EP0893576A3 - Connection of rotating elements - Google Patents

Connection of rotating elements Download PDF

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Publication number
EP0893576A3
EP0893576A3 EP98810441A EP98810441A EP0893576A3 EP 0893576 A3 EP0893576 A3 EP 0893576A3 EP 98810441 A EP98810441 A EP 98810441A EP 98810441 A EP98810441 A EP 98810441A EP 0893576 A3 EP0893576 A3 EP 0893576A3
Authority
EP
European Patent Office
Prior art keywords
connection
components
positive
takes place
insert ring
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.)
Granted
Application number
EP98810441A
Other languages
German (de)
French (fr)
Other versions
EP0893576A2 (en
EP0893576B1 (en
Inventor
Harry Alkelin
Mikael Fryklund
Roland Nilsson
Per Thörnblad
Hans Dr. Wettstein
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.)
General Electric Technology GmbH
Original Assignee
ABB Asea Brown Boveri Ltd
Asea Brown Boveri AB
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 ABB Asea Brown Boveri Ltd, Asea Brown Boveri AB filed Critical ABB Asea Brown Boveri Ltd
Publication of EP0893576A2 publication Critical patent/EP0893576A2/en
Publication of EP0893576A3 publication Critical patent/EP0893576A3/en
Application granted granted Critical
Publication of EP0893576B1 publication Critical patent/EP0893576B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/025Fixing blade carrying members on shafts
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/026Shaft to shaft connections
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/06Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • 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
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods
    • F05D2230/64Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/21Utilizing thermal characteristic, e.g., expansion or contraction, etc.
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/21Utilizing thermal characteristic, e.g., expansion or contraction, etc.
    • Y10T403/217Members having different coefficients of expansion
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/48Shrunk fit

Abstract

Bei einer kraft- und formschlüssige Verbindung von rotierenden Bauteilen (1,2), welche im Bereich der Verbindung während der Rotation unterschiedliches Dehnungsverhalten aufweisen, erfolgt der Formschluss über einen gestuften Zentriersitz (3). Der Kraftschluss zwischen den beiden Bauteilen erfolgt mittels axial vorgespannter Elemente. Zumindest eines der Bauteile weist einen Hohlraum (6) im Innern auf, in dem ein Einlagering (7) angeordnet ist, welcher während des Betriebes eine radiale Kaft auf den Zentriersitz (3) ausübt. Der vorgespannte Einlagering (7) liegt nur mit einem Teil seiner axialen Erstreckung an dem mit ihm zusammenwirkenden Bauteil (1) an.

Figure 00000001
In the case of a non-positive and positive connection of rotating components (1, 2) which have different expansion behavior in the area of the connection during rotation, the positive connection takes place via a stepped centering seat (3). The frictional connection between the two components takes place by means of axially prestressed elements. At least one of the components has a cavity (6) inside, in which an insert ring (7) is arranged, which exerts a radial force on the centering seat (3) during operation. The pretensioned insert ring (7) lies only with a part of its axial extent on the component (1) interacting with it.
Figure 00000001

EP98810441A 1997-07-03 1998-05-14 Connection of rotating elements Expired - Lifetime EP0893576B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19728345 1997-07-03
DE19728345A DE19728345A1 (en) 1997-07-03 1997-07-03 Non-positive and positive connection of rotating components

Publications (3)

Publication Number Publication Date
EP0893576A2 EP0893576A2 (en) 1999-01-27
EP0893576A3 true EP0893576A3 (en) 1999-12-08
EP0893576B1 EP0893576B1 (en) 2003-12-03

Family

ID=7834469

Family Applications (1)

Application Number Title Priority Date Filing Date
EP98810441A Expired - Lifetime EP0893576B1 (en) 1997-07-03 1998-05-14 Connection of rotating elements

Country Status (4)

