Abstract: A flat cushioning air bag for cargo container with a plurality of inner partitioned air chambers, comprises: inner films, stuck together to form a main air chamber by hot sealing; a valve device, coupled to the main air chamber, allowing air to be filled into the main air chamber; connecting films, positioned between the outer films; connecting lines, coupling the outer films to the connecting films, and connecting films being adapted to partition the main air chamber; and inner partitioned air chambers, formed among the outer films and connecting films. A curved portion is formed on each outer film between each two adjacent connecting lines when the inner partitioned air chambers are filled with air and expanded, and the curved portions are tangent to the same plane, allowing each outer film to be in multi-point contact with an object surface to provide the object with cushioning protection.

Abstract: Disclosed is an anchor bolt including a metal wedge having a surface with a plurality of anti-galling protrusions and a metal sleeve in operable communication with the surface. The sleeve is expandably receptive to the surface. The plurality of anti-galling protrusions is configured and disposed to produce a substantially smooth loading curve for the anchor bolt.

Abstract: A tensioner for a strap brace comprising: a cap for receiving a fastener and a strap brace, wherein the fastener secures the strap brace to the cap; the fastener comprising first and second members with interengageable threads, wherein either can be turned to bring the strap brace under tension; and a frictioned surface to prevent rotation of the other member when one member is turned.

Abstract: A low torque nut is capable of easily generating a large axial force by a small torque to fasten and has stable anti-loosening qualities. The low torque nut includes a nut member having a screwed runner, an engagement portion, and plural screwed runners drilled from an outer periphery plane toward an inner diameter direction. The low torque nut also includes a ring-shaped saucer member rotatably mounted in a lower portion of the nut member, plural rolling elements that lie within a contact portion in an axial direction between the nut member and the saucer member, and a locking member that has an engagement groove being engaged with a spline groove and an inserting hole of a screw threadedly connecting to the screwed runner of the nut member.

Abstract: In various representative aspects, an apparatus for clamping and grounding an upper and lower solar panel mounting rail is disclosed herein. The apparatus comprises a fastener with an enlarged end, and a shank, with the enlarged end having one or more sharp protrusions that resemble teeth, and a washer with one or more sharp protrusions, and an opening. When installed, the shank is inserted through the opening of the washer, the sharp protrusions of the enlarged end penetrate either the lower or upper mounting rail and the sharp protrusions of the washer penetrate the other mounting rail while at the same time creating a grounding path through the apparatus.

Abstract: A fastening arrangement includes a threaded fastener (5) including a head (11), a shank (9) and a laterally expandable member (17). A bridging member (7) is provided on the shank of the fastener, the bridging member having an aperture through which the shank passes. The aperture has a dimension greater than the dimension of the shank (9) but less than the dimension of the head (11), and an outer dimension greater than a dimension of the laterally expandable member (17) in a first configuration but less than the dimension of the laterally expandable member in a second configuration.

Abstract: A screw comprises a head, a shank disposed at one end of the head and provided with two inclined surfaces at a distal end thereof, at a joint of the inclined surfaces is formed an inclined reaming edge, at least one thread wound around a lateral surface of the shank and a positioning tip disposed at a middle section of the reaming edge. The positioning tip of the screw is firstly abutted against an object to be locked, so as to fix the screw to the object to be locked and prevent the screw from swinging. And then, the reaming edge of the shank performs the reaming operation in the object to be locked, and finally the thread performs cutting and locking operations, which can reduce the extruded material around the locking hole and prevent the object from being ruptured or deformed.

Abstract: In an airfield with a short bi-directional runway and a long bi-directional runway intersecting with each other perpendicularly a system for storing and launching a plurality of airplanes includes a plurality of platforms, a plurality of rectangular cages and a frame. Onto each platform one airplane may be placed. Each cage has an opening into which one platform and one airplane are inserted through the opening. The frame has a plurality of slots and is disposed in ground beneath the airfield. One rectangular cage may be inserted into one of the slots. An elevator is disposed adjacent to the frame and has a bottom platform and an opening which may be aligned with the opening of one of the slots.

