EP0051178B1 - Appareil et méthode pour l'assemblage et le désassemblage - Google Patents

Appareil et méthode pour l'assemblage et le désassemblage Download PDF

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Publication number
EP0051178B1
EP0051178B1 EP19810108316 EP81108316A EP0051178B1 EP 0051178 B1 EP0051178 B1 EP 0051178B1 EP 19810108316 EP19810108316 EP 19810108316 EP 81108316 A EP81108316 A EP 81108316A EP 0051178 B1 EP0051178 B1 EP 0051178B1
Authority
EP
European Patent Office
Prior art keywords
rotor
coupling end
machine
disc
impeller
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
Application number
EP19810108316
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German (de)
English (en)
Other versions
EP0051178A1 (fr
Inventor
Carl J. Schuster
William A. Straslicka
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Carrier Corp
Original Assignee
Carrier Corp
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Filing date
Publication date
Application filed by Carrier Corp filed Critical Carrier Corp
Publication of EP0051178A1 publication Critical patent/EP0051178A1/fr
Application granted granted Critical
Publication of EP0051178B1 publication Critical patent/EP0051178B1/fr
Expired legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/60Mounting; Assembling; Disassembling
    • F04D29/64Mounting; Assembling; Disassembling of axial pumps
    • 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
    • F01D25/28Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures

Definitions

  • This invention generally relates to rotary machines, and more specifically to assembling and disassembling rotary machines.
  • Applicants European Patent Application EP-Al-50796. is also concerned with assembly and disassembly of similar equipment.
  • the impeller rotor and blades of a rotary machine such as a centrifugal compressor or expander must be removed from the machine for cleaning, maintenance or replacement.
  • rotary machines are often used with fluids containing a significant amount of particulates or debris. Over a period of time, these particulates and debris tend to collect or accumulate on the impeller blade surfaces, necessitating periodic removal of the impeller rotor and blades from the machine to clean or replace the blade surfaces. Routine inspection and maintenance, for example to repair or realign a rotor seal or blade, may also require removal of the impeller rotor from the machine.
  • French Patent FR-A-802529 utilizes a jib-type crane which may be mounted on a centrifugal compressor or blower to remove the casing from about the impeller of a turbomachine.
  • the apparatus of the invention is directed towards removing an axially extending impeller rotor. Since this rotor may be of significant length, apparatus is provided for jacking both ends of the rotor and thereafter displacing the rotor axially such that is may be serviced outside of the casing environment. Specific means are provided for lifting both ends of the rotor and for removing the casing around the blades. In this manner the entire shaft is made available for service without requiring further disassembly of the machine.
  • the machine is additionally designed such that the rotor is slid through the casing with one end of the rotor being supported by a carriage which cooperates with the machine frame to provide a rolling surface for displacing the rotor through the casing.
  • French Patent FR-A-802529 does not disclose any such casing nor is the problem addressed in what manner a long shaft may be serviced without physical removal from the equipment.
  • the invention is now concerned with the assembling and disassembling of an impeller rotor of a rotary machine.
  • assembly and disassembly apparatus for use with a rotary machine having an axially extending, rotatable impeller rotor, a fluid casing annularly extending around the rotor, and a machine frame supporting the rotor and casing, characterized by a disc end fixture disengagably connected to a disc end of the impeller rotor for vertically moving the disc end thereof between a rotor assembled position and a rotor lifted position and for horizontally moving the rotor through the fluid casing between the rotor lifted position and a rotor disassembled position; a coupling end fixture for vertically moving a coupling end of the impeller rotor between the rotor assembled and lifted positions, and a coupling end carriage supported by the machine frame and supporting the coupling end of the rotor as the rotor moves between the rotor lifted and disassembled positions.
  • machine 100 includes base plate 102, machine frame 104, impeller rotor 106, bearing means 110, and fluid casing 112.
  • Machine 100 also includes impeller blades 114, stator blades 116, diaphragm 120, stator housing 122, and rotor seal 124.
  • Machine frame 104 rests on base plate 102, which preferably extends forward, to the left as viewed in Figure 1, of the machine frame.
  • Impeller rotor 106 having disc end 126 and coupling end 130, axially extends along the top of machine frame 104 and is rotatably supported by bearing means 110 which, in turn, are supported by the machine frame.
  • bearing means 110 are of a conventional horizontal split type including disc end bearing 132, intermediate bearing housing 134, and coupling end bearing 136, which are all bolted to the top of machine frame 104.
  • Impeller blades 114 are rigidly secured to disc end 126 of rotor 106 and radially extend outward therefrom. Although two axially spaced sets of impeller blades 114 are shown in the drawings, it will be apparent to those skilled in the art that the present invention may be employed with a rotary machine having one or more sets of impeller blades.
