Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
  • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
  • F04D29/00—Details, component parts, or accessories
  • F04D29/60—Mounting; Assembling; Disassembling
  • F04D29/64—Mounting; Assembling; Disassembling of axial pumps
  • F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
  • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
  • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
  • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
  • F04D29/00—Details, component parts, or accessories
  • F04D29/26—Rotors specially for elastic fluids
  • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
  • F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
  • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
  • F05D2230/00—Manufacture
  • F05D2230/60—Assembly methods
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
  • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
  • F05D2230/00—Manufacture
  • F05D2230/70—Disassembly methods
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
  • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
  • F05D2240/00—Components
  • F05D2240/20—Rotors
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
  • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
  • F05D2240/00—Components
  • F05D2240/90—Mounting on supporting structures or systems
• • Y—GENERAL 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
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T29/00—Metal working
  • Y10T29/37—Impeller making apparatus
• • Y—GENERAL 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
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49316—Impeller making
• • Y—GENERAL 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
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49316—Impeller making
  • Y10T29/4932—Turbomachine making
• • Y—GENERAL 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
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49316—Impeller making
  • Y10T29/4932—Turbomachine making
  • Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
• • Y—GENERAL 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
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49826—Assembling or joining
• • Y—GENERAL 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
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49826—Assembling or joining
  • Y10T29/49828—Progressively advancing of work assembly station or assembled portion of work

