EP0647769A1 - Méthode pour changer et monter des boîtiers de turbine de grandes dimensions - Google Patents

Méthode pour changer et monter des boîtiers de turbine de grandes dimensions Download PDF

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Publication number
EP0647769A1
EP0647769A1 EP93116220A EP93116220A EP0647769A1 EP 0647769 A1 EP0647769 A1 EP 0647769A1 EP 93116220 A EP93116220 A EP 93116220A EP 93116220 A EP93116220 A EP 93116220A EP 0647769 A1 EP0647769 A1 EP 0647769A1
Authority
EP
European Patent Office
Prior art keywords
guide
wedge
pilot hole
fitting bolt
guide wedge
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.)
Withdrawn
Application number
EP93116220A
Other languages
German (de)
English (en)
Inventor
Helmut Karaus
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.)
ABB Management AG
Original Assignee
ABB Management AG
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 Management AG filed Critical ABB Management AG
Priority to EP93116220A priority Critical patent/EP0647769A1/fr
Publication of EP0647769A1 publication Critical patent/EP0647769A1/fr
Withdrawn legal-status Critical Current

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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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243Flange connections; Bolting arrangements
    • 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
    • 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

Definitions

  • the invention relates to a method for assembling and replacing large turbine housing parts.
  • Joints of turbine housing parts are usually fixed or positioned against each other with so-called guide, centering or fitting pieces, with wedges, fitting bolts, pins and similar parts.
  • the invention tries to avoid all these disadvantages. It is based on the task of creating a simple method for assembling and exchanging large turbine housing parts, in which no large machine tools have to be used and post-processing of the turbine housing parts is no longer necessary.
  • this is achieved in that a two-part guide wedge and a fitting bolt are used, the two parts of the guide wedge first being fitted in the wedge pockets of the housing parts to be connected, then a pilot hole is made in the parting plane of the pair of wedges, then the two halves of the Guide wedge are removed, fit over the pre-drilled hole and the final hole for the fitting bolt is now drilled, the guide wedges are then mounted and fixed by inserting the fitting bolt.
  • the advantages of the invention are, inter alia, that the inaccuracies between the independently produced wedge pockets are compensated for in a very simple and quick manner, no large machine tools are required, and the assembly and replacement of large divided turbine housings are easy to handle.
  • pilot bores are carried out as a prison bore with a hand drill and the wedge halves are positioned in front of the finished bore using a prison pin because this is the easiest and most precise way of drilling.
  • FIGS. 1 and 2 The invention is explained in more detail below using an exemplary embodiment and FIGS. 1 and 2.
  • the two housing parts 1 and 2 of a turbine have been manufactured at different locations, so that the manufacturing accuracy achieved is not sufficiently great.
  • the inaccuracies between the independently manufactured wedge pockets can be compensated for relatively easily by using a guide wedge 3 divided on the longitudinal side and a fitting bolt 4 which is cylindrical in this exemplary embodiment.
  • the two-part guide wedge 3 is first installed without a fitting bolt hole. There is a threaded hole in each half of the guide wedge 3 5 for a puller. The puller may be necessary when dismantling the guide wedge 3.
  • a Prison bore is carried out with the hand drill, for example ⁇ 10H7.
  • the next step is the removal of the two halves of the guide wedge 3. These are then positioned over a prison pin and clamped in a machine vise, where the final hole for the dowel pin 4, for example ⁇ 40H7, is made.
  • a conical fitting bolt connection can also be produced in another exemplary embodiment.
  • the guide wedge 3 is definitely installed and the finished fitting bolt 4, e.g. ⁇ 40k6, used.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Plates (AREA)
EP93116220A 1993-10-07 1993-10-07 Méthode pour changer et monter des boîtiers de turbine de grandes dimensions Withdrawn EP0647769A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP93116220A EP0647769A1 (fr) 1993-10-07 1993-10-07 Méthode pour changer et monter des boîtiers de turbine de grandes dimensions

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP93116220A EP0647769A1 (fr) 1993-10-07 1993-10-07 Méthode pour changer et monter des boîtiers de turbine de grandes dimensions

Publications (1)

Publication Number Publication Date
EP0647769A1 true EP0647769A1 (fr) 1995-04-12

Family

ID=8213328

Family Applications (1)

Application Number Title Priority Date Filing Date
EP93116220A Withdrawn EP0647769A1 (fr) 1993-10-07 1993-10-07 Méthode pour changer et monter des boîtiers de turbine de grandes dimensions

Country Status (1)

Country Link
EP (1) EP0647769A1 (fr)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1056624B (de) * 1958-07-11 1959-05-06 Licentia Gmbh In einer oder in mehreren Achsebenen geteiltes Axialturbinengehaeuse
DE1141997B (de) * 1952-05-20 1963-01-03 Prvni Brnenska Stojirna Zd Y K Turbomaschine
US3892500A (en) * 1974-07-10 1975-07-01 Westinghouse Electric Corp Adjustable axial positioning device
FR2310469A1 (fr) * 1975-05-06 1976-12-03 Rolls Royce Dispositif de positionnement de modules constitutifs d'un ensemble
FR2316467A1 (fr) * 1975-07-04 1977-01-28 Bbc Brown Boveri & Cie Dispositif d'ajustage d'elements coaxiaux de machine
JPS61223300A (ja) * 1985-03-27 1986-10-03 Hitachi Ltd 半割構造ターボ機械
FR2644843A1 (fr) * 1989-03-23 1990-09-28 Snecma Procede de montage de la turbine basse pression sur le corps haute pression d'une turbomachine a palier inter-arbres et outillages pour la mise en oeuvre du procede

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1141997B (de) * 1952-05-20 1963-01-03 Prvni Brnenska Stojirna Zd Y K Turbomaschine
DE1056624B (de) * 1958-07-11 1959-05-06 Licentia Gmbh In einer oder in mehreren Achsebenen geteiltes Axialturbinengehaeuse
US3892500A (en) * 1974-07-10 1975-07-01 Westinghouse Electric Corp Adjustable axial positioning device
FR2310469A1 (fr) * 1975-05-06 1976-12-03 Rolls Royce Dispositif de positionnement de modules constitutifs d'un ensemble
FR2316467A1 (fr) * 1975-07-04 1977-01-28 Bbc Brown Boveri & Cie Dispositif d'ajustage d'elements coaxiaux de machine
JPS61223300A (ja) * 1985-03-27 1986-10-03 Hitachi Ltd 半割構造ターボ機械
FR2644843A1 (fr) * 1989-03-23 1990-09-28 Snecma Procede de montage de la turbine basse pression sur le corps haute pression d'une turbomachine a palier inter-arbres et outillages pour la mise en oeuvre du procede

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 011, no. 067 (M - 566) 28 February 1987 (1987-02-28) *

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