  • Fluid casing 112 is secured to machine frame 104 and annularly extends around the machine frame and impeller rotor 106 rearward, to the right as viewed in Figures 1 and 2, of impeller blades 114.
  • the top of fluid casing 112 defines discharge or outlet opening 140.
  • Stator housing 122 is secured to the front end of fluid casing 112 and annularly extends around one or more impeller blades 114.
  • stator housing 122 is horizontally split, having upper section 142 and lower section 144, which preferably are bolted together along adjacent horizontal flanges.
  • Diaphragm 120 annularly extends around rotor 106 within stator housing 122; and the diaphragm also is horizontally split, including top half 146 and bottom half 150, which preferably are bolted together along adjacent horizontal flanges.
  • Stator blades 116 are secured to diaphragm 120 and radially extend inward therefrom between rotor blades 114.
  • a sealing member is secured to stator blades 116 and radially extends inward therefrom substantially to impeller rotor 106 to retard fluid flow through the area between the rotor and the stator blades.
  • Diaphragm 120 is radially spaced from stator housing 122, allowing radial expansion of the diaphragm.
  • Dowels 152 radially extend into generally concentric apertures 154 and 156 defined by diaphragm 120 and stator housing 122 respectively, preventing rotation of the diaphragm and stator blades 116 relative to the stator housing.
  • apertures 156 radially extend through stator housing 122, providing access to dowels 152 from the exterior of the stator housing.
  • Caps 160 may be disengagably secured to stator housing 122, for example by being threaded into apertures 156, to align dowels 152 within apertures 156 and to cover the dowels, preventing undesired outward radial movement thereof.
  • Fluid casing 112 includes inside radial flange 162, which annularly extends above machine frame 104 and rotor 106.
  • Rotor seal 124 is secured, preferably bolted, to machine frame 104 and fluid casing 112, specifically flange 162 thereof, covering the space between the machine frame, the fluid casing, and impeller rotor 106 to prevent leakage of a working fluid through this space.
  • Rotor seal 124 defines a plurality of axially extending threaded apertures located near the peripheral edge of the rotor seal, and some of these apertures are aligned with axially extending threaded apertures defined by radial flange 162 for bolting the rotor seal thereto.
  • some of the axial, threaded apertures defined by rotor seal 124 are located adjacent flat surfaces of radial flange 162.
  • inlet duct 164 is secured to the front of stator housing 122.
  • support means such as a stand (not shown) is secured to inlet duct 164 to support the duct and to provide additional support for stator housing 122 and the forward end of fluid casing 112.
  • a fluid is induced to flow through the inlet duct and past blades 114 and 116. If machine 100 is a compressor, then rotor blades 114 are rotated to compress the fluid flowing therepast. Alternately, if machine 100 is an expander, then the fluid causes rotation of blades 114. In either case, the fluid flows past blades 114 and 116 and through fluid casing 112, and the fluid is discharged from machine 100 via discharge opening 140.
  • FIGS 3 through 16 illustrate apparatus for assembling and disassembling machine 100 in accordance with a preferred embodiment of the present invention. More specifically, Figures 3 through 5 disclose apparatus for assembling and disassembling stator housing 122, specifically lower section 144 thereof, Figures 6 through 9 show apparatus for assembling and disassembling rotor seal 124 and disc end bearing 132, and Figures 10 through 16 illustrate apparatus for assembling and disassembling impeller rotor 106.
  • apparatus 200 for assembling and disassembling stator housing 122, specifically lower section 144 thereof.
  • apparatus 200 includes rails 202, screw jacks 204, posts 206, jack supports 210, guide rods 212, and wheels 214, 216, and 220.
  • Apparatus 200 further includes flanges 222, which radially extend outward from stator housing section 144, and flanges 224, which are located at the top of posts 206.
  • Jack supports 210 are fixed to posts 206.
  • screw jacks 204 are mounted on supports 210.
  • Screw jacks 204 extend through supports 210, and plates 226 are mounted on the tops of the screw jacks, above supports 210. With this arrangement, as is conventional, extension and retraction of screw jacks 204 move plates 226 upward and downward respectively relative to supports 210.
  • flanges 222 and 224 are then secured together by any conventional means wherein posts 206 provide additional support for stator housing 122.
  • flanges 222 and 224 define a plurality of vertically extending apertures (not shown) which are aligned as posts 206 are positioned adjacent to stator housing 122. Flanges 222 and 224 may then be secured to gether via bolts extending through aligned apertures.
  • guide rods 212 may be lowered through aligned apertures of flanges 222 and 224 into abutting contact with support platforms 210 of posts 206 wherein the guide rods help to guide movement of stator housing section 144 as section 144 is vertically moved between the assembled position shown in Figure 3 and rails 202.
  • inlet duct 164 is disengaged from the stator housing and removed in any suitable manner, for example by an overhead crane.
