# US 10,309,300 B2 · Electric rotor fit onto a turbomachine shaft

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- Number: US 10,309,300 B2
- Document ID: US10309300B2
- Status: Granted
- Kind: B2
- Application number: 14/767,848
- Filed: 2014-02-20
- Published: 2016-01-07
- Granted: 2019-06-04
- Earliest claimed: 2013-02-22
- Assignees: BorgWarner Inc.
- Applicants: BorgWarner Inc.
- Inventors: Tyler Garrard; Will Robert Nielsen Hippen; Christopher Meszaros
- Web page: https://patentgrep.com/patent/US10309300B2

## CPC

- F02B 39/10: electric
- F01D 5/02: Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28})
- F01D 15/10: Adaptations for driving, or combinations with, electric generators
- F01D 25/16: Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se F16C)
- F01D 25/166: {Sliding contact bearing (gas bearings F01D25/22)}
- F01D 25/24: Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045})
- F02B 33/34: with rotary pumps (with cell-type pressure exchangers or the like F02B33/42)
- F02B 37/04: Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
- F02B 39/00: Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F05D 2220/40: in turbochargers
- F05D 2230/233: Electron beam welding
- F05D 2230/234: Laser welding
- F05D 2230/235: TIG or MIG welding
- F05D 2230/239: Inertia or friction welding
- F05D 2230/60: Assembly methods
- F05D 2240/24: for turbines
- Y02T 10/12: Improving ICE efficiencies
- F02B: INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL (gas-turbine plants F02C; hot-gas or combustion-product positive-displacement engine plants F02G)
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION

## Abstract

By relieving the shaft of an electronically-controlled turbocharger (ECT) in a central region of where a rotor of an electric machine couples with the shaft eases assembly of the electric machine onto the shaft. On either side of the relieved section, the fit between the shaft and the rotor may be a slip fit or an interference fit. Alternatively, the rotor is relieved in a central section. In some embodiments, the shaft is welded to the rotor. In yet other embodiments, the outside of the shaft and the inside of the rotor are threaded with a nut or a pin to secure the shaft to the rotor or the rotor itself has threads to engage with threads on the shaft. Such arrangements ease assembly and allow adjustment of dynamic characteristics of the rotor system.

## Claims

### Claim 1

An electronically-controlled turbomachine, comprising:
a shaft having a turbine wheel coupled to a first end of the shaft;
a turbine housing section disposed over the turbine wheel;
a compressor wheel secured to a second end of the shaft;
a compressor housing section disposed over the compressor wheel; and
an electric machine disposed on the shaft and located between the turbine and the compressor housing sections, wherein: the electric machine comprises a rotor and a stator; the rotor is fixed onto a portion of the shaft; the portion of the shaft has first, second, and third axial sections; an inside diameter of the rotor is greater than a diameter of the second axial section; and the second axial section is located between the first and third axial sections;
wherein the shaft has a stop section that is located between the third axial section and the turbine wheel; the stop section of the shaft has a greater diameter than the third axial section; and the stop section locates the rotor onto the shaft in an axial direction;
and wherein the shaft has a threaded section between the rotor and the compressor section, the turbomachine further comprising: a nut engaged with the threads on the shaft to cause the rotor to abut against the stop.

### Claim 2 (depends on 1)

The turbomachine of claim 1 wherein the inside diameter of the rotor is equal to an outside diameter of the shaft along the first and third axial sections.

### Claim 3 (depends on 1)

The turbo machine of claim 1 wherein the shaft and rotor are welded by one of ultrasonic welding and friction welding by rotating the shaft relative to the rotor.

### Claim 4 (depends on 3)

The turbomachine of claim 3 wherein a weld is located along an interface between the shaft and the rotor in at least one of the first and third axial sections.

### Claim 5 (depends on 3)

The turbomachine of claim 3 wherein the stop section includes a surface that extends outwardly in a radial direction that mates with a surface of the rotor that extends in a radial direction; and the mating surfaces are friction welded.

### Claim 6 (depends on 1)

The turbo machine of claim 1 wherein the inside diameter of the rotor is smaller than an outside diameter of the shaft along the third axial section so that an interference fit is formed along the third axial section and the third axial section is located closer to the turbine wheel than the first and second sections.

### Claim 7 (depends on 1)

The turbo machine of claim 1 wherein the inside diameter of the rotor is equal to the outside diameter of the shaft along the first axial section and the inside diameter of the rotor is less than the outside diameter of the shaft along the third axial section to thereby form an interference fit.

### Claim 8 (depends on 1)

The turbomachine of claim 1, further comprising:
a motor housing disposed over the electric machine; and
first and second bearings disposed on the shaft wherein the first bearing is located between the compressor section and the rotor; and the second bearing is located between the turbine section and the rotor.

### Claim 9

An electronically-controlled turbomachine, comprising:
a rotor; and
a shaft having a wheel coupled to a first end of the shaft, the shaft having an axial portion that mates with the rotor, the axial portion having:
a first axial section having a first diameter;
a second axial section having a second diameter; and
a third axial section having a third diameter wherein
the second axial section is located between the first and third axial sections; the second diameter is smaller than the first and third diameters; and the wheel is one of a turbine wheel and a compressor wheel,
and wherein an inside diameter of the rotor is uniform along at least a majority of the length of the rotor, one of a slip fit and an interference fit exists between the rotor and the shaft along the first axial section and one of a slip fit and an interference fit exists between the rotor and the shaft along the third axial section,
and wherein the shaft has a stop that is located between the third axial section and the wheel; the stop has a greater diameter than the third axial section; and the stop locates the rotor onto the shaft in an axial direction.