Abstract: A storage and discharge apparatus for particulate material includes a silo and a dispensing cone adjacent a lower end of the silo. The dispensing cone is formed in a partial conical shape and includes a fill portion oriented to face the lower end of the silo at a base end of the conical shape and a dispense portion at an apex end of the conical shape. The dispense portion includes extension sections that extend longitudinally outward from the apex end of the conical shape.

Abstract: A system and method of loading and unloading a shipping container onto and off a tilt-tray vehicle is described. The system includes a drawbar assembly adapted to be releasably attached to opposite corner connectors provided on the container. A winch is provided for applying fraction to the drawbar assembly to draw the container onto the vehicle tray and to facilitate loading of the container onto the tray. An ejector assembly is also provided to releasably engage the drawbar assembly connected to the container. When it is desired to unload the container, the ejector assembly is moved towards the rear of the tray to move the container partially off the vehicle.

Abstract: A fork lift for attachment to a truck frame of a truck, include A first mounting beam carried by the truck frame, a detachable attachment mechanism connecting the mounting beam to the truck frame, the detachable attachment mechanism extending through a truck body of the truck, a fork lift mast pivotably connected to the mounting beam, and a tilt actuator connected between the mounting beam and fork lift mast.

Abstract: A lift arm cross member may connect a tilt lever support to a pair of lift arms. The lift arm cross member may have a top plate with a generally convex outer surface as the outer surface extends from a first end edge to a second end edge, and a bottom plate having first and second end edges, a first planar portion extending from the second end edge, and a curved portion extending from the first planar portion opposite the second end edge. The first end edge of the bottom plate may be connected to an inner surface of the top plate and the second end edge of the first plate may be connected to an inner surface of the bottom plate. A buffer plate may be provided within the lift arm cross member and extend between the inner surfaces of the top and bottom plates.

Abstract: An arm of a hydraulic excavator is formed as a box-shaped structural body surrounded by left and right side plates, an upper plate joined to each of the upper end sides of each side plate, a lower plate joined to each of the lower end sides of each side plate, and a thick rear plate joined to each of the rear end sides of each side plate and the upper plate. The side plates are formed by joining a rear thick side plate and a front thin side plate. The upper plate is formed by joining two members, that is, a rear thick upper plate and a front thin upper plate, and the lower plate is formed by joining two members, that is, a rear thick lower plate and a front thin lower plate.

Abstract: Boom drive apparatus for substrate transport systems and methods are described. The boom drive apparatus is adapted to drive one or more multi-arm robots rotationally mounted to the boom to efficiently put or pick substrates. The boom drive apparatus has a boom including a hub, a web, a first pilot above the web, and a second pilot below the web, a first driving member rotationally mounted to the first pilot, a second driving member rotationally mounted to the second pilot, a first driven member rotationally mounted to the boom above the a web, a second driven member rotationally mounted to the boom below the a web, and a first and second transmission members coupling the driving members to driven members located outboard on the boom. Numerous other aspects are provided.

Abstract: A feeding device includes a housing, a first conveying mechanism mounted on the housing, and a distribution mechanism. The housing forming a receptacle space includes a top surface defining a receiving opening communicated with the receptacle space. The distribution mechanism includes a slide platform slidably mounted on the top surface, a distribution member, and elastic members. The slide platform defines an unloading opening communicated with the receiving opening and a mounting groove adjacent to the unloading opening. The distribution member is movably mounted in the mounting groove. The elastic member elastically resists the distribution member to protrude out from the unloading opening. The stacked feeding trays resist the distribution member to move away from the unloading opening. When the top feeding tray is moved above the distribution member, the distribution member retracts by an elastic force to separate the top feeding tray from the stacked feeding trays located below.

Abstract: An absorbing mechanism includes a positioning member, an absorbing member, and at least one separating member. The positioning member defines a receiving chamber, for receiving a plurality of workpieces. The attaching member is constructed for absorbing the workpieces. The at least one separating member comprises a main body and a detaching portion. The main body is mounted on the positioning member. The detaching portion protrudes from the main body toward an axis of the positioning member, and forming an inclined surface away from the main body. The inclined surface defines at least one blow hole. The inclined surface towards the receiving chamber.

