CA2771922C - Turbomachine - Google Patents

Turbomachine Download PDF

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Publication number
CA2771922C
CA2771922C CA2771922A CA2771922A CA2771922C CA 2771922 C CA2771922 C CA 2771922C CA 2771922 A CA2771922 A CA 2771922A CA 2771922 A CA2771922 A CA 2771922A CA 2771922 C CA2771922 C CA 2771922C
Authority
CA
Canada
Prior art keywords
shaft
impeller wheel
impeller
bearing
wheel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CA2771922A
Other languages
French (fr)
Other versions
CA2771922A1 (en
Inventor
Frank Wiebe
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Atlas Copco Energas GmbH
Original Assignee
Atlas Copco Energas GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Atlas Copco Energas GmbH filed Critical Atlas Copco Energas GmbH
Publication of CA2771922A1 publication Critical patent/CA2771922A1/en
Application granted granted Critical
Publication of CA2771922C publication Critical patent/CA2771922C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10Adaptations for driving, or combinations with, electric generators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/06Arrangements of bearings; Lubricating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/40Application in turbochargers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/70Application in combination with
    • F05D2220/76Application in combination with an electrical generator
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/50Bearings
    • F05D2240/51Magnetic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/50Bearings
    • F05D2240/52Axial thrust bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/50Bearings
    • F05D2240/54Radial bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position
    • F05D2260/34Balancing of radial or axial forces on regenerative rotors

Abstract

A turbomachine has a shaft extending along and rotatable about an axis and having an outer surface, a first impeller wheel permanently mounted on the shaft and having a respective back face, a second impeller wheel detachably mounted on the shaft axially offset from the first impeller wheel and having a respective back faces axially confront the back face of the first impeller wheel, and respective first and second axial bearings each having a respective rotor bearing half fixed to the respective impeller wheel and a respective nonrotatable stator bearing half axially juxtaposed with the respective rotor bearing half. The rotor shaft is of increasingly smaller cross-sectional size from the first wheel to the second wheel.