Definitions

• Securing device for securing a rotor of a fluid machine erected transversely to a horizontal plane against overturning and alignment methods for this purpose
• the invention relates to a securing device for securing a transverse to a horizontal plane erected rotor of a turbomachine against tipping, with at least one support surface through which a transverse to the horizontal plane rotor is laterally supported by the securing device. Furthermore, the invention relates to a method for the vertical alignment of a perpendicular to the horizontal plane auf mixden rotor of a turbomachine.
• a rotor variant comprises a plurality of adjacent elements, which are braced by a tie rod extending centrally through the elements.
• these elements are rotor disks and, on the other hand, pipe sections, so-called hollow shafts, which can rest on the rotor disks.
• the clamping of the rotor disks and the hollow shafts takes place with respective end nuts screwed on the tie rod nuts, often the compressor side provided screw nut is designed as a hollow shaft.
• the face-side juxtaposed rotor discs usually carry at their outer peripheries the blades of the turbine and the compressor. Instead of a central tie rod, it is also known to use several decentralized tie rods.
• an assembly tool which essentially comprises two bearing blocks.
• the two bearing blocks are placed at a distance from each other and the rotor is placed on them.
• One of the two bearing blocks - the so-called turning block - is equipped with a joint arranged between foot and bearing surface, which is fastened to one end of the rotor.
• the rotor is thus placed so that its example compressor side end can be attached directly to the joint of the turning block.
• the other bracket then supports the rotor on the turbine side.
• the joint which is attached to the reversing jack, serves to relocate the rotor from the horizontal position to a vertical position. This is done at the turbine end of the
• Rotor screwed on a trailer nut on the tie rod A rope of a crane is attached to the hanger by means of a shackle. As the crane lifts the turbine end of the rotor, the compressor end rotates about the pivot point of the joint. The lifting process is completed when the rotor has reached an approximately vertical position. Then this is secured by means of a fuse, which is also provided on the turning block against tipping over. As a rule, this lock comprises a locking bolt, which is provided on the turning bracket above the hinge and blocks the return movement of the rotor from the vertical. Then the trailer nut is dismantled, after which the actual work can be done on the vertical rotor (or tie rod).
• the tie rod is first set up vertically and then the individual rotor discs are threaded successively from above onto the tie rod by means of a crane. Subsequently, a turbine-side rotor nut is screwed. When disassembling a fully assembled rotor, the turbine-side rotor nut is removed after its vertical placement, after which the individual rotor discs can be removed by means of a crane tie rods. The rotor then essentially only comprises the tie rod.
• a similar set-up device with a turning block is known from German Offenlegungsschrift 24 26 231.
• Central A first stop is fastened to the foundation below the turnbuckle.
• the end of the rotor is not attached to the turning block, but a rotor point spaced from the end.
• the arranged on the shorter rotor portion coupling flange is located after the vertical installation on the first stop, after which on the other side of the flange then adapted a second stop and fixedly connected by screws with the first stop to secure the rotor against tipping
• Object of the present invention is to provide a securing device for securing a transversely mounted over a horizontal plane rotor or tie rod of a turbomachine in which the rotor resp. Tie rod is particularly easy to align in the vertical. Another task is to specify a corresponding method for this purpose.
• the first object is achieved by a securing device having the features of claim 1.
• the object directed to the method is achieved by a method according to the features of claim 11.
• the invention is based on the recognition that a particularly simple alignment of the approximately perpendicular to the horizontal plane erected rotor resp. Tie rod can be achieved in the vertical if the at least one support surface of the securing device, on which the rotor is already present during the alignment according to the invention, preferably at least slightly displaced.
• the forces acting from the rotor to the securing device transverse to the normal force forces are comparatively small, so that the securing device can be adapted accordingly adapted.
• the vertical rotor allows a particularly simple threading or unthreading of rotor disks on the tie rods, without these touching during lifting or lowering due to a misalignment of the tie rod latter.
• the securing device is part of a modular mounting device, which in addition to the preferably designed as a scaffold safety device comprises a separately formed turning block. The inventive method is then time-saving feasible with a device according to the invention while achieving the aforementioned advantages.
• the support surface is arranged on a ring composed of at least two ring segments.
• the support surface can thereby create a part of the lateral surface of the rotor, in particular on the lateral surface of a hollow shaft or a rotor disk.
• the support surface is the inner cylindrical surface of the ring, wherein the ring attached to the rotor may also be provided as a mechanical protection.
• the ring can either be attached to the still located in the horizontal rotor, so even before the erection of the rotor in the vertical. Or, the ring is already preassembled in the frame-like securing device and opened so far that the rotor section, which is to be inserted into the ring, can be introduced.
• one of the two ring segments pivotally mounted opposite the other ring segment. This allows a particularly easy mounting of the ring on the rotor, regardless of whether the ring is pre-assembled on the horizontal rotor or whether the ring is attached to the securing device in advance.
• a plurality of screw connections or a plurality of hydraulic cylinders which each extend parallel or nearly parallel to the horizontal plane and which have elements movable parallel or nearly parallel to the horizontal plane, such as screws or hydraulic pistons.
• at least three screw or hydraulic cylinder are provided in such a way to shift the rotor positioned approximately vertically that it can be brought from an approximately vertical position in the vertical.
• more than three, in particular preferably eight or nine screw connections or hydraulic cylinders are provided in order to ensure a particularly secure lateral support and a particularly exact alignment. This is particularly required for heavy duty gas turbines used in commercial power generation, since their rotor weight can be several tens of thousands of kilograms.
• the screw or hydraulic cylinder of the securing device are arranged like a beam around a virtual center.
• the securing device and the turning block are to be aligned and fastened to one another on the foundation in such a way that, in the vertical, the projection of the virtual center point is centralized
• Rotor support point on the turning block coincides.
• the central rotor support point is the point on the axis of rotation of the joint, on which the center of gravity of the rotor is to be placed.
• the vertical alignment of the rotor can take place comparatively quickly with comparatively little effort.
• at least one eccentric disc may be provided, in which the support surface is arranged.
• the rotor arranged approximately perpendicularly is preferably provided with two nested eccentric disks, of which the inner eccentric disk has the supporting surface. This also makes it possible to achieve a particularly simple alignment of the approximately vertically positioned rotor in the vertical.
