Adjustable-trim centrifugal compressor with ported shroud, and turbocharger having same

Patent metadata

Field	Value
Publication number	US-9719518-B2
Application number	US-201414537339-A
Country	US
Kind code	B2
Filing date	Nov 10, 2014
Priority date	Nov 10, 2014
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

A ported-shroud centrifugal compressor for a turbocharger includes an inlet-adjustment mechanism in an air inlet for the compressor, operable to move between an open position and a closed position in the air inlet. The inlet-adjustment mechanism includes an axially elongated ring. In the open position, the radially outer surface of the ring is spaced from a tapering inner surface of the air inlet so that air can flow in an annular passage between the tapering surface and the ring, and the ring opens the ported shroud. In the closed position, the ring abuts the tapering surface to close off the annular passage and to close off the ported shroud. Movement of the inlet-adjustment mechanism from the open position to the closed position is effective to shift the compressor's surge line to lower flow rates.

First claim

What is claimed is:

1. A turbocharger, comprising:
a turbine housing and a turbine wheel mounted in the turbine housing and connected to a rotatable shaft for rotation therewith, the turbine housing receiving exhaust gas and supplying the exhaust gas to the turbine wheel;
a centrifugal compressor assembly comprising a compressor housing and a compressor wheel mounted in the compressor housing and connected to the rotatable shaft for rotation therewith, the compressor housing defining an air inlet for leading air generally axially into the compressor wheel, the compressor housing further defining a volute for receiving compressed air discharged generally radially outwardly from the compressor wheel, the air inlet having an inner surface a portion of which forms a sliding surface that extends for an axial length along a downstream axial direction, the sliding surface being followed by a tapering surface that extends for an axial length along the downstream axial direction, the tapering surface becoming smaller in diameter in the downstream axial direction, wherein the compressor housing defines a flow recirculation system comprising a bleed port located adjacent an inducer portion of the compressor wheel for allowing air to pass therethrough, a recirculation passage connected with the bleed port and extending upstream from the bleed port, and an injection port leading from the recirculation passage into the air inlet upstream from the inducer portion, whereby air may flow through the recirculation system in either direction between the air inlet and the inducer portion; and
a compressor inlet-adjustment mechanism disposed in the air inlet of the compressor housing and movable between an open position and a closed position, the inlet-adjustment mechanism comprising an axially elongated ring comprising a tubular wall whose inner surface becomes smaller in diameter in the downstream axial direction toward the compressor wheel such that the diameter of the inner surface is smaller at a downstream end of the ring than at an upstream end of the ring, the downstream end of the ring terminating at a trailing edge, an inner diameter of the ring at the trailing edge being smaller than an inner diameter of a shroud surface of the compressor housing at the inducer portion of the compressor wheel,
the ring being arranged so that when the inlet-adjustment mechanism is in the open position the bleed port is open and the ring is spaced from the tapering surface of the air inlet such that there is an annular passage between the tapering surface and the ring for a flow of air therethrough and the ring opens the injection port to allow air flow through the recirculation system, and when the inlet-adjustment mechanism is in the closed position the bleed port remains open and the ring abuts the tapering surface to eliminate said annular passage and the ring closes the injection port and prevents air flow through the recirculation system.

2. The turbocharger of claim 1 , wherein the ring in the closed position extends in the downstream direction substantially to the inducer portion of the compressor wheel such that an effective diameter of the air inlet at the inducer portion is determined by the inner diameter of the ring at the trailing edge.

3. The turbocharger of claim 1 , wherein the inlet-adjustment mechanism further comprises a support portion that includes a plurality of circumferentially spaced struts connected to the ring, the support portion having a radially outer surface that engages the sliding surface of the air inlet and is movable along the sliding surface.

4. The turbocharger of claim 3 , wherein there are three said struts circumferentially spaced apart.

5. The turbocharger of claim 1 , the tubular wall of the ring at a trailing edge thereof defining an inside diameter d r that is between 0.45 and 0.98 times d lS , where d lS is a diameter of the inducer portion of the compressor wheel.

6. The turbocharger of claim 5 , wherein the tubular wall has an axial length L and the trailing edge of the tubular wall in the closed position is spaced an axial distance S from a leading edge of the inducer portion of the compressor wheel, and wherein L is substantially larger than S.

7. The turbocharger of claim 6 , wherein S<8.5(d lS −d r ).

Assignees

• Honeywell Int Inc

Inventors

• Mohtar Hani
• Smith William Joseph
• Pees Stephane

Classifications

• F04D29/462

  especially adapted for elastic fluid pumps · CPC title

• F04D29/4213

  suction ports · CPC title

• F04D27/0284

  Conjoint control of two or more different functions · CPC title

• F04D27/0253

  by throttling (F04D27/0246 takes precedence) · CPC title

• F04D27/0215

  Arrangements therefor, e.g. bleed or by-pass valves · CPC title