Description

TURBOMACHINE
SPECIFICATION
FIELD OF THE INVENTION
The present invention relates to a turbomachine. More particularly this invention concerns a turbomachine two axially spaced but jointly rotatable impeller wheels.
BACKGROUND OF THE INVENTION
A turbomachine is known having at least one first and one second impeller wheel whose back faces confront each other, a rotor shaft carrying both of the radial impeller wheels, and a bearing system. Adjacent each of the radial-blade impeller wheels is an axial bearing with one respective rotor bearing half and one respective stator bearing half. The rotor bearing halves are each formed on the back face of the respective radial impeller wheel.
In practice, to contain the axial thrust of a rotor of a turbomachine using a magnetic bearing system, axial bearing surfaces are customarily used that are either formed directly on the shaft, or fixed by an additional axial bearing washer to the shaft. Correspondingly, turbomachines having an axial magnetically mounted rotor shaft are known in which the magnetic bearing halves for axial bearing are on an axial bearing washer, or on opposed shaft shoulders shrunk onto the rotor shaft.
EP 2 017 435 A2 describes a design having the features cited above for a turbomachine having as short a rotor as possible, and a rotor mass that is as small as possible. Because the rotor bearing halves are formed on the back faces of the radial impeller wheels, the space taken up by the axial bearing can be reduced significantly, the axial bearing halves being integrated into a housing wall and also integrated into the rear side of the radial impeller wheels, which must also be present independent of the bearing. The number of separate components is thereby reduced. The design known from EP 2 017 435 A2 is substantially symmetrical starting at an electric machine located centrally of the rotor between the two radial impeller wheels.
Starting at the electric machine, sequentially in both directions, a radial magnetic bearing, a safety bearing, an opening through the assigned stator bearing half having an interior shaft gasket and finally at the end of the rotor shaft, the corresponding impeller wheel is mounted overhung. Starting at the electric machine, the diameter of the rotor shaft decreases in both directions successively, according to the cited components that are provided along the rotor shaft. During assembly, first the rotor shaft must be inserted through with the electric machine into the housing, the further components and finally the two impeller wheels are then installed on the two shaft ends. To make subsequent maintenance possible, the
- 2 -turbomachine must be accessible on both sides, and both axial impeller wheels must be made removable as well.
OBJECTS OF THE INVENTION
It is therefore an object of the present invention to provide an improved turbomachine.
Another object is the provision of such an improved turbomachine that overcomes the above-given disadvantages, in particular that is simple to assemble and disassemble as well as to maintain.
SUMMARY OF THE INVENTION
A turbomachine has according to the invention a shaft extending along and rotatable relative to a support about an axis and having an outer surface. A first impeller wheel permanently mounted on the shaft has a respective back face. The outer surface of the shaft is formed with steps of increasingly small diameter away from the first wheel. A second impeller wheel detachably mounted on a respective one of the steps of the shaft axially offset from the first impeller wheel has a respective back face axially confronting the back face of the first impeller wheel. Respective first and second axial magnetic bearings each have a respective annular rotor bearing half fixed to the respective impeller wheel and a respective one-piece nonrotatable
- 3 -annular stator bearing half axially juxtaposed with the respective rotor bearing half, axially spacedly traversed by the shaft, and carried on the support. A radial bearing mounted on the rotor shaft between the axial bearings has an inner rotor ring carried on a respective one of the steps and an outer stator ring carried on the support.
In accordance with one embodiment of the present invention there is provided a turbomachine comprising a support; a shaft extending along and rotatable relative to the support about an axis and having an outer surface; a first impeller wheel produced as a separate part and shrunk, welded or pressed onto the shaft to be permanently mounted on the shaft and having a respective back face, the outer surface of the shaft being formed with steps of increasingly small diameter away from the first wheel; a second impeller wheel detachably mounted on a respective one of the steps of the shaft axially offset from the first impeller wheel and having a respective back face axially confronting the back face of the first impeller wheel;
respective first and second axial magnetic bearings each having a respective annular rotor bearing half fixed to the respective impeller wheel and a respective one-piece nonrotatable annular stator bearing half axially juxtaposed with the respective rotor bearing half, axially spacedly traversed by the shaft, and carried on the support, said stator bearing halves each having a one-piece support having an axial through hole through which the shaft passes; a radial bearing mounted on the shaft between the axial bearings and having an inner rotor ring carried on a respective one of the steps and an outer stator ring carried on the support.
The first impeller wheel is fixedly mounted together
- 4-with further machine components in a main housing. The shaft extends out the main housing and the second impeller wheel is mounted outside the main housing. An electric machine is provided between the first and second impeller wheels.
According to one embodiment of the invention, an asymmetric design is provided, and the first impeller wheel is mounted fixedly and nonremovably on the rotor shaft. Thus according to the invention the first radial impeller wheel cannot be separated from the rotor shaft, or can be separated from the rotor shaft only upon the exertion of a very large force or by taking special steps. Thus, it is possible, for example, to shrink the first axial impeller wheel onto the rotor shaft, to weld it or to press it onto the rotor shaft. Then, during assembly, starting with the first radial impeller wheel that is connected nonremovably, the further components, i.e. at least the stator bearing halves and finally the second radial impeller wheel are installed sequentially. According to the invention the individual steps of the shaft outer surface have outer diameters adapted to the inner diameters of the respective components to be mounted thereon. The individual components can easily be pushed up to the section at which they are to be mounted. As a result of the removable design of the second radial impeller wheel - depending on the design - disassembly or at least maintenance of the described components is possible. In particular, the components of the - 4a-axial bearings are accessible starting from the second radial impeller wheel.
Because the stator bearing halves are pushed onto the rotor shaft from one end during assembly, separation into two half shells or segments is not required, as a result of which stability and impermeability are improved and production expense is also reduced.
To form an axial bearing, in particular an actively controllable axial bearing, magnetic windings of one of the halves of each bearing generate a magnetic field affecting the other bearing half, preferably controllable as needed. For practical reasons it is advantageous when the magnetic windings are in the fixed stator bearing halves.
To form a magnetic axial bearing, the rotor bearing halves must consist of a suitable material that magnetically interacts with the coils, or be covered with permanent magnets.
