Abstract: An outer platform leading edge cooling system includes a radially outer platform having a platform leading edge; a hollow cooling channel is defined extending generally longitudinally along the platform leading edge of the radially outer platform; an inlet port located in a radially outer end region of the platform leading edge being fluidly coupled with the hollow cooling channel; and the hollow cooling channel comprising an outlet conduit extending from a cooling channel exit, the outlet conduit being connected in fluid flow communication with a trailing edge cavity.

Abstract: Dental implant, comprising an external thread arranged on an outside of the dental implant for fastening the dental implant to a jawbone. Further, the implant comprises an opening extending along a longitudinal axis of the dental implant, in which opening an internal thread for fastening a superstructure to the dental implant is arranged. Still further, the implant comprises an interface for fastening the superstructure to the dental implant, which interface is arranged at a front end of the dental implant. The interface is suitable for direct attachment of a superstructure to the dental implant without the use of an abutment.

Abstract: Dental implant, comprising an external thread arranged on an outside of the dental implant for fastening the dental implant to a jawbone. Further, the implant comprises an opening extending along a longitudinal axis of the dental implant, in which opening an internal thread for fastening a superstructure to the dental implant is arranged. Still further, the implant comprises an interface for fastening the superstructure to the dental implant, which interface is arranged at a front end of the dental implant. The interface is suitable for direct attachment of a superstructure to the dental implant without the use of an abutment.

Abstract: An ergometric treadmill for sport training comprising a screen, a control system and a system configured for collecting, processing, analyzing and visualizing the biomechanical response of a sportsperson while running on the ergometric treadmill; wherein the ergometric treadmill comprises (a) a plurality of MEMS sensors attached by means of supports to the ergometric treadmill connected to a data capture unit; and (b) a data processing unit configured to generate a plurality of parameters related to the physical exercise performed on the ergometric treadmill by a user and synthesize and show, in graphic form, the parameters generated for the user's biofeedback from the treadmill.

Abstract: A gas turbine engine component includes a substrate having first surface and a second surface disposed opposite the first surface, a plurality of holes extending through the substrate from the first surface to the second surface, the holes defined by a plurality of respective walls each extending from the first surface to the second surface, a metallic bond coat disposed on the first surface, and an aluminide coating disposed on the first surface, the second surface, and the walls. The metallic bond coat is disposed between the first surface and the aluminide coating and the walls are free of the metallic bond coat.

Abstract: A gas turbine engine component includes a substrate having first surface and a second surface disposed opposite the first surface, a plurality of holes extending through the substrate from the first surface to the second surface, the holes defined by a plurality of respective walls each extending from the first surface to the second surface, a metallic bond coat disposed on the first surface, and an aluminide coating disposed on the first surface, the second surface, and the walls. The metallic bond coat is disposed between the first surface and the aluminide coating and the walls are free of the metallic bond coat.

Abstract: The disclosed technology concerns an aircraft turbomachine part comprising a part body drilled with at least one cavity open to the outside and at least one conduit joining the cavity on the one hand and leading to the outside on the other hand. Each cavity receives a pressure sensor, and the conduit corresponds to the cavity guides the cables connected to the sensor to the outside of the part body. The part is an aircraft turbomachine vane.

Abstract: Dental implant and superstructure each with an interface that allows direct attachment of the superstructure to the dental implant without the use of an abutment. The dental implant comprises an anti-rotation element that is arranged in the opening and is configured to prevent the superstructure from rotating about a longitudinal axis relative to the dental implant. The superstructure comprises an interface corresponding to the anti-rotation element, having a recess with two mutually opposite side flanks which are at a first distance from each other in a first region and, in a second region which is at a greater distance from the longitudinal axis than the first region, are at a second distance from each other, the second distance being smaller than the first distance.

Abstract: Vane assemblies for turbine engines are described. The vane assemblies include a vane having an internal cavity and a vane platform and a vane rail defining, in part, an outer diameter supply cavity. A blade outer air seal support (BOAS support) is arranged adjacent the vane and engages with a portion of the vane, the blade outer air seal support having BOAS support rail, and a BOAS supported on the BOAS support and engaging with a portion of the vane. The BOAS support includes a first cooling flow aperture configured to enable a cooling flow to cool at least the BOAS and a second cooling flow aperture formed in the BOAS support rail. The vane rail includes a third cooling flow aperture to form a cooling flow path through the second cooling flow aperture and the third cooling flow aperture to fluidly connect to the outer diameter supply cavity.

Abstract: Superstructure and dental implant each with an interface that allows direct attachment of the superstructure to the dental implant without the use of an abutment and can be manufactured in a cost-effective manner.

Abstract: Dental implant comprising an implant body having on an outer side an external thread for fastening the dental implant to a jaw bone and having an opening extending along a longitudinal axis of the dental implant. The opening comprises an internal thread for fastening a superstructure to the dental implant. The implant body further comprises an interface for fastening the superstructure to the dental implant, which interface is arranged at a front end of the implant body. The dental implant further comprises an anti-rotation element which is configured to prevent rotation of the superstructure around the longitudinal axis relative to the dental implant, wherein the anti-rotation element is configured as a component separate from the implant body, which is attached to the implant body in an area of the interface.