Abstract: The invention relates to a device for handling objects, comprising at least one inflatable air chamber and a retaining unit for objects, which is attached to the air chamber, to a robot or manipulator, characterized by at least one device for handling objects, and to a method for handling objects using the aforementioned device, characterized by the steps of: moving the device with the side thereof comprising the retaining unit to the object to be handled in a first position; establishing an adhesive connection between the retaining unit and the object to be handled, thus retaining the object; moving the device to a desired second position, and releasing the object from the retaining unit by inflating the at least one air chamber.

Abstract: A basin which stackably interlocks with 20-inch square racks that hold dish and glassware washed in commercial dishwashers. The basin has substantially the exterior configuration of a commercial dishwasher rack and receives a plurality of dishwasher racks slacked above. The basin solid on its base and sides for prohibiting substances which drip down into it from racks stacked above from dripping onto the floor. The basin has circular indentations in the top surface or the base, trapping water and preventing it from sloshing from side to side of the basin when it is carried or moved. The basin may be loaded into a dolly used to transport commercial dishwasher racks, as the dollies typically have an open bottom. Thus, the basin can provide the water-catching function for racks loaded onto a dolly. Grooves in the basin's bottom surface permit stacking on top of a rack or other basins for storage.

Abstract: The disclosure describes a novel collection bin for a waste collection vehicle. The collection bin includes an automated cover system.

Abstract: A compressor intake mixer system for internal combustion gas engines having a compressed charge bypass system comprises a bypass charge and fuel pre-mixer connected in line with the charge bypass system to reduce pressure gradient between the high pressure bypass charge and the low pressure fuel. A single volume main mixer is connected to the compressor inlet downstream of the pre-mixer to mix the flow of premixed charge and air and provide a mixed gas to the compressor inlet. Thus a need for a separate volume for a fuel mixer and a bypass mixer is eliminated and a single volume is provided at the compressor inlet. The locational constraint of necessarily locating the volumes at the compressor inlet is also obviated by providing a pre-mixer.

Abstract: An airfoil according to an exemplary embodiment of the present disclosure can include an airfoil body having a plurality of film cooling holes that extend through an exterior surface of the airfoil body. Each of the plurality of film cooling holes break through the exterior surface at geometric coordinates in accordance with Cartesian coordinate values of X, Y and Z as set forth in Table 1. Each of the geometric coordinates is measured from a reference point on a leading edge rail of a platform of the airfoil.

Abstract: A particle deflector for a gas turbine engine deters accumulation of particles in cooling passages of nozzle vanes of the engine. The particle deflector is arranged to be disposed around a turbine housing over cooling passages that supply cooling air to nozzle vanes within the housing. The particle deflector includes circumferentially distributed mounting holes for mounting the particle deflector to the turbine housing. The particle deflector also includes circumferentially distributed spacers to space the particle deflector from the housing.

Abstract: A preswirler of a gas turbine engine includes an outer ring. The outer ring includes an outer flange with a plurality of first holes, and an outer cylindrical portion extending from the outer flange. The preswirler also includes an inner ring. The inner ring includes an inner flange spaced apart from the outer flange. The inner ring also includes an inner cylindrical portion located within the outer cylindrical portion and a back portion extending from the inner flange to the inner cylindrical portion. The inner ring further includes a plurality of second holes.

Abstract: This invention relates to a fluid supply system for a rotary machine, the system comprising: a rotor assembly comprising an array of blades arranged to be driven about a primary axis in use, the rotor assembly comprising a casing structure, wherein the casing structure is rotatable in unison with the blades about the primary axis; a directional fluid intake, said intake being rotatably mounted at an outer surface of the casing structure about a second axis which is angularly offset from the primary axis.

