Systems and methods of laser ablating a component to form a cavity are provided. In one aspect, a laser system laser ablates a component to remove a slice of material therefrom so that at least a portion of a section of the cavity is formed. With the slice of material removed, the laser system laser ablates the component along an outline of the section to remove excess sidewall material therefrom to form one or more sidewalls of the section. This removes tapering of the sidewalls. This process can be iterated to form the depth of the cavity. The laser system then laser ablates the component to remove excess end wall material therefrom to form an end wall of the cavity to a predetermined depth.

Systems and methods for coating surgical needles are provided.

A method for producing a diffusion cooling hole extending between a wall having a first wall surface and a second wall surface includes forming a cooling hole inlet at the first wall surface, forming a cooling hole outlet at the second wall surface, forming a metering section downstream from the inlet and forming a multi-lobed diffusing section between the metering section and the outlet. The inlet, outlet, metering section and multi-lobed diffusing section are formed by laser drilling, particle beam machining, fluid jet guided laser machining, mechanical machining, masking and combinations thereof.

A processing device for film cooling holes on blade of aviation engine includes a working box. A workpiece clamping mechanism is arranged in the working box for holding the workpiece. A cover body having an internal space communicated with an internal space of the working box is connected to an upper part of the working box. A laser processing mechanism is connected to a top end of the cover body and can produce laser rays to carry out laser processing on the workpiece. The cover body is connected to a liquid supply mechanism and an acid gas filtration mechanism. The liquid supply mechanism can spray an acidic solution to the workpiece in the working box, and the working box can collect the acidic solution. The acid gas filtration mechanism can filter acid steam produced during processing. A working method of the processing device is also provided.

A computer-implemented method for optimizing control of a process includes a computer receiving a process definition and a collection of elements to be arranged in a way that optimizes the utility of the process; initializing the process using a collection of discrete elements (stops, events, work orders, tasks, locations, etc.), and producing a solution for the collection by inserting the elements into the solution using the Minimum Insertion Heuristic; modifying the order of the elements to be inserted and continuing the process to produce solutions with better scores; and continuing to produce solutions based on improving the order of insertion until the process is determined to be sufficiently optimized.

A method of forming a passage in a turbine component includes: using an additive manufacturing process to form a first support structure on a first surface of the turbine component; forming a second support structure on a second surface of the turbine component, the second support structure being spaced apart from the first support structure; and forming a passage in the turbine component between the first and second support structures.

Provided is a laser processing method for drilling a hole in a glass substrate with using a carbon dioxide laser, including the steps of: irradiating the laser onto a drilling position on the glass substrate from a side of the glass substrate on which a protective sheet is adhered so as to form a blind hole; removing the protective sheet from the glass substrate and performing an annealing treatment; and performing a wet-etching process on a side of the glass substrate not irradiated with the laser so as to convert the blind hole into a through hole.

Disclosed is a device for protecting the back wall of a fuel injector nozzle during drilling of nozzle holes.

A method for producing a cavity in a blade platform of a blade, in particular of a turbine blade, as part of a blade-platform cooling system, wherein the method has the steps of: producing a first bore from a first platform lateral face in the direction of an opposite second platform lateral face, with a first opening in the first platform lateral face being created, and expanding the first bore in a fan-like manner by an electrical discharge machining method, in particular using a wire- or bar-form electrode, such that the first opening, created in the first step, of the first bore represents the starting point of the fan-like expansion. A blade is produced in particular with such a method.

Systems and methods for coating surgical needles are provided.