Abstract: A blade for a gas turbine engine comprises an airfoil having a pressure side and a suction side, with a root and a tip wall. The pressure side and suction side extend beyond the tip wall to define a tip channel, defining a plurality of internal and external corners. The corners comprise fillets to define a thickness being greater than the thickness for the pressure, suction, or tip walls. A film hole can extend through the fillet, such that the length of the film hole at the fillet can be increased to define an increased length-to-diameter ratio for the film hole to improve film cooling through the film hole.

Abstract: An airfoil for a gas turbine engine includes a pressure side and a suction side, with a root and a tip wall. The pressure side and suction side extend beyond the tip wall to define a tip channel, defining a plurality of internal and external corners. A tip shelf can be defined in the pressure or suction sidewalls. A film hole can extend to the tip shelf, such that the film hole can be shaped to direct a flow of cooling fluid to the film hole to improve film cooling at the tip shelf.

Abstract: A filter system and method use a filter housing that defines an interior chamber and that includes an inlet opening extending into the interior chamber. The outer air flow housing has an outlet conduit through which a flow of air having particles is directed toward the inlet opening of the filter housing along a flow direction toward the interior chamber of the filter housing. The outer air flow housing engages the filter housing such that the filter housing is separated from the outer air flow housing along the flow direction to permit at least some of the air to pass around an exterior of the filter housing and exit the outer air flow housing while the particles in the at least some of the air pass into the interior chamber of the filter housing through the inlet opening.

Abstract: An apparatus and method of cooling a hot portion of a gas turbine engine, such as a rotor disk, by having a vane assembly with a cooling air passage and a flow control insert located within the cooling air passage defining a conduit. A turning nozzle is mounted to the vane and has a turning passage with an inlet and an outlet, the turning nozzle is fluidly coupled to the flow control insert outlet.

Abstract: A method of forming a structure in a turbine component having a seal slot, the slot including walls defining an opening therebetween, the method includes the step of using an additive manufacturing process to form a neck structure on a wall so as to reduce a size of the opening.

Abstract: A turbine engine having a bypass fluid conduit coupled to the turbine section includes at least one particle separator located within the bypass fluid conduit to separate particles from a bypass fluid stream prior to the bypass stream reaching the turbine section for cooling. A centrifugal separator for removing particles from a fluid stream includes an angular velocity increaser, a particle outlet, an angular velocity decreaser downstream of the angular velocity increaser, and a bend provided between the angular velocity increaser and the angular velocity decreaser.

Abstract: A centrifugal separator for removing particles from a fluid stream includes an angular velocity increaser configured to increase the angular velocity of a fluid stream, a flow splitter configured to split the fluid stream to form a concentrated-particle stream and a reduced-particle stream, and an exit conduit configured to receive the reduced-particle stream. An inducer assembly for a turbine engine includes an inducer with a flow passage having an inducer inlet and an inducer outlet in fluid communication with a turbine section of the engine, and a particle separator, which includes a particle concentrator that receives a compressed stream from a compressor section of the engine and a flow splitter. A turbine engine includes a cooling air flow circuit which supplies a fluid stream to a turbine section of the engine for cooling, a particle separator located within the cooling air flow circuit, and an inducer forming a portion of the cooling air flow circuit in fluid communication with the particle separator.

Abstract: A gas inlet member of a CVD reactor includes a gas inlet housing having a gas distribution volume supplied with a process gas by a feed line and a multiplicity of gas lines, each formed as a tube and engaging openings of a gas outlet plate arranged in front of an inlet housing wall, and through which the process gas enters a process chamber. A coolant chamber adjoins the gas inlet housing wall and a coolant cools the gas inlet housing wall and outlet ends of the gas lines that are in heat-conductive contact with the gas inlet housing wall. The gas outlet plate is thereby thermally decoupled from the gas inlet housing wall such that the gas outlet plate, which is acted on by radiation heat coming from the process chamber, heats up more intensely than the outlet ends which extend into the openings of the gas outlet plate.

Abstract: A gas turbine engine arcuate segment includes arcuate flange with anti-chording means extending away from annular wall. Anti-chording means may include insert in or bonded to flange and made of different alpha material than the annular wall. Anti-chording means may be heating means for heating flange. Heating means includes hot air inlet to and an outlet from a circumferentially extending heating flow passage embedded in flange and may further include a cold air inlet to heating flow passage. Heating flow passage may be a serpentine heating flow passage with an undulating heating flowpath. A turbine nozzle segment includes one or more airfoils extending radially between inner and outer arcuate band segments and forward and aft outer flanges extending radially from the outer arcuate band segment include anti-chording means. An arcuate turbine shroud segment includes forward and aft shroud rail segments with anti-chording means.

Abstract: The invention relates to a device with at least one first electrically conductive contact plate (11) and with at least one second electrically conductive contact plate (12), and with a plurality of electrically parallel-connected first heating elements (1 to 9) each with at least one resistance heating unit (1.3 to 9.3), wherein each of the heating elements (1 to 9) is connected with the first contact plate (11) by means of a first terminal contact (1.1 to 9.1), and with the second contact plate (12) by means of a second terminal contact (1.2 to 9.2), wherein the two contact plates (11, 12) lie in a shared first plane (E1), wherein the resistance heating units (1.3 to 9.3) are arranged along a spiral or circular arc line around a center of the device. In order to increase the service life of the device while reducing manufacturing costs, it is proposed that several heating units (1.3 to 9.