Abstract: A motor base includes a bottom plate and at least one vibration reduction unit. The bottom plate has opposite top and bottom surfaces. A shaft-coupling portion is arranged on the top surface. The at least one vibration reduction unit encloses the shaft-coupling portion. Each of the at least one vibration reduction unit includes at least one protrusion and at least one groove. The at least one protrusion is arranged on one of the top and bottom surfaces. The at least one groove is correspondingly arranged on the other one of the top and bottom surfaces.

Abstract: An assembly includes a torque box and a first bell crank. The torque box has a housing with an interior cavity. The first bell crank is pivotally supported from the housing and extends through the interior cavity. The first bell crank has three arms for transferring an actuating force to a plurality of variable guide vanes for positioning the guide vanes within a gas turbine engine.

Abstract: The present invention relates to a turbomachine comprising at least one bladed disk, be it mobile or static, and vortex generators (17) positioned upstream of the blading (1) of said disk, wherein the vortex generators (17) are of variable pitch.

Abstract: A gas turbine engine includes a fan case radially outwardly of a core compartment. A compressor section is located within an engine core compartment and includes a front mount flange and an aft mount flange. An oil tank is mounted to at least one of the fan case or the front and aft mount flanges. The oil tank has a cooling structure integrated into an outer surface such that the oil tank is subjected to cooling air flow from a plurality of air sources.

Abstract: A pump assembly having improved cooling for use in a selective catalytic reduction system is disclosed. The pump assembly comprises a pump housing having a body portion and a nozzle portion extending from the body portion, a jacket including a cavity for receiving the pump housing, first and second ports for cooling fluid, and a flow guide disposed between the jacket and the pump housing. The cavity includes a first compartment for cooling fluid defined in part by the flow guide and in part by the pump housing and being in fluid communication with the first port; and a second compartment for cooling fluid defined in part by the flow guide and in part by the jacket. The first compartment is in fluid communication with the second port by way of the second compartment.

Abstract: An exhaust system for use with a steam turbine is provided. An exhaust hood includes an input and an output, the input receiving fluid from the steam turbine. The exhaust hood includes a first side wall that extends between the input and the output. The first side wall includes an aperture. An ejector is coupled to the exhaust hood. The ejector includes inlets and an outlet. At least one of the inlets receives fluid from the exhaust hood via the aperture.

Abstract: A stator of an electric motor or generator comprises a core formed of ferromagnetic material having a plurality of teeth arranged circumferentially about an axis. In one aspect of the invention, at least one retaining member connects the end portions of at least two of the teeth to each other in a manner inhibiting relative movement between said tooth end portions. By inhibiting relative movement between said tooth end portions, vibration is reduced. Vibration can also be reduced by welding interior surfaces of a core to each other. Reducing the vibration reduces the noise emissions of the stator during operation.

Abstract: The invention relates to a method for manufacturing a steam turbine low-pressure or medium-pressure module deflector, said deflector comprising an internal ring and an external ring as well as vanes, said method comprising a step of welding said vanes to said rings. The main characteristic of a method according to the invention is that the welding step is preceded by a step of automatically machining the ends of each vane to create a peripheral recess around each of said ends.

Abstract: A transition duct assembly for a turbine engine includes a transition duct with an inner liner removably received therein. The duct is hollow with an inner peripheral surface and an outer peripheral surface. The duct can have an inlet end and an outlet end. The inner peripheral surface of the duct can be convergent along a majority of the length of the duct when moving from the inlet end to the outlet end thereof. The liner is hollow body with an inner peripheral surface and an outer peripheral surface. The outer peripheral surface of the liner can be correspondingly convergent to the inner peripheral surface of the duct. The inner peripheral surface of the liner can define an internal flow passage through the assembly. Such a construction permits the use of different materials for the liner and the duct and can allow the liner to be readily removed and replaced.