• the securing device has a platform or working platform jacked up on a plurality of supports and struts above the foundation.
• the platform can serve, for example, as a work platform for fitters, who make the alignment of the rotor in the vertical.
• the support surface at the height of the platform, for example in the bottom is provided.
• the one or more support surfaces may then be connected to the platform via the fittings or the hydraulic cylinder.
• the distance between the joint of the turning block and the supporting surface arranged above about 2 - 3 m.
• FIG 2 shows the mounting device according to FIG 1 with vertical rotor
• 3 shows the top view of the securing device with open recording and 4 shows the top view of the securing device with inserted rotor.
• FIG. 1 a stored on two bearing blocks 11 rotor 13 a heavy stationary gas turbine is shown.
• the rotor 13 includes a tie rod 15 which extends centrally through a plurality of turbine disks 17 and compressor disks 19.
• the compressor-side end of the rotor 13 is shown on the left.
• the turbine disks 17 and the compressor disks 19 are rotor disks 21 and carry at their outer ends blades which can be exposed to a compressible flow medium of the gas turbine.
• a front hollow shaft 22 is screwed onto the tie rod 15 at the compressor-side end 33 of the rotor 13.
• a nut 24 is provided.
• a mounting device 23 is provided next to the two bearing blocks 11, which is arranged rotorend perfume.
• the mounting device 23 comprises a turning bracket 27 which is mounted on a foundation 29.
• the turning block 27 is set up in alignment with the two bearing blocks 11 and has at its tip a joint 31 which is connected to the compressor-side end 33 of the rotor 13.
• the rotor 13 is rotatable about an axis of rotation parallel to the horizontal plane 47 of the joint 31.
• the joint 31 comprises a roller-mounted receptacle for a turntable 37 rotatable about a vertical axis 35.
• the rotor support point is also located on the vertical axis 35.
• a trailer nut 41 is mounted on the means of a shackle the rope of a crane can be struck.
• the mounting device 23 further comprises a securing device 45 designed as a frame 43, which is anchored separately in the foundation 29 by the turning block 27.
• the framework 43 comprises a platform 49 or work platform jacked up on four vertical supports 64.
• further struts 65 extending transversely to the supports 64 are provided on each side edge of the framework 43, which additionally connect the foundation-side ends of the supports 64 to the platform 49.
• part of the platform 49 and the struts 65 arranged underneath can be moved out of the pivoting range of the rotor 13.
• the platform 49 and the securing device 45 then have an opened receptacle (see FIG.
• the rotor 13 By lifting the turbine-side end 39 of the rotor 13 with the crane, the rotor 13 is lifted from the two bearing blocks 11, wherein the compressor-side end of the rotor 13 rotates about the axis of rotation of the joint 31.
• the rotor 13 can then be turned from its horizontal position (FIG. 1) into the vertical position (FIG. 2), after which it is secured against overturning by means of the securing device 45. For this purpose, the recording is closed. Subsequently, the rotor 13 is in the position shown in FIG 2.
• the entire weight of the stationary in stationary gas turbine comparatively heavy rotor 13 then loads on the turn block 27, whereas the frame 43 can prevent the tipping of the rotor 13 with comparatively small forces.
• the least force is required when the rotor 13 is vertical is aligned and the axis of symmetry 46 of the rotor 13 coincides with the axis 35 of the turntable 37.
• earthquake safety means that the acceleration forces that occur in comparatively weak earthquakes with a comparatively low level of force on the
• Rotor 13 in the order of about H g (Ig simple acceleration of gravity) collected by the securing device 45 and can be derived via the platform 49 and the struts 65 into the foundation 29.
• FIGS. 3 and 4 show the plan view of the platform 49 of the securing device 45 according to the sectional view IV. IV of FIG 2.
• FIG. 4 shows the closed platform 49 with centrally arranged tie rod 15 and front hollow shaft 22 according to the sectional view IV. IV of FIG 2.
• a centrally disposed opening 51 is provided, in which an axial portion of the hollow shaft 22 can be inserted.
• the opening 51 is surrounded by a segmented ring 53 whose first segment 55 comprises a segment arc of approximately 270 ° and whose second segment 57 comprises a segment arc of approximately 90 °.
• the second ring segment 57 is pivotable relative to the first ring segment 55 about an axis of rotation 59, which serves for easy and quick closing and opening of the ring 53 (see FIG. Both segments 55, 57 each have an inwardly directed support surface 61, which can each be applied to a portion of the lateral surface of the rotor 13 and the tie rod 15.
• the ring 53 lies in a plane parallel to the horizontal plane 47, ie parallel to the foundation 29, and can be displaced by means of an auxiliary device supporting it within this plane for vertical alignment of the rotor 13.
• the Auxiliary device comprises, for example, a plurality of screw connections 63 fastened to the platform 49. Each of these screw connections 63 has a screw axis 67 which likewise lies in the plane parallel to the horizontal plane 47.
• the screwed connections 63 are arranged radially in the closed ring 53, so that their screw axes 67 meet in a virtual center 66.
• screw 63 can also be provided in each case a hydraulic arrangement with a movable piston rod to laterally support the ring 53 and thereby align the rotor 13 (or tie rod 15) relative to the turn block 27 such that of this from an approximately vertical orientation in a vertical alignment can be shifted.
• the ring 53 may be mounted in a double-nested eccentric, so that the opening 51 relative to the axis 35 of the turning block 27 is arbitrarily alignable.
• the ring 53 is only optional.
• the lateral support of the rotor 13 it is also possible for the lateral support of the rotor 13 to take place directly from the screw connections 63 or directly from the piston rods of the hydraulic cylinders.
• the support surfaces 61 would then be arranged on the inwardly projecting free ends 69 of the screw 63 or the inwardly projecting free ends of the piston rods of the hydraulic cylinders, which would then be applied directly to the lateral surface of the rotor 13.
• the ring 53 and the platform 49 In order for the rotor 13 to be pivoted into the opening 51 when lifting its turbine-side end 39, the ring 53 and the platform 49 must first be opened.
• the second segment 57 of the ring 53 is pivotable about the rotation axis 59 according to the arrow 60 from a closed position to an open position (shown).
• the struts 65 and the railing 70 of the working platform shown in the bottom of FIG. 3 are of the Platform 49 folded away according to the arrow 62, so that a total of the recording is open.
• FIG 4 shows the top view of the securing device 45 with the approximately completely closed ring 53.
• the ring 53 surrounds the hollow shaft 22, so that the support surfaces 61 abut against the lateral surface of the hollow shaft 22.
• the ring 53 is displaceable over the individual screw 63 in the plane parallel to the foundation 29, so that the center of the ring 53 and thus the center of the tie rod 15 relative to the turn block 27 and thus relative to the central Rotorabstütztician is slightly displaced to the rotor thirteenth in a vertical orientation.
• the rotor 13 to be vertically aligned may comprise only the tie rod 15, which is secured against overturning by the support surfaces 61.
• the rotor 13 can also be understood to mean a tie rod 15 which is fully fitted with rotor disks 19, 21 and which is supported in an analogous manner.
• Tie rod 15 are aligned in the vertical, by the contact surfaces 61, at which the rotor 13, respectively, during alignment. the tie rod 15 is supported so displaced that it comes to stand perpendicular with respect to the horizontal plane.

