Abstract: A method and apparatus for building a fuselage assembly for an aircraft. A number of fixtures may be drive across a floor to an assembly area to form an assembly fixture. The fuselage assembly may be built on the assembly fixture.

Abstract: A tooling assembly for installation relative to a first and second turbomachine component is provided. The tooling assembly includes an axial mounting portion removably couplable to the first turbomachine component. The axial mounting portion includes a first plate, a second plate spaced apart from the first plate, and at least one turnbuckle assembly that extends between, and is coupled to, the first plate and the second plate. At least one of the first plate and the second plate include a radial compression portion. The radial compression portion includes a compression bar radially movable relative to the axial mounting portion and configured to contact the second turbomachine component.

Abstract: The present disclosure relates to tools and methods for handling a tower section of a wind turbine tower. A tool comprises a first wheeled platform, a second wheeled platform, and a frame. The frame comprises a first side portion, and a second side portion. The first side portion is attached to the first wheeled platform and is configured to support a first end portion of a sling. The second side portion is attached to the second wheeled platform and is configured to support a second end portion of the sling. The first and second wheeled platforms are separated along a horizontal direction.

Abstract: A repair system for repairing a surface of a workpiece includes a first tool configured to rotate in a first direction. The first tool contacts the surface of the workpiece during the rotation of the first tool in order to repair the surface of the workpiece. The repair system further includes a second tool configured to rotate in a second direction opposite to the first direction. The second tool contacts the surface of the workpiece during the rotation of the second tool in order to repair the surface of the workpiece. The repair system further includes a drive mechanism coupled to each of the first tool and the second tool.

Abstract: Provided is an arrangement for transporting a wind turbine component, the arrangement including: a first portion adapted to be placed on a loading area, in particular of a trailer; a second portion, in particular component adapter portion, adapted to support the component; the first portion and the second portion each having a respective connection interface via which the first portion and the second portion are reversibly couplable to each other.

Abstract: A catheter including a tubular catheter body defining a distal portion, a distal end and a lumen that extends to the distal end, a radiopaque marker carried within the lumen, and a non-metal tip that is bonded to distal end of the catheter body.

Abstract: Methods for repairing electric machines, such as wind generators, and stators implemented thereof. One method includes replacing a first stator core with a second stator core, wherein the second stator core has fewer stator slots than the first stator core, and wherein the stator slots are configured to receive coil windings. The method includes increasing a number of coil turns forming each coil winding from a first value to a second value, wherein the first value is associated with the first stator core and the second value is associated with the second stator core. The electric machine with the second stator core has rated power output at least as high as the electric machine with the first stator core.

Abstract: A snake-arm robot and a servicing device are mechanically coupled. The mechanical coupling is accomplished by a longitudinal insertion of the snake-arm robot into the servicing device or the servicing device into the snake-arm robot. An actuator moves the snake-arm robot through a passage within an engine until the snake-arm robot reaches a desired location. The movement of the snake-arm robot concurrently moves the servicing device through the passage. Subsequently, the snake-arm robot is de-coupled from the servicing device and the snake-arm robot is removed from the engine while leaving the servicing device in place within the engine.

Abstract: An application position of a processing force directed radially outward is continuously changed in the circumferential direction of a cylindrical portion (25) while applying the processing force to a part of the cylindrical portion (25) of a hub main body (21) in the circumferential direction. An application position of a processing force directed radially inward is continuously changed in the circumferential direction of a staking portion intermediary body (41) while applying the processing force to a part of the staking portion intermediary body (41) in the circumferential direction.

Abstract: The tooling system can have an extension unit having a pushing member and a pulling member extending along a length, the pushing member and the pulling member in sliding engagement and displaceable relative to one another, the extension unit having an internal passage configured for receiving a portion of the shaft via the first end; a pushing adapter engageable with and disengageable from the pushing member at the first end, and further engageable with and disengageable from one of the shaft and the component; and a pulling adapter engageable with and disengageable from the pulling member at the first end, and further engageable with and disengageable from an other one of the shaft and the component.

Abstract: A system and a method of forming a wear surface of a wheel of a rail vehicle include depositing one or more alloy powders onto a main body of the wheel, and plasma transfer arc welding the one or more powders to form one or more alloy layers secured to the main body.

Abstract: A vehicle body assembly system each forming a pre-buck section and a main-buck section set along a transport path of the floor assembly according to an exemplary embodiment of the present disclosure includes a pre-buck unit configured in the pre-buck section to regulate the seal side and the front and rear sides of side assemblies that are different for each vehicle type, and to assemble the side assembly and the floor assembly, and a main-buck unit configured in the main-buck section to regulates the roof portion and the quarter portion of the side assembly assembled to the floor assembly in the pre-buck section, assemble the roof portion, cowl, roof rail and package tray and assemble the quarter portion and the floor assembly.