Country Link
US (2) US6126357A (en)
EP (1) EP0893576B1 (en)
JP (1) JPH1172002A (en)
DE (2) DE19728345A1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19728345A1 (en) * 1997-07-03 1999-01-07 Asea Brown Boveri Non-positive and positive connection of rotating components
DE10134611A1 (en) * 2000-12-16 2002-06-27 Alstom Switzerland Ltd Fixing device for a blade mounting of a compressor or turbine stage of a gas turbine system comprises a blade having a counter-contour corresponding to a connecting element of a wedge element to produce a form-locking connection
GB0116479D0 (en) * 2001-07-06 2001-08-29 Rolls Royce Plc Coupling arrangement
DE10319629A1 (en) * 2003-05-02 2004-11-18 Zf Friedrichshafen Ag Shaft-hub-connection
FR2867223B1 (en) * 2004-03-03 2006-07-28 Snecma Moteurs TURBOMACHINE AS FOR EXAMPLE A TURBOJET AIRCRAFT
US20140064976A1 (en) * 2012-08-14 2014-03-06 Kevin L. Corcoran Rotor keyhole fillet for a gas turbine engine
GB2512016A (en) * 2012-09-24 2014-09-24 Arterius Ltd Methods
CA2966126C (en) * 2014-10-15 2023-02-28 Safran Aircraft Engines Rotary assembly for a turbine engine comprising a self-supported rotor collar
CN105570189B (en) 2014-10-31 2020-08-18 特灵国际有限公司 System and method for securing an impeller to a compressor shaft
US9909595B2 (en) * 2015-07-21 2018-03-06 General Electric Company Patch ring for a compressor
US10125785B2 (en) * 2015-10-16 2018-11-13 Pratt & Whitney Reduced stress rotor interface
US10190598B2 (en) * 2016-02-18 2019-01-29 Pratt & Whitney Canada Corp. Intermittent spigot joint for gas turbine engine casing connection

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3713676A (en) * 1971-05-07 1973-01-30 Gen Electric Predeformed rabbit joint
US4247256A (en) * 1976-09-29 1981-01-27 Kraftwerk Union Aktiengesellschaft Gas turbine disc rotor
EP0028217A1 (en) * 1979-10-25 1981-05-06 ELIN-UNION Aktiengesellschaft für elektrische Industrie Rotor for a thermic turbomachine
US4836750A (en) * 1988-06-15 1989-06-06 Pratt & Whitney Canada Inc. Rotor assembly
US5503490A (en) * 1994-05-13 1996-04-02 United Technologies Corporation Thermal load relief ring for engine case

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3088758A (en) * 1958-02-12 1963-05-07 Atomic Energy Authority Uk Thermocompensating joint
CH590414A5 (en) * 1975-07-04 1977-08-15 Bbc Brown Boveri & Cie
DE2851507C2 (en) * 1978-11-29 1982-05-19 Aktiengesellschaft Kühnle, Kopp & Kausch, 6710 Frankenthal Isolation spring body and its use
DE3625996A1 (en) * 1986-07-31 1988-02-04 Kuehnle Kopp Kausch Ag Rotor for an exhaust turbocharger
US4859143A (en) * 1987-07-08 1989-08-22 United Technologies Corporation Stiffening ring for a stator assembly of an axial flow rotary machine
KR0154105B1 (en) * 1989-10-30 1998-11-16 제랄드 피. 루니 Turbocharger compressor wheel assembly with boreless hub compressor wheel
US5056950A (en) * 1990-08-31 1991-10-15 Allied-Signal Inc Thermally activated joint
US5163816A (en) * 1991-07-12 1992-11-17 General Motors Corporation Wheel lock, centering and drive means and turbocharger impeller combination
DE4141427A1 (en) * 1991-12-16 1993-06-17 Stroemungsmaschinen Gmbh Gas turbine with radial-flow compressor of aluminium - has support sleeve in front side hub bore between drive shaft and compressor hub.
DE19540745A1 (en) * 1995-11-02 1997-05-07 Asea Brown Boveri Compressor vane to shaft connection
DE19728085A1 (en) * 1997-07-02 1999-01-07 Asea Brown Boveri Joint connection between two joining partners and their use
DE19728345A1 (en) * 1997-07-03 1999-01-07 Asea Brown Boveri Non-positive and positive connection of rotating components

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3713676A (en) * 1971-05-07 1973-01-30 Gen Electric Predeformed rabbit joint
US4247256A (en) * 1976-09-29 1981-01-27 Kraftwerk Union Aktiengesellschaft Gas turbine disc rotor
EP0028217A1 (en) * 1979-10-25 1981-05-06 ELIN-UNION Aktiengesellschaft für elektrische Industrie Rotor for a thermic turbomachine
US4836750A (en) * 1988-06-15 1989-06-06 Pratt & Whitney Canada Inc. Rotor assembly
US5503490A (en) * 1994-05-13 1996-04-02 United Technologies Corporation Thermal load relief ring for engine case

Also Published As

Publication number Publication date
DE19728345A1 (en) 1999-01-07
US6276863B1 (en) 2001-08-21
EP0893576A2 (en) 1999-01-27
US6126357A (en) 2000-10-03
JPH1172002A (en) 1999-03-16
DE59810313D1 (en) 2004-01-15
EP0893576B1 (en) 2003-12-03

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