Often, the material used for impeller wheels is not suited for forming rotor bearing halves of a magnetic bearing. In such a case, at least one of the radial impeller wheels can be formed by an impeller wheel body that includes a blade system and a disk consisting of a different material, e.g. an aluminum alloy, fastened at the rear side of the impeller wheel body, the disk forming the rotor bearing half of the corresponding axial bearing. Such a disk or such a ring with a central opening for the rotor shaft can, for example, be welded onto the impeller wheel body. To make precise welding possible, in particular, a
- 5 -connection by friction welding can be provided. Alternatively, it is also possible to provide a suitable material, for example, permanent magnets or a magnetizable material in the form of segments on the rear side of the radial impeller wheels, in particular to insert them into corresponding recesses.
The assembly and the optionally provided disassembly from one end permits, within the scope of the invention, that the first radial impeller wheel with further machine components is also mounted fixedly in a main housing. Advantageously, it is then provided that the rotor shaft extends out of the main housing, as a result of which the second radial impeller wheel is correspondingly located outside the main housing.
The turbomachine having at least two radial impeller wheels whose back faces confront each other (back-to-back arrangement), can serve as a compressor, expander or compander.
While with a compressor having two compressor impeller wheels a drive, in particular by an electric machine, is to be provided, in the case of an expander having two impeller wheels, the energy that is being released can be recovered and used by an electric machine in the form of a generator. In the case of a compander having a compressor impeller wheel and an expander impeller wheel, an electric machine is only optionally provided, and it can be operated as a generator or as a motor depending on application.
According to a preferred design of the invention, the two radial impeller wheels are mounted overhung at respective
- 6 -ends of the rotor shaft. But in principle, it is also conceivable that on at least one of the two radial impeller wheels, the rotor shaft extends beyond this radial impeller wheel, and still at least one further device can be mounted on the rotor shaft, for example, a further radial impeller wheel.
BRIEF DESCRIPTION OF THE DRAWING
The above and other objects, features, and advantages will become more readily apparent from the following description, reference being made to the accompanying drawing in which:
FIG. 1 shows components of a turbomachine according to the invention; and FIG. 2 shows the system according to FIG. 1 attached to a main housing.
DETAILED DESCRIPTION
As seen in FIG. 1 a turbomachine according to the invention has a first impeller wheel 1 and a second impeller wheel 2 with respective back faces 3a and 3b turned axially relative to an axis A toward each other in a so-called back-to-back arrangement. The two wheels 1 and 2 are carried by and rotationally fixed to a common axially centered rotor shaft 4 mounted on a bearing system that in turn is carried on a fixed
- 7 -support constituted by a machine housing.
The bearing system includes respective axial bearings 5a and 5b each having a rotor bearing half 6a or 6b and a stator bearing half 7a or 7b. The rotor bearing halves 6a and 6b are formed on back faces 3a and 3b of the respective assigned radial impeller wheels 1 and 2. The stator halves 7a and 7b are carried on the fixed support.
According to the invention, the first radial impeller wheel 1 is permanently mounted on to the rotor shaft 4, for example by shrinking on, while the second radial impeller wheel 2 can be detached from the shaft 4. Thus, during assembly, the two stator bearing halves 7a and 7b and then the second radial impeller wheel 2 can be pushed in sequence onto the rotor shaft 4 to which the wheel 1 has already been fixed. To_make_this possible, the rotor shaft 4 decreases in cross-sectional size or diameter from the first radial impeller wheel 1 toward the second impeller wheel 2. Disassembly of the rotor system is also possible in reverse order.
FIG. 1 further shows that the stator bearing halves 7a and 7b each have a respective one-piece support 8 having an axially centered and throughgoing hole for the rotor shaft 4 and an electromagnetic winding 9 set in a groove formed in the respective support 8. In contrast, the rotor halves 6a and 6b on the back faces 3a and 3b of the radial impeller wheels 1 and 2 consist of a material that interacts magnetically with the
- 8 -magnetic windings 9. Thus the rotor bearing halves 6a and 6b are for example fitted with permanent magnets, magnetizable material or a material in which an opposing field is induced.
The specific embodiment according to FIG. 1 shows by way of example a design in which the first radial impeller wheel 1 is comprised of a body 10 formed with axially and radially extending blades and a flat disk 11 of a different material integrally fixed to the rear side of the body 10. The disk 11 forms the rotor bearing half 6a of the corresponding axial bearing 5a and is of a material selected for its magnetic properties. The rotor half 6a of the annular disk 11 with an axially centered and throughgoing through hole can, for example, be permanently connected to the blade body 10 by friction welding.
FIG. 1 further .shows that the_axially_oppositelv effective bearings 5a and 5b flank a radial bearing 12 mounted on the rotor shaft 4 and formed as a magnetic bearing with an inner rotor ring 13 carried on the shaft 4 and an outer stator ring 14 carried on the fixed support- While the stator ring 14 has magnetic windings 18, the rotor ring 13 consists of a material with suitable magnetic properties to form a radial magnetic bearing together with the magnetic windings 18 of the stator ring 14.
It can be seen that during assembly, first one stator bearing half 7a1 then the radial bearing 12, then the other stator bearing half 7b, and finally the second radial impeller
- 9 -wheel 2 with the corresponding rotor bearing half 6b mounted on its back face 3b, are installed, one after the other. To facilitate assembly, the diameter of the rotor shaft 4 decreases in steps each intended to carry a respective one of the described components.
Within the scope of the design according to the invention, the described configuration is not only to be assembled successively, but can also in reverse sequence be at least partially disassembled, so that subsequent maintenance or the exchange of individual components is still possible.
For example, the first impeller wheel 1 can be fixed with other machine components in a main housing 15, with the rotor shaft 4 extending out of the main housing 15 and the second radial impeller wheel 2 mounted outside the main housing 15. A
corresponding design is shown in FIG. 2. The advantage results_ that during assembly, maintenance, and disassembly of the bearing system, the main housing 15 can remain closed, while only an additional housing 16 that covers the bearing system must be removed.
In principle, the turbomachine can also have an electric machine that is provided together with the radial bearing 12 between the radial impeller wheels 1 and 2. This machine can be a motor, a generator, or a motor/generator.
Furthermore, the radial impeller wheels 1 and 2 can also be mounted overhung, that is each at a respective end of the rotor shaft 4. But the invention is not limited to this type of
- 10 -design. In principle, it is also possible that the rotor shaft 4 extends beyond at least one of the two radial impeller wheels 1 and 2, for instance into the housing 15.
- 11 -