Abstract: A fan structure includes a cap, a fixing shaft, a bearing, an impeller and a protection lid, wherein the cap comprises a bottom portion, a body and an accommodating space. The fixing shaft is disposed within the accommodating space, a first end portion of the fixing shaft couples the bottom portion, and a second end portion of the fixing shaft protrudes to the body. The bearing couples to the fixing shaft, the second end portion of the fixing shaft protrudes to the bearing, and a hub of the impeller couples to the bearing. The second end portion of the fixing shaft protrudes to the hub. The protection lid couples to the second end portion of the fixing shaft to prevent lubricants for lubricating the bearing from splashing. The protection lid provides the impeller with protection to prevent the impeller from being compressed by external force to avoid destruction.

Abstract: According to one aspect of the invention, a turbine assembly includes a frame coupled to a ground surface, a bearing housing supporting a rotor bearing and a sleeve assembly attached to the frame and the bearing housing. The sleeve assembly includes an outer sleeve with a first flange on a first end that is positioned in an opening in the bearing housing and a second end that abuts the shim, an inner sleeve positioned within a portion of the outer sleeve and a bolt positioned within the inner sleeve and threadably coupled to the frame, wherein the bolt compressively loads the inner sleeve thereby loading a portion of the outer sleeve at the second end between the inner sleeve and the frame and wherein a first gap dimension is substantially maintained between the first flange and bearing housing as the bolt is preloaded and coupled to the frame.

Abstract: A turbocharger and a method of manufacturing a floating bush with which noise can be reduced, and the rotation speed can be increased. In a turbocharger in which a rotating shaft having a circular cross-section and connecting a turbine rotor and a compressor rotor is supported in a freely rotatable manner, at two axially separated positions via floating bushes, by an inner circumferential surface disposed so as to surround the rotating shaft in a bearing housing, an inner circumferential surface of each of the floating bushes has a non-circular shape in which the curvature of the cross-sectional shape varies in the circumferential direction.

Abstract: A support bearing arrangement comprises a gas turbine rotor shaft, a bearing stack, a bearing sleeve, and a support bearing. The bearing stack comprises a fore seal plate, and aft seal plate, and a bearing mount situated axially between the fore and aft seal plates. The bearing sleeve surrounds at least a portion of the rotor shaft, and is configured to form an insulating air gap between the rotor shaft and the bearing stack. The support bearing is mounted on the bearing mount to couple the gas turbine rotor shaft to a stationary structure, thereby centering and retaining the gas turbine rotor shaft.

Abstract: A seal support comprises a body, a seal carrier disposed circumferentially around an outer surface of the body, and a meshing ring extending axially forward of the seal carrier.

Abstract: A turbine airfoil comprises a suction sidewall, a pressure sidewall, a tip wall, and a tip leakage control channel. Each sidewall extends spanwise from an airfoil base and chordwise between a leading edge and a trailing edge. The tip wall extends chordwise from the leading edge to the trailing edge and joins respective outer spanwise ends of the suction and pressure sidewalls. The tip leakage control channel has an inlet and an outlet recessed into an outer surface of the tip wall. An inlet of the channel begins proximate a junction of the airfoil pressure sidewall and the tip wall. An outlet of the channel terminates at a recessed portion of the junction of the tip wall and the suction sidewall.

Abstract: A method of locking a rotor of a wind turbine, the method including positioning of the rotor in a locking position; applying a rotor lock; forcing the rotor to turn in a first direction; and, applying a rotor brake.

Abstract: A hybrid powertrain for an aircraft may include a drive shaft, the drive shaft, an internal combustion engine to selectably drive the drive shaft, a propeller coupled to the drive shaft and an electric motor having a stator and a rotor and operable to selectably drive the drive shaft. The drive shaft may extend through the electric motor. The rotor may be coupled to the drive shaft to rotate with the drive shaft and the rotor is a flywheel for the internal combustion engine.

Abstract: The present invention relates to a device for inserting a balancing weight into a rotor of a turbine, that includes an external component and an internal component. The internal component is connected in a helical manner to the external component. The internal component delimits a chamber which has a first and a second opening, a lower surface which is provided with a sealing joint and a cap in order to close in a tight manner the first opening of the chamber. The connection between the external component and the internal component is helical, that is to say, the result of a threading operation. Therefore, the internal component can thus move in a coaxial manner with respect to the external component.