  • Caps 160 and dowels 152 associated with upper stator housing section 142 are removed, freeing section 142 from upper diaphragm section 146.
  • Upper section 142 of stator housing 122 is then disengaged from lower stator housing section 144 and fluid casing 112 and removed in any conventional manner, again for example by an overhead crane.
  • Upper diaphragm section 146 is disengaged from lower diaphragm section 150, and the upper diaphragm section is lifted up and away from machine 100, preferably by an overhead crane.
  • Rails 202 are then positioned on base plate 102 adjacent machine 100, between posts 206, and the rails are secured to the base plate by means such as bolts. If rails 202 extend forward of base plate 102 for any appreciable length, additional supports (not shown) may be provided for the rails. Preferably, rails 202 longitudinally extend parallel to the axis of rotor 106. Screw jacks 204 are then extended to move plates 226 into abutting contact with stator housing flanges 222.
  • lower stator housing section 122 is disengaged from fluid casing 112, and flanges 222 are disengaged from flanges 224.
  • Stator housing section 144 and diaphragm section 150 are now free to move downward; and by retracting screw jacks 204, plates 226, stator housing section 144, and diaphragm section 150 are lowered toward rails 202.
  • wheels 214, 216 and 220 are secured to the lower stator housing section.
  • wheels 214 are located beside stator housing section 144, wheels 216 are positioned to the sides and forward of the lower stator housing section, and wheels 220 are disposed to sides and rearward of stator housing section 144. This arrangement provides a very stable support for lower stator housing section 144 and lower diaphragm section 150 as these parts move along rails 202.
  • wheels 214, 216 and 220 may be secured to stator housing section 144 in any suitable manner.
  • wheels 214 are secured to stator housing section 144 via brackets 228, front wheels 216 are secured to the lower stator housing section via forwardly extending legs 230, plates 232, and flanges 222, and rear wheels 220 are secured to stator housing section 142 by means of rearwardly extending arms 234 and brackets 236.
  • screw jacks 204 are retracted to lower stator housing section 144 onto rails 202, as shown in Figures 4 and 5.
  • guide rods 212 are removed, freeing stator housing section 144 for movement along the rails.
  • posts 206 are carried away, thereby also removing screw jacks 204, supports 210, flanges 224, and plates 226.
  • Stator housing section 144 and diaphragm section 150 are then manually moved along rails 202 away from machine 100 into a diassembled position where the stator housing section and the diaphragm section are easily accessible to a laborer or to material handling equipment such as a crane.
  • Stator housing section 144 and diaphragm section 150 are then moved to a remote location.
  • rails 202 are kept in place because, as subsequently explained, they are further used in the disassembly of machine 100.
  • a selected rail 202 includes longitudinal flange 240 which cooperates with recess 242 defined by at least one wheel of assembly and diassembly apparatus 200 for guiding movement of lower section 144 along the rails.
  • the axial orientation of lower stator housing section 144 is maintained as section 144 moves between the assembled and disassembled positions. That is, as stator housing section 144 moves between the assembled and disassembled positions, the axis of section 144 is maintained substantially parallel to the axis of section 144 as assembled in machine 100.
  • apparatus 300 for assembling and disassembling rotor seal 124 and disc end bearing 132 in accordance with a preferred embodiment of the present invention.
  • apparatus 300 includes carrier rod 302, disc end bracket 304, coupling end frame 306, coupling end bracket 310, and turnbuckle 312.
  • Apparatus 300 further includes axially extending hole 314 defined by rotor seal 124, vertically extending aperture 316 defined by disc end bearing 132, shaft 320 extending from turnbuckle 312, and cylindrical bearing means 322 and 324.
  • aperture 316 and shaft 320 define complimentary threads, the inside diameters of bearing means 322 and 324 are approximately equal to the diameter of carrier rod 302, and the outside diameter of bearing means 322 is substantially equal to the diameter of hole 314. It should be noted that when machine 100 operates, a plate (not shown) covers opening 314 of rotor seal 124 and is secured thereto for preventing the working fluid from passing through opening 314.
  • disc end bracket 304 defines hole 326 and is disengagably secured to fluid casing 112, preferably to the forward radial surface of flange 162. Further, it is preferred that disc end bracket 304 be secured in place when machine 100 is originally assembled, before rotor seal 124 and disc end bearing 132 are initially positioned within the rotary machine.
  • coupling end frame 306 includes feet 330, upwardly extending, spaced, parallel legs 332, top cross member 334 which extends between the legs, and braces 336.
  • Coupling end bracket 310 defines hole 340, extends downward from cross member 334, and is secured thereto via means such as connecting plate 342 and bolts 344.
