow-up support head, such that the accurate ultrasonic surface rolling process of blade is realized.
STRESS RELIEVING FOR CONTINUOUS FLOW ENGINE COMPONENTS
The present invention refers to an improved method of relieving a 3D printed continuous flow engine of stress. Furthermore, the present invention refers to a 3D printed continuous flow engine component relieved from stress by such method. Furthermore, the present invention refers to a computer program product causing a computing entity to execute such method. Furthermore, the present invention refers to a powder removal device to be utilized in such method.
MANUFACTURING METHOD FOR AN ALUMINUM ALLOY MEMBER, AND SHOT PEENING APPARATUS
A manufacturing method for an aluminum alloy member includes preparing an aluminum alloy member composed of an aluminum alloy, and performing shot peening on the aluminum alloy member in a range in which a speed of the shot when contacting the aluminum alloy member is from 1 m/s to 7 m/s to impart residual stress to the aluminum alloy member.
MANUFACTURING METHOD FOR AN ALUMINUM ALLOY MEMBER, AND SHOT PEENING APPARATUS
A manufacturing method for an aluminum alloy member includes preparing an aluminum alloy member composed of an aluminum alloy, and performing shot peening on the aluminum alloy member in a range in which a speed of the shot when contacting the aluminum alloy member is from 1 m/s to 7 m/s to impart residual stress to the aluminum alloy member.