| Class / Patent application number | Description | Number of patent applications / Date published |
|---|
| 416192000 | Having radial flange | 8 |
| 20090297350 | HOOP SNAP SPACER - A mount interface between two rotating gas turbine engine components includes a rigid ring to provide radial deflection restraint. In one example, the rigid ring is comprised of a metal matrix composite material. | 12-03-2009 |
| 20130251531 | ROTARY MACHINE - Provided is a rotary machine including: a shaft that rotates; a disc that has a substantially cylindrical hub fitted into the shaft and is provided so as to widen outward in a radial direction from a front end to a rear end of the hub; and an impeller having a plurality of blades provided on a surface of the disc. The hub has a tight fit section having an internal radius that is smaller than a radius of the shaft, and a loose fit section having an internal radius that is greater than the internal radius of the tight fit section. The loose fit section is provided on the front end side of the hub with respect to the tight fit section. | 09-26-2013 |
| 20140105747 | CENTRIFUGAL PUMP IMPELLERS - A centrifugal pump impeller includes front and back shrouds and a plurality of pumping vanes therebetween, each pumping vane having a leading edge in the region of an impeller inlet and a trailing edge, the front shroud has an arcuate inner face in the region of the impeller inlet, the arcuate inner face having a radius of curvature (R | 04-17-2014 |
| 20140127022 | FAN BLADE STRUCTURE - A fan blade structure includes a hub, an annular partition surrounding the hub, a first blade group and a second blade group. The hub has a top surface and a flank connected to the top surface. The first blade group, disposed on one side of the annular partition, includes two blade arrays having multiple first and second blades respectively. The clearance between the two adjacent first blades is less than that between the two adjacent second blades. The second blade group, disposed on another side of the annular partition, includes another two blade arrays having a plurality of third and fourth blades respectively. The clearance between the two adjacent third blades is less than that between the two fourth blades adjacent to each other. | 05-08-2014 |
| 20140127023 | CENTRIFUGAL COMPRESSOR IMPELLER - An impeller of a centrifugal compressor, the impeller including a web and blades secured to the web on a front face of the web. A point of intersection between a trailing edge and a blade root is at least one half-thickness of the web further forward than the blade root at an intermediate diameter of the impeller, and a point of intersection between the trailing edge and the blade tip is also further forward than the blade tip at an intermediate diameter of the impeller. | 05-08-2014 |
| 20140363298 | DIFFUSER-TYPE ENDPLATE PROPELLER - A diffuser-type endplate propeller for driving a hull is provided. The diffuser-type endplate propeller includes a propeller hub and a plurality of blades. The propeller hub is connected to a transmission shaft of the hull. Each of blades respectively has a blade-body and an endplate connected to each other, wherein each of the blade-bodies is connected to the propeller hub and extends outward from the propeller hub to the corresponding endplate, each the endplate bends from the corresponding blade-body to extend towards a stern of the hull, each of the endplates has a leading edge and a trailing edge, each the leading edge keeps a first distance from an axis of the propeller hub, each the trailing edge keeps a second distance from the axis of the propeller hub, and the first distance is less than the second distance. | 12-11-2014 |
| 20150354396 | MOULD FOR AN ABRADABLE TRACK BENEATH THE INNER SHROUD OF AN AXIAL-FLOW TURBOMACHINE COMPRESSOR - The invention relates to a mould for injecting a layer of abradable material, such as silicone, inside an inner shroud of an axial-flow turbomachine. The mould comprises a circular wall or tubular wall extending axially and two annular walls extending radially outwardly from the axial ends of the axial wall. Each radial wall of the mould comprises an annular hook in contact with the outer surface of the shroud so as to hold the mould against the shroud. The injection pressure presses the hooks against the shroud, providing a seal. The walls form an annular moulding cavity inside the inner shroud in combination with the inner shroud. The invention also relates to a method for moulding an abradable layer inside the shroud with the aid of the mould. The latter is deformed by spreading apart the hooks so as to fit over the shroud. | 12-10-2015 |
| 20160102681 | FAN ASSEMBLY FOR VEHICLES - A fan assembly includes a shroud having a through opening, around which the shroud defines an air conveying ring, a motor-fan assembly which includes an axial fan rotatable with respect to the support about an axis of rotation, and a noise-reducing annular structure, having a plurality of projections which are arranged in succession in a circumferential direction and extend radially towards the axis of rotation of the fan, each projection having a face which is directed towards the axis of rotation and is substantially parallel thereto, and a plurality of portions radially recessed towards the air conveying ring. | 04-14-2016 |
