摘要:
A turbocharger assembly (200) includes a compressor wheel (240) with a base surface (244), a nose surface (242), a z-plane disposed between the base surface and the nose surface and a bore (245) extending from the base surface to the nose surface and a shaftt (220) hat includes a first pilot surface (PA) disposed in the bore of the compressor wheel at a position between the z-plane and the nose surface, a second pilot surface (PB) disposed in the bore of the compressor wheel at a position between the z-plane and the base surface, and a recessed surface (225) disposed between the first pilot surface and the second pilot surface. Such an assembly can include a nut (270) adjustably disposed on the shaft adjacent to the nose surface of the compressor wheel where adjustment of the nut tensions the shaft to apply a compressive load between the base surface and the nose surface of the compressor wheel.
摘要:
This impeller (24) is provided with: an impeller body (31) formed in a disk-like shape and having a boss hole section (31a) formed therein, the boss hole section (31a) allowing a rotating shaft to be fitted therein; and compressor blades (25) provided on the front surface side of the impeller body (31) so as to protrude from the hub surface (31b) of the impeller body (31). The impeller (24) consists either of a first resin member (41) and a second resin member (45), which are engaged with each other and which consist of a resin, or of a resin member (64, 74) and a metallic member (67, 77), which are engaged with each other.
摘要:
An object is to provide a centrifugal compressor in which an axial force applied from a shrink-fit impeller to a sleeve section is ensured even if the sleeve section is separated from a clamp surface in an axial direction of an attachment hole, as well as a turbocharger provided with the centrifugal compressor and a method of producing the centrifugal compressor. An inner peripheral surface of an attachment hole formed on a hub includes a clamp surface and a diameter-widening surface, and an outer peripheral surface of a sleeve section includes a diameter-reducing surface. The diameter-widening surface and the diameter-reducing surface respectively include an impeller-side contacting portion and a sleeve-side contacting portion which contact each other, and a relationship represented by an expression θs
摘要:
The invention relates to a rotor (1), in particular gas turbine rotor, having a plurality of rotor discs (3), which each have an axial through-opening (2), which rotor discs are axially stayed by means of at least one tie rod (5), which extends through the through-openings (2), and which rotor discs are assembled to form at least one rotor disc unit (7, 8), at least one support ring (11) bearing against the outer diameter of the tie rod (5), which support ring is engaged with one of the rotor discs (3) and via which the tie rod (5) is supported on the rotor disc (3), and at least one securing element (14) being provided for axially securing the at least one support ring (11), characterised in that the securing element (14) has an annular design and is fastened to the rotor disc (3) to which the support ring (11) is connected and is formed such that the securing element fits around an end face (15) of the support ring (11) that faces away from the rotor disc (3).
摘要:
A compressor 10 has an axial portion 24 and a centrifugal portion 26. A disk structure 74 is provided to support the centrifugal portion and is connected to the centrifugal portion with a rabbet joint 83.
摘要:
A connection arrangement comprising a shaft having an axial through hole, a tie rod located inside the axial through hole, an impeller comprising a solid hub, a plurality of blades, and an integral stub protruding axially from the solid hub; at an end of the tie rod there is an integral body having a shape radially protruding from the tie rod; the stub has a cavity for receiving the body and an axial hole for inserting the body into the cavity; the stub axial hole has a shape corresponding to the shape of the body; the cavity is so sized and shaped as to allow rotation of the body inside the cavity and trapping of the body in the cavity once rotated; the shaft and the impeller are coupled together by a coupling.
摘要:
A method for assembling a compressor comprises: a bundle arrangement step in which a bundle is arranged behind the opening of a casing in the insertion direction; a first insertion step in which the front end of the bundle is inserted into the casing by moving the bundle by means of both an outside traveling device and an intermediate traveling device; and a second insertion step in which the intermediate traveling device is removed from the bundle and the bundle is inserted further inward into the casing by moving the bundle by means of both an inside traveling device and the outside traveling device.
摘要:
An impeller is equipped with: a disk part (30), having a cylindrical part (32) into which a rotary shaft (5) that rotates around an axis line (O) is inserted, with a portion of the cylindrical part in the axis line (O) direction of the rotary shaft (5) being fixed to the rotary shaft (35) as a grip part (33), and a disk main body part (35) extending from the cylindrical part (32) outward in the radial direction of the rotary shaft (5); a blade part (40) protruding from the disk main body part (35) toward a side in a first direction in the axis line (O) direction; a reinforcing member attachment part (50) formed on the cylindrical part (32) closer to a side in a second direction in the axis line (O) direction than the disk main body part (35); and a reinforcing member (53) formed of material having a higher specific strength than the disk part (30), and attached so as to cover the reinforcing member attachment part (50) from the outside.