Abstract: A turbine assembly comprises an anchor plate, at least one turbine blade mounted to the anchor plate and having an elongated blade body having a longitudinal axis parallel to an axis of rotation, and the at least one turbine blade being operable to move between a first position relative to the axis of rotation and a second position relative to the axis of rotation.

Abstract: A roller bearing that includes an outer ring, a first inner ring, and a first sealing ring that is disposed axially adjacent of the outer ring is provided. The roller bearing also includes a first retaining ring that is attached to the outer ring. The first sealing ring is fixed between the first retaining ring and a first clamping ring.

Abstract: A fixation device for fixing a shaft connecting a rotor and a generator of a wind turbine, the fixation device comprising: a rotor lock for locking the shaft providing a locking clearance; and a rotor brake for braking the shaft; wherein the rotor lock is arranged for positioning the shaft in a selectable angular position within the locking clearance of the rotor lock.

Abstract: A blower wheel for use in a blower assembly includes a hub, a concentrically arranged outer ring, an array of spaced apart blades extending between the hub and the outer ring. The hub includes an outer first surface and an inner second surface. An interface between an outer edge of a first end of each of the blades and an outer peripheral edge of the outer first surface of the hub is minimized, increasing an effective blade exit height of the blower wheel. As such, an effective open area for airflow between the blades of the blower wheel is increased over that of the prior art blower wheels. Further, a substantially planar lower face of the hub provides additional structural integrity to the hub, and thereby the blades.

Abstract: The invention involves craneless dismounting and/or mounting a vertically arranged wind turbine blade from a wind turbine generator hub mounted to a nacelle placed on a tower, said hub being arranged for having a number of blades attached. The method comprises mounting a number of bolt-like extensions in positions, where fastening bolts have been removed or could be received. These extensions are much longer than the fastening bolts, so that the blade may be handled using the extensions to a position where a lifting yoke may be attached or detached, either for lowering or lifting the blade. The method may be performed without at separate crane and is particularly useful in relation to blade maintenance, repair or replacement at remote wind turbine sites which would incur high costs for a mobile crane. Moreover, the method may be performed without having personnel going outside the hub or nacelle, but can stay at the ground and within the hub.

Abstract: Provided are a stator blade assembly advantageous for improving the evacuation performance by shortening the evacuation time, and an exhaust pump provided with such a stator blade assembly. Inner and outer stator blade bases of a plurality of stator blades are supported by frames. A projecting portion protruding from the frame supporting the inner stator blade base, or from the frame supporting the outer stator blade base, or from both of the frames is provided in a gap in the vicinity of the inner or outer stator blade base between one of the supported stator blades and the stator blade transversely adjacent thereto.

Abstract: The invention relates to an axial-radial rolling contact bearing, in particular for supporting rotor blades (2) on a wind turbine (1), comprising a first bearing ring (7) and a second bearing ring (8), which form an inner ring and an outer ring, and comprising a radial rolling contact bearing row (4) and a plurality of axial rolling contact bearing rows between the first bearing ring (7) and the second bearing ring (8). According to the invention, at least four axial rolling contact bearing rows (5a, 5b, 5c, 5d) which are arranged at a distance from each other in the axial direction (x) are provided, said radial rolling contact bearing row (4) being arranged between the second axial rolling contact bearing row (5b) and the third axial rolling contact bearing row (5c) in the axial direction (x).

Abstract: The invention relates to a wind turbine blade bearing removal apparatus and method for facilitating the change-over of the blade root bearing assembly (58) of a wind turbine blade (54). A plurality of support shoulders or yokes (60) are located on the hub (50) of the wind turbine rotor and provide attachment points for respective actuators (62). Corresponding attachment points (66) are provided in the wind turbine blade (54) via a blade support (section 64), which is constructed in the blade between the blade root bearing assembly (58) and the tip. The actuators (62) are mounted between the hub (50) and the blade root bearing assembly (58) and therefore support the blade (54) in a suspended position when the bearing is to be retained. The actuators (62) allow the blade to be easily reattached to the hub (50) when the blade root bearing replacement is completed.