### Claim 10 (depends on 9)

The turbomachine of claim 9 wherein the first axial section is farther from the wheel than the third axial section and the third diameter is equal to the first diameter.

### Claim 11 (depends on 9)

The turbomachine of claim 9 wherein the rotor is affixed to the shaft by one of: electron beam welding, laser welding, tungsten inert gas welding, ultrasonic welding, and friction welding by rotating the shaft relative to the rotor.

### Claim 12 (depends on 9)

The turbo machine of claim 9 wherein the wheel coupled to the first end of the shaft is a turbine wheel, the turbomachine further comprising:
a compressor wheel coupled to a second end of the shaft with the rotor located between the turbine wheel and the compressor wheel.

### Claim 13 (depends on 9)

The turbo machine of claim 9 wherein the shaft has a threaded section proximate the first axial section, the turbomachine further comprising: a nut engaged with the threads on the shaft to cause the rotor to abut against the stop.

### Claim 14 (depends on 9)

The turbomachine of claim 9 wherein:
the shaft has a threaded section proximate the first axial section;
an inside surface of the rotor has a threaded section engaged with the threaded section associated with the shaft; and
the rotor abuts the stop.

### Claim 15

A turbomachine, comprising:
a shaft of the turbomachine having a turbine wheel coupled to a first end of the shaft;
a turbine housing section disposed over the turbine wheel;
a compressor section disposed on a second end of the shaft;
a compressor wheel disposed within the compressor section, the compressor wheel being secured to the second end of the shaft;
a rotor fit over a portion of the shaft, the rotor being located between the turbine and compressor wheels wherein: the portion of the shaft over which the rotor is fit has first, second, and third axial sections having first, second, and third diameters, respectively; an inside diameter of the rotor is greater than the second diameter with a gap defined therebetween; and the second axial section is located between the first and third axial sections,
wherein the shaft is threaded along at least a fraction of the first axial section portion and an inside surface of the rotor is threaded along a portion that engages with the threads on the shaft, and
wherein the first diameter is equal to the inside diameter of the rotor and the third diameter is greater than the inside diameter of the rotor.

### Claim 16 (depends on 15)

The turbocharger of claim 15 wherein the length of the first, second, and third axial sections are selected to minimize vibrational characteristics within the speed range of the turbocharger.

### Claim 17 (depends on 15)

The turbomachine of claim 15 wherein:
the third axial section is located between a fourth axial section and the second axial section;
the fourth axial section has a fourth diameter that is greater than the third diameter; and
an interface between the third and fourth axial sections forms a stop that prevents the rotor from being slid onto the fourth axial section.

### Claim 18

An electronically-controlled turbomachine, comprising:
a rotor having a bore, the bore having a first axial rotor section, a second axial rotor section and a third axial rotor section; and
a shaft having a wheel coupled to a first end of the shaft, the shaft having an axial portion adapted to engage with the rotor, the axial portion having: a first axial shaft section engaged with the first axial rotor section, a second axial shaft section within the second axial rotor section, and a third axial shaft section engaged with the third axial rotor section wherein:
the second axial shaft section is located between the first and third axial shaft sections; and
a difference between an inner diameter of the second axial rotor section and an outer diameter of the second axial shaft section is greater than a difference between an inner diameter of the third axial rotor section and an outer diameter of the third axial shaft section,
wherein a part of the first axial shaft section is threaded,
and wherein a part of the first axial rotor section is threaded and engaged with the threads on the first axial shaft section or the turbomachine further comprises a nut engaged with the threads on the first axial shaft section.

### Claim 19 (depends on 18)

The turbomachine of claim 18 wherein:
an outer diameter of the first axial shaft section equals the outer diameters of the second and third axial shaft sections; and
the inner diameter of the first axial rotor section is equal to the outer diameter of the first axial shaft section.

### Claim 20 (depends on 18)

The turbomachine of claim 18 wherein:
the outer diameter of the second axial shaft section is less than the outer diameter of the first axial shaft section.

### Claim 21 (depends on 18)

The turbomachine of claim 18 wherein the first axial shaft section is farther from the wheel than the third axial shaft section and an outer diameter of the third axial shaft section is equal to an outer diameter of the third axial shaft section such that the third axial shaft section and the third axial rotor section form one of a slip fit and an interference fit.

### Claim 22 (depends on 18)

The turbomachine of claim 18 wherein the wheel is a turbine wheel, the turbomachine further comprising:
a compressor wheel coupled to a second end of the shaft with the rotor located between the turbine wheel and the compressor wheel.

### Claim 23 (depends on 18)

The turbomachine of claim 18 wherein the first axial shaft section is farther from the wheel than the third axial shaft section; the shaft has a stop that is located between the third axial shaft section and the wheel; the stop has a greater diameter than an outer diameter of the third axial shaft section; and the stop locates the rotor onto the shaft in an axial direction.

### Claim 24 (depends on 18)

The turbomachine of claim 18 wherein:
the first axial shaft section is farther from the wheel than the third axial shaft section;
a gap exists between the second axial shaft section and the second axial rotor section;
the third axial shaft section engages with the third axial rotor section with an interference fit; and
the wheel is a turbine wheel, the turbomachine further comprising:
a compressor wheel coupled to a second end of the shaft.

### Claim 25 (depends on 18)

The turbomachine of claim 18 wherein the rotor is affixed to the shaft by one of:
electron beam welding, laser welding, tungsten inert gas welding, ultrasonic welding, and
friction welding by rotating the shaft relative to the rotor.