Flow rotor, in particular turbine wheel

Patent metadata

Field	Value
Publication number	US-10113428-B2
Application number	US-201214355309-A
Country	US
Kind code	B2
Filing date	Nov 9, 2012
Priority date	Nov 15, 2011
Publication date	Oct 30, 2018
Grant date	Oct 30, 2018

Abstract

A flow rotor (1), in particular a turbine wheel, having a wheel core (2) and an outer part (3) which surrounds the wheel core (2) and is connected thereto. The wheel core (2) and the outer part (3) are constructed from different materials.

First claim

The invention claimed is:

1. A radial flow exhaust gas turbocharger turbine wheel ( 1 ) having a turbine wheel hub ( 2 , 3 ) and turbine wheel blades ( 7 ), the turbine wheel hub ( 2 , 3 ) having a wheel hub axis,
wherein said turbine wheel is adapted for receiving a radially directed flow of exhaust gas and converting exhaust energy into rotational energy for driving a compressor wheel,
wherein the turbine wheel hub includes a turbine wheel hub core ( 2 ) and a turbine wheel hub outer part ( 3 ) which radially surrounds the turbine wheel hub core ( 2 )
the turbine wheel hub core ( 2 ) being coaxial with said wheel hub axis, having a bell-shaped cross-section having a base and a peak,
and
the turbine wheel outer part ( 3 ) shaped for redirecting radially directed inflow to axial outflow the turbine wheel blades ( 7 ) extending outward from the hub outer part ( 3 ) and axially located between said base and said peak,

wherein the turbine wheel hub core ( 2 ) is made of a nickel-based alloy and the turbine wheel hub outer part ( 3 ) and turbine blades ( 7 ) are made of titanium aluminide or ceramic.

2. The turbine wheel as claimed in claim 1 , wherein the turbine wheel core ( 2 ) is provided with a coating applied to the outer face ( 8 ) thereof.

3. The turbine wheel as claimed in claim 1 , wherein the turbine wheel core ( 2 ) is connected to the outer part ( 3 ) via a form-fitting connection device ( 4 ).

4. The turbine wheel as claimed in claim 1 , wherein the turbine wheel core ( 2 ) is provided with a continuous longitudinal center recess ( 5 ).

5. The turbine wheel as claimed in claim 1 , wherein the material of the outer part ( 3 ) is titanium aluminide.

6. The turbine wheel as claimed in claim 1 , wherein the material of the outer part ( 3 ) is ceramic.

7. The turbine wheel as claimed in claim 1 , wherein the turbine wheel is a boreless turbine wheel.

8. An exhaust gas turbocharger turbine wheel ( 1 ) having a turbine wheel hub ( 2 , 3 ) and turbine wheel blades ( 7 ),
wherein said turbine wheel is adapted for receiving a radially directed flow of exhaust gas and converting exhaust energy into rotational energy for driving a compressor wheel,
wherein the turbine wheel hub includes a turbine wheel hub core ( 2 ) and a turbine wheel hub outer part ( 3 ) which surrounds the turbine wheel hub core ( 2 ) and is connected thereto and is shaped for redirecting radially directed inflow to axial outflow,
wherein the turbine wheel hub core ( 2 ) is made of a first material and the turbine wheel hub outer part ( 3 ) and turbine blades ( 7 ) are made of a second material having a lower density than the first material,
wherein the turbine wheel core ( 2 ) is provided with a continuous longitudinal center recess ( 5 ), and
wherein the turbine wheel core ( 2 ) and the outer part ( 3 ) are connected by means of a weld pin ( 6 ), which extends through the longitudinal center recess ( 5 ) and is formed from the same material as the outer part ( 3 ).

9. An exhaust gas turbocharger including
a compressor wheel in a compressor housing,
a turbine wheel ( 1 ) in a turbine housing, connected via a shaft to the compressor wheel, the shaft having a shaft axis (L),
the turbine wheel having a turbine wheel hub ( 2 , 3 ) including
a turbine wheel hub core ( 2 ) and a turbine wheel hub outer part ( 3 ) the hub outer part provided radially surrounding the turbine wheel hub core ( 2 ) the turbine wheel hub core ( 2 ) having a bell-shaped cross-section and extending axially between a base and a peak,
wherein turbine wheel blades ( 7 ) extend radially outward from the hub outer part ( 3 ) and are axially located between said hub core ( 2 ) base and peak, and
wherein the turbine wheel hub core ( 2 ) is made of a nickel-based alloy and the turbine wheel hub outer part ( 3 ) and turbine blades ( 7 ) are made of titanium aluminide or ceramic.

10. The turbocharger as claimed in claim 9 , wherein the turbine wheel is a boreless turbine wheel.

Assignees

• Borgwarner Inc

Inventors

• Koenig Igor
• Loewenberg Michael

Classifications

• B23P15/006

  turbine wheels · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F05D2300/17

  Alloys · CPC title

• F05D2300/522

  Density · CPC title

• F01D5/02 Primary

  Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title