Abstract: An airfoil comprises at least one wall defining a leading edge, a trailing edge, a pressure side extending between the leading edge and the trailing edge, and a suction side extending between the leading edge and the trailing edge. The airfoil is curved in three dimensions and has one or more cavities defined by an interior surface of the at least one wall. A plurality of cooling film holes extending between the cavity and at least one cooling trench located on at least one of the pressure side and the suction side, spaced from the leading edge. The at least one trench has a floor spaced from an outer surface of the airfoil. The plurality of cooling film holes extend through the floor at an angle other than perpendicular.

Abstract: An apparatus and a method for a thermal treatment, in particular a coating of a substrate, includes a heating device which is regulated by a regulating device which interacts with a first temperature sensor device. In order to counteract a temperature drift of the first temperature sensor device, a second temperature sensor device is used to detect the temperature drift and recalibrate the first temperature sensor device. The second temperature sensor device is used to measure the surface temperature of a substrate. This measured value is compared with a desired value, and if the desired value deviates from the measured actual value, a correction factor is formed and is used to apply the measured value used to regulate the heating device to the first temperature sensor device in order to bring the actual temperature value measured by the second temperature sensor device closer to the associated desired temperature value.

Abstract: A turbine comprising a first turbine component being of a first material having a first coefficient of thermal expansion. A second turbine component being of a second material having a second coefficient of thermal expansion, said second turbine component adjacent said first turbine component. A space between said first and second turbine components. A seal assembly sealing said space, wherein at least a portion of said seal assembly has a coefficient of thermal expansion substantially similar to at least one of said first or second turbine components to thereby maintain a seal in said space during thermal expansion or contraction of said first and second turbine components.

Abstract: A centrifugal compressor apparatus includes: an impeller mounted for rotation about a central longitudinal axis, the impeller including an impeller disk carrying an array of impeller blades around its periphery; a diffuser disposed downstream of the impeller, configured to diffuse and turn airflow discharged from the impeller; an extraction scoop disposed in fluid communication with the impeller and with a plenum disposed adjacent the impeller, and a dirt collector disposed in fluid communication with the plenum and configured to trap dirt therein.

Abstract: An engine component for a turbine engine includes a particle collector having a substrate configured to retain at least some particles from a particle-laden stream passing through a portion of the engine. A fluid bypass around the substrate of the collector enables the particle-laden stream to bypass the substrate if the substrate is filled with particles.

Abstract: An inertial separator for removing particles from a fluid stream includes a body defining a through passage, with at least one separator inlet and at least one separator outlet, a turn provided in the body between the at least one separator inlet and the at least one separator outlet, and a flow splitter having at least one particle outlet fluidly coupled to the outside of the through passage.

Abstract: There is disclosed a method for forming a TiSiN thin film on a substrate according to ALD including a first process of preheating a substrate while supplying Ar or N2 containing inert gas to a chamber, after disposing a substrate in a chamber; a second process of forming a TiN film on the substrate by repeating at least one time a process of purging over-supplied Ti containing gas after supplying Ti containing gas and inert gas after that and a process of purging residual product after supplying N containing gas and inert gas after that; a third process of forming a SiN film by repeating at least one time a process of purging over-supplied Si containing gas after supplying Si containing gas on the TiN film and supplying inert gas after that and a process of purging residual product after supplying N containing gas and supplying inert gas after that; and a fourth process of forming a TiSiN film having a desired thickness by repeating the second and third processes at least one time, a partial pressure range of

Abstract: There is disclosed a method for forming a TiSiN thin film on a substrate according to ALD including a first process of preheating a substrate while supplying Ar or N2 containing inert gas to a chamber, after disposing a substrate in a chamber; a second process of forming a TiN film on the substrate by repeating at least one time a process of purging over-supplied Ti containing gas after supplying Ti containing gas and inert gas after that and a process of purging residual product after supplying N containing gas and inert gas after that; a third process of forming a SiN film by repeating at least one time a process of purging over-supplied Si containing gas after supplying Si containing gas on the TiN film and supplying inert gas after that and a process of purging residual product after supplying N containing gas and supplying inert gas after that; and a fourth process of forming a TiSiN film having a desired thickness by repeating the second and third processes at least one time, a partial pressure range of

Abstract: A gas inlet member of a CVD reactor includes a gas inlet housing having a gas distribution volume supplied with a process gas by a feed line and a multiplicity of gas lines, each formed as a tube and engaging openings of a gas outlet plate arranged in front of an inlet housing wall, and through which the process gas enters a process chamber. A coolant chamber adjoins the gas inlet housing wall and a coolant cools the gas inlet housing wall and outlet ends of the gas lines that are in heat-conductive contact with the gas inlet housing wall. The gas outlet plate is thereby thermally decoupled from the gas inlet housing wall such that the gas outlet plate, which is acted on by radiation heat coming from the process chamber, heats up more intensely than the outlet ends which extend into the openings of the gas outlet plate.

Abstract: The invention relates to a CVD reactor, with a process chamber (4) which is arranged therein and into which a process gas can be fed by means of a gas inlet member (2), with a substrate holder (3) which, on the upper side (3?) thereof facing the process chamber (4), has one or more pockets (5) which are designed in such a manner that one substrate (7) in each case rests only on selected, raised support regions (6), and with a heating system (9) which is arranged below the substrate holder (3) and is spaced apart from the lower side (3?) of the substrate holder (3), wherein the lower side (3?) of the substrate holder (3) is configured differently in a central region (b) with respect to the heat transmission from the heating system (9) to the substrate holder (3), which central region is located under a central zone of the pocket (5), than in a surrounding region (a) which surrounds the central region (a) and is located below a zone close to the edge of the pocket (5).