Abstract: Vane assemblies for turbine engines are described. The vane assemblies include a vane having an internal cavity and a vane platform and a vane rail defining, in part, an outer diameter supply cavity. A blade outer air seal support (BOAS support) is arranged adjacent the vane and engages with a portion of the vane, the blade outer air seal support having BOAS support rail, and a BOAS supported on the BOAS support and engaging with a portion of the vane. The BOAS support includes a first cooling flow aperture configured to enable a cooling flow to cool at least the BOAS and a second cooling flow aperture formed in the BOAS support rail. The vane rail includes a third cooling flow aperture to form a cooling flow path through the second cooling flow aperture and the third cooling flow aperture to fluidly connect to the outer diameter supply cavity.

Abstract: Dental prosthesis comprising a dental implant comprising an external thread for screwing the dental implant into a jawbone and an internal thread arranged inside the dental implant. The dental prosthesis further comprises a superstructure having an internal bore and a screw for fastening the superstructure to the dental implant. The screw has a screw head with a cylindrical or conical lateral surface and a shank which adjoins a lower end of the screw head and on which an external thread is arranged. In an assembled state of the dental prosthesis, the screw is inserted through the internal bore of the superstructure into the dental implant and the external thread of the screw engages the internal thread of the dental implant. The screw head comprises a convexly rounded chin between the cylindrical or conical lateral surface and its lower end, with which chin the screw abuts the superstructure in the internal bore in the assembled state of the dental prosthesis.

Abstract: Shroud assembly of an axial turbomachine (2) having a rotor (12), such as a turbomachine compressor air-intake shroud (28). The assembly comprises an annular layer (32) of abradable material that is able to cooperate by abrasion with lips (44) of the turbomachine in order to ensure tightness, and a heating module (38) for the abradable layer (32). The module (38) comprises electrical heating resistors (42) within the abradable material in order to prevent the presence of ice on the shroud (28). The abradable material is thus used as a heating body which receives, transports and distributes the heat used for de-icing.

Abstract: Methods and devices including amorphous magnetic microwires are provided for biomedical energy transfer for diagnosis or therapy, to promote cellular growth, or to deliver pharmaceutical agents. Applications of the technology include in sensors, actuators, and therapeutic coatings, and for increasing the amount, directionality, or length of nerve growth. The technology also can be utilized for nerve regeneration, hyperthermic treatment of tumors, vascular theranostics, probing a nerve, stimulating a nerve, sensing a biological condition, catheterization, and micro-actuation.

Abstract: A turbine blade for a gas turbine engine. The turbine blade having a plurality of cooling holes defined therein, at least some of the plurality of cooling holes being located on a suction side of an airfoil of the turbine blade and in fluid communication with an internal cavity of the turbine blade; and wherein the at least some of the plurality of cooling holes are located in the airfoil according to the coordinates of Tables 1 and/or 2.

Abstract: Dental implant, comprising an external thread arranged on an outside of the dental implant for fastening the dental implant to a jawbone. Further, the implant comprises an opening extending along a longitudinal axis of the dental implant, in which opening an internal thread for fastening a superstructure to the dental implant is arranged. Still further, the implant comprises an interface for fastening the superstructure to the dental implant, which interface is arranged at a front end of the dental implant. The interface is suitable for direct attachment of a superstructure to the dental implant without the use of an abutment.

Abstract: The invention relates to a system of vanes with adjustable orientation, also called a system of variable stator vanes, for a low-pressure compressor of an axial turbine engine. The system comprises vanes, each having a vane extending radially in a flow of the turbine engine and a spindle having a cylindrical portion connected to a telescopic actuating lever. The cylindrical portion comprises radially extending slot, and the actuating lever comprises a pivot joint housed in the slot, that is configured to communicate a rotary movement to the vane about its spindle. The invention also proposes a compressor and a turbine engine.

Abstract: Systems and methods are provided for producing a continuous survey of a previously drilled portion of a wellbore. The method includes receiving a plurality of stationary survey measurements taken at a corresponding plurality of locations along the portion of the wellbore. The method further includes receiving at least one continuous survey including a plurality of continuous survey measurements taken between a pair of stationary survey measurements of the plurality of stationary survey measurements. The method further includes combining the plurality of stationary survey measurements and the plurality of continuous survey measurements to produce the continuous survey of the portion of the wellbore.

Abstract: The disclosed technology concerns an aircraft turbomachine part comprising a part body drilled with at least one cavity open to the outside and at least one conduit joining the cavity on the one hand and leading to the outside on the other hand. Each cavity receives a pressure sensor, and the conduit corresponds to the cavity guides the cables connected to the sensor to the outside of the part body. The part is an aircraft turbomachine vane.