Claims (3)

The embodiments of the present invention for which an exclusive property or privilege is claimed are defined as follows:
1. A turbomachine comprising:
a support;
a shaft extending along and rotatable relative to the support about an axis and having an outer surface;
a first impeller wheel produced as a separate part and shrunk, welded or pressed onto the shaft to be permanently mounted on the shaft and having a respective back face, the outer surface of the shaft being formed with steps of increasingly small diameter away from the first wheel;
a second impeller wheel detachably mounted on a respective one of the steps of the shaft axially offset from the first impeller wheel and having a respective back face axially confronting the back face of the first impeller wheel;
respective first and second axial magnetic bearings each having a respective annular rotor bearing half fixed to the respective impeller wheel and a respective one-piece nonrotatable annular stator bearing half axially juxtaposed with the respective rotor bearing half, axially spacedly traversed by the shaft, and carried on the support, said stator bearing halves each having a one-piece support having an axial through hole through which the shaft passes;
a radial bearing mounted on the shaft between the axial bearings and having an inner rotor ring carried on a respective one of the steps and an outer stator ring carried on the support;

wherein the first impeller wheel is fixedly mounted together with further machine components in a main housing, the shaft extending out the main housing, the second impeller wheel being mounted outside the main housing; and wherein an electric machine is provided between the first and second impeller wheels.
2. The turbomachine defined in claim 1, wherein at least one of the impeller wheels is formed by an impeller wheel body including a blade system and a disk of a different material mounted on the rear side of the impeller wheel body, the disk forming the rotor bearing half of the respective axial bearing.
3. The turbomachine defined in claim 1, wherein both impeller wheels are mounted overhung at respective ends of the shaft.
CA2771922A 2011-03-24 2012-03-20 Turbomachine Expired - Fee Related CA2771922C (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102011001530A DE102011001530A1 (en) 2011-03-24 2011-03-24 turbomachinery
DE102011001530.2 2011-03-24

Publications (2)

Publication Number Publication Date
CA2771922A1 CA2771922A1 (en) 2012-09-24
CA2771922C true CA2771922C (en) 2015-07-07

Family

ID=45421987

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2771922A Expired - Fee Related CA2771922C (en) 2011-03-24 2012-03-20 Turbomachine

Country Status (9)

Country Link
US (1) US20120243986A1 (en)
EP (1) EP2503104B1 (en)
JP (1) JP2012202406A (en)
CN (1) CN102691534B (en)
BR (1) BR102012006452A2 (en)
CA (1) CA2771922C (en)
DE (1) DE102011001530A1 (en)
IN (1) IN2012DE00522A (en)
RU (1) RU2498079C1 (en)

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Also Published As

Publication number Publication date
EP2503104A3 (en) 2016-01-27
BR102012006452A2 (en) 2014-04-22
CN102691534B (en) 2016-01-20
EP2503104B1 (en) 2018-02-28
CA2771922A1 (en) 2012-09-24
DE102011001530A1 (en) 2012-09-27
RU2012111266A (en) 2013-09-27
US20120243986A1 (en) 2012-09-27
IN2012DE00522A (en) 2015-06-05
RU2498079C1 (en) 2013-11-10
CN102691534A (en) 2012-09-26
EP2503104A2 (en) 2012-09-26
JP2012202406A (en) 2012-10-22

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