Abstract: A duct comprising: an inlet; an outlet; a shell having a tubular form extending between the inlet and the outlet; a main flow path (H) within the shell for conveying a main flow between the inlet and the outlet; and a heat exchange structure, wherein the heat exchange structure comprises: an intake port provided in the shell; an output port provided in the shell; and a secondary flow path (C) within the shell for conveying a secondary flow between the intake port and the output port, wherein the secondary flow path is spirally intertwined with the main flow path for a section of the duct to provide a heat exchanger within the duct.

Abstract: A method for manufacturing an evaporator for ice-making includes: a preparation step for preparing a plate member, a finger member, and a capillary tube, the plate member being provided with a through hole and formed as a developed view of a tube; an insertion step for inserting the finger member into the through hole so that the finger member at least partially passes through the through hole; a connection step for fixedly connecting the finger member to the plate member; an insert placement step for placing at least a part of the capillary tube on the plate member; and an evaporation tube formation step for forming an evaporation tube, which is provided with a refrigerant flow path through which a refrigerant flows, by bending the plate member into a tube shape and connecting end portions.

Abstract: A wafer manufacturing method includes: a crack layer forming step of applying a laser beam of such a wavelength as to be transmitted through an ingot to the ingot, with a focal point of the laser beam positioned in a region spaced from an end face of the ingot by a distance corresponding to the thickness of the wafer to be manufactured, to form a crack layer, a cut groove forming step of positioning a cutting blade on an extension line of the crack layer and forming a cut groove continuous with the crack layer in a periphery of the ingot; and a peeling step of applying an ultrasonic wave to the end face of the ingot to peel off the wafer to be manufactured, along the crack layer.

Abstract: An accessory includes a body that has a first hole surrounded by a first inner surface, and a component that has a first hole surrounded by a first inner surface to be engaged with the first inner surface. A method of manufacturing the component includes: a piercing step of forming, by blanking, the second hole through a sheet-like member of which the component is formed; a first reshaping step of swelling the second inner surface into the second hole by compressing a rim portion surrounding the second hole; a shearing step of cutting the component out of the sheet-like member; and a second reshaping step of rounding a tip portion of the second inner surface having swelled by the first reshaping. The second reshaping step includes barreling the component cut out by the shearing.

Abstract: A bearing component composed of a chromium-molybdenum-vanadium alloyed tool steel is produced by a process that includes: (i) performing a first preheating within a temperature range of 600-650° C., (ii) performing a second preheating within a temperature range of 850-900° C., (iii) austenitizing in vacuum at 1000-1180° C. for 20-40 min, (iv) gas quenching at a minimum of 4-5 bar overpressure, and (v) tempering by performing either a double temper at 520-560° C. for 1.5-2.5 hours in each temper, or a triple temper at 520-560° C. for 0.5-1.5 hours in each temper. The steel alloy may be composed (in mass percent) of 1.32-1.45 C, 0.32-0.50 Si, 0.26-0.48 Mn, 4.0-4.85 Cr, 3.35-3.55 Mo, 3.55-3.85 V, 0-0.13 W, 0-0.20 Ni, 0-0.15 Cu, 0-0.8 Co, 0-0.03 P, and 0-0.03 S, the balance being iron and unavoidable impurities. Mo may be replaced with W or vice versa in a replacement ratio Mo:W of 1:2.

Abstract: A method for setting a blind fastener comprising the steps of: providing a workpiece with a through hole; providing the fastener; providing a setting tool comprising: a tool housing; a screw tool with a male thread movable within the housing along and around a tool axis between a retracted and an extended positions; a first electric motor with a first drive shaft axially fixed to the tool housing, the first drive shaft defining a first axis radially spaced from the tool axis; a second electric motor with a second drive shaft axially fixed to the tool housing, the second drive shaft defining a second axis radially spaced from the tool axis and from the first axis; and a solid roller screw arranged for rotation and axial movement in the tool housing, and axially concentric with and in driving connection to the screw tool; supplying the fastener in front of the screw tool when the screw tool is in the retracted position; engaging the screw tool with the fastener; and setting the fastener to the workpiece.

Abstract: A protection and loading device for an interventional valve system is provided. The interventional valve system includes a valve and a delivery system. The valve is fixed on a distal rod body of the delivery system. The protection and loading device includes: a first protector, a second protector, and a third protector. The first protector is located at a front end of the distal rod body and encompasses a half of the valve. The third protector is configured to fix and sleeve on the distal rod body. In a protection state, the first protector cooperates with the third protector at the first position. In a state of valve loading the first protector cooperates with the third protector at the second position.

Abstract: A method of manufacturing a hub unit bearing (1) includes the step of applying an axial load to a shaft end of a hub body (21) so that a staking portion (26) for inner races (22a, 22b) is formed in the hub body (21). The load is adjusted based on at least one of first information acquired before applying the load and second information acquired while applying the load.