A laser processing machine for carrying out hole-forming on a plate-shaped workpiece is provided. A first program storage that stores a plurality of hole-forming programs and a second program storage that stores a plurality of cutout piece drop programs are also provided. A program selector that selects, from the second program storage, a cutout piece drop program associated with a hole-forming program selected from the first program storage to form the hole on the workpiece. A working head controller that controls a laser processing head according to the hole-forming program and the cutout piece drop program that are selected is also provided. A motion path of the processing head after forming the hole on the workpiece and a jetting condition of assist gas to an inside of the outline from the processing head on the motion path are programed in each of the plurality of cutout piece drop programs.

A process is provided for forming a plurality of apertures in a fiber-reinforced composite object using a laser. The apertures include at least a first aperture and a second aperture. During the process, a scanner head of the laser is operated from a location to selectively scan a laser beam over the object to form a first portion of the first aperture and to form a first portion of the second aperture. The scanner head is also operated from the location to selectively scan the laser beam over the object to form a second portion of the first aperture and to form a second portion of the second aperture.

A process is provided for forming a plurality of apertures in a fiber-reinforced composite object using a laser. The apertures include at least a first aperture and a second aperture. During the process, a scanner head of the laser is operated from a location to selectively scan a laser beam over the object to form a first portion of the first aperture and to form a first portion of the second aperture. The scanner head is also operated from the location to selectively scan the laser beam over the object to form a second portion of the first aperture and to form a second portion of the second aperture.

A laser machining device includes a laser generating component, a light moving component, a gas source and a laser machining scrap removal device. The laser generating component generates a laser beam passing through an optical channel. The light moving component is positioned along a path of the laser beam to make the laser beam move along an annular machining path. The laser machining scrap removal device utilizes an internal flow path of the nozzle to increase the speed of the ejected airflow and reduce the pressure of a suction area. The gas source provides an airflow and is located on the laser machining scrap removal device in communication with the internal flow path of the nozzle. The laser machining scrap removal device induces suction on the laser processed area to assist in laser cutting/drilling processes by removing large areas of scrap, thereby improving the production speed and hole quality.

A laser machining device includes a laser generating component, a light moving component, a gas source and a laser machining scrap removal device. The laser generating component generates a laser beam passing through an optical channel. The light moving component is positioned along a path of the laser beam to make the laser beam move along an annular machining path. The laser machining scrap removal device utilizes an internal flow path of the nozzle to increase the speed of the ejected airflow and reduce the pressure of a suction area. The gas source provides an airflow and is located on the laser machining scrap removal device in communication with the internal flow path of the nozzle. The laser machining scrap removal device induces suction on the laser processed area to assist in laser cutting/drilling processes by removing large areas of scrap, thereby improving the production speed and hole quality.

An arrangement for a turbomachine is provided. The arrangement includes a vane for directing a hot gas during the operation of the turbomachine, a stator ring for securing the vane, a heat shield for protecting the stator ring from the hot gas flow wherein the heat shield is arranged in downstream direction of the hot gas flow in front of the stator ring characterized in that the heat shield comprises a plurality of channels formed therein for directing a cooling air.

An arrangement for a turbomachine is provided. The arrangement includes a vane for directing a hot gas during the operation of the turbomachine, a stator ring for securing the vane, a heat shield for protecting the stator ring from the hot gas flow wherein the heat shield is arranged in downstream direction of the hot gas flow in front of the stator ring characterized in that the heat shield comprises a plurality of channels formed therein for directing a cooling air.

A method for making shaped cooling holes in a substrate by pulsing and stopping a laser while moving the laser or substrate. The method produces shaped cooling holes with a bore angled relative to an exit surface of the combustor liner. One end of the bore is an inlet formed in an inlet surface of the combustor liner. The other end of the bore is an outlet formed in the exit surface of the combustor liner. The outlet has a shaped portion that expands in only one dimension.

A method for making shaped cooling holes in a substrate by pulsing and stopping a laser while moving the laser or substrate. The method produces shaped cooling holes with a bore angled relative to an exit surface of the combustor liner. One end of the bore is an inlet formed in an inlet surface of the combustor liner. The other end of the bore is an outlet formed in the exit surface of the combustor liner. The outlet has a shaped portion that expands in only one dimension.

The invention relates to a drilling device comprising a light source configured to provide a light beam and a diffractive beam propagation device having a substantially planar surface, wherein the light source is configured such that the light beam is incident on the planar surface of the diffractive beam propagation device, and wherein the diffractive beam propagation device is configured to propagate the light beam as one or more propagated beams such that the one or more propagated beams, at least when being integrated over time, surround an area with a substantially circular shape. A use of the drilling device for drilling a hole in a work piece and a method suitable for drilling a hole in a work piece are also provided.