Landscapes

• Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Turbine Rotor Nozzle Sealing (AREA)
• Structures Of Non-Positive Displacement Pumps (AREA)

Priority Applications (1)

Applications Claiming Priority (3)

Publications (2)

Family

ID=38436746

Family Applications (3)

Family Applications Before (1)

Family Applications After (1)

Country Status (7)

Families Citing this family (9)

Family Cites Families (16)

• 2007
  • 2007-04-16 EP EP20070007681 patent/EP1983161A1/fr not_active Withdrawn
• 2008
  • 2008-04-03 PL PL08735742T patent/PL2134928T3/pl unknown
  • 2008-04-03 ES ES08735742T patent/ES2365375T3/es active Active
  • 2008-04-03 US US12/595,556 patent/US8667678B2/en not_active Expired - Fee Related
  • 2008-04-03 JP JP2010503450A patent/JP4937408B2/ja not_active Expired - Fee Related
  • 2008-04-03 WO PCT/EP2008/053993 patent/WO2008125507A1/fr active Application Filing
  • 2008-04-03 WO PCT/EP2008/053992 patent/WO2008125506A1/fr active Application Filing
  • 2008-04-03 JP JP2010503449A patent/JP4948644B2/ja not_active Expired - Fee Related
  • 2008-04-03 EP EP08735741.4A patent/EP2134927B1/fr not_active Not-in-force
  • 2008-04-03 EP EP20080735742 patent/EP2134928B1/fr active Active
  • 2008-04-03 US US12/596,215 patent/US9003656B2/en not_active Expired - Fee Related
  • 2008-04-03 AT AT08735742T patent/ATE510998T1/de active

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