  • coupling end frame 306 is secured to machine frame 104. More specifically, referring to Figures 6 and 8, coupling end frame 306 is positioned with feet 330 resting on transversely opposed sides of machine frame 104, with cross member 334 transversely extending over coupling end 130 of impeller rotor 106, and with hole 340 of coupling end bracket 310 axially aligned with hole 326 of disc end bracket 304. Feet 330, and thus support frame 306, are then secured to machine frame 104 by, for example, bolts 346.
  • rotor seal 124 is axially spaced from radial flange 162 a distance sufficient to permit slight upward movement of the rotor seal, threaded pull rods 352 are threaded through vertically extending apertures defined by the rotor seal into abutting contact with the top surface of machine frame 104. Further rotation of these pull rods lifts rotor seal 124 away from machine frame 104. Preferably, rotor seal 124 is lifted into the lifted position shown in Figures 6 and 7 wherein hole 314 of the rotor seal is aligned with holes 326 and 340 of disc and coupling end brackets 304 and 310 respectively.
  • Bearing means 322 is inserted into hole 314 of rotor seal 124 and connected thereto in any conventional manner for unitary axial movement therewith.
  • bearing means 322 may be connected to rotor seal 124 by snap ring 354, plate 356, and bolt 360.
  • Turnbuckle 312 is secured to bearing means 324 via bolt 362.
  • the forward end of carrier rod 302 is inserted through coupling end hole 340; and then bearing means 324, with turnbuckle 312 connected thereto, is slid onto the forward end of the carrier rod.
  • Carrier rod 302 is then axially moved forward into fluid casing 112, through hole 314 of rotor seal 124, and through hole 326 of disc end bracket 304.
  • carrier rod 302 is threaded and nuts 364 and 366 are.located on the rear end of carrier rod, one on each side of coupling end bracket 310. Once carrier rod 302 is properly positioned, nuts 364 and 366 are tightened against coupling end bracket 310, as shown in Figure 6, preventing inadvertent axial movement of the carrier rod.
  • bearing means 324 and turnbuckle 312 are axially moved along carrier rod 302 until threaded shaft 320 is vertically aligned with aperture 316 of disc end bearing 132. Turnbuckle 312 is then extended, threading shaft 320 into aperture 316. Once shaft 320 securely engages disc end bearing 132, the disc end bearing is disengaged from machine frame 104 and turnbuckle 312 is retracted, lifting the disc end bearing from the assembled position shown in Figure 2 to the lifted position shown in Figures 6 and 7.
  • Disc end bearing 132 and rotor seal 124 are axially slid rearward along carrier rod 302 into a disassembled position where bearing 132 and seal 124 are easily accessible to a worker.
  • rotor seal 124 and disc end bearing 132 are moved completely outside of fluid casing 112.
  • rotor seal 124 is provided with support independent of carrier rod 302.
  • rotor seal 124 may be manually supported or supported by an overhead crane. Nut 364 is loosened, and carrier rod 302 is axially pulled rearward through holes 326 and 314, freeing rotor seal 124 from the carrier rod. Rotor seal 124 may then be further carried away from machine 100 either manually or by additional, conventional material handling equipment.
  • bearing means 324 is slid off the forward end of the carrier rod, removing turnbuckle 312 and disc end bearing 132 therefrom. Bearing 324, turnbuckle 312, and disc end bearing 132 may then be transported to a remote location.
  • Nut 364 is removed from carrier rod 302, and the carrier rod itself is pulled rearward through hole 340 and thence removed from machine 100.
  • disc end bracket 304 is manually disengaged from fluid casing 112 and carried away from machine 100.
  • Coupling end bracket 310 is similarly unbolted from coupling end support frame 306 and carried away from rotary machine 100.
  • coupling end frame 306 is left secured in place because, as explained below, it is used to remove rotor 106 from machine 100.
  • Machine 100 is now in the partially disassembled position shown in Figure 10.
  • the rotor seal 124 and disc end bearing 132 are quickly and easily removed from machine 100. Furthermore, with the preferred embodiment, the axial orientation of rotor seal 124 and disc end bearing 132 are maintained as the rotor seal and the disc end bearing move between their assembled and disassembled positions. More specifically, as rotor seal 124 moves between its assembled and disassembled positions, the longitudinal axis thereof, that is, the axis of the rotor seal which is parallel to the axis of impeller rotor 106 when both the impeller rotor and rotor seal are assembled in machine 100, is maintained substantially parallel to or colinear with the longitudinal axis of the rotor seal as assembled.
  • the longitudinal axis thereof that is, the axis thereof which is parallel to the axis of impeller rotor 106 when both the impeller rotor and the disc end bearing are assembled, is maintained substantially parallel to or colinear with the longitudinal axis of the disc end bearing as assembled.
  • Apparatus 400 includes disc end fixture 402, coupling end fixture 404, coupling end carriage 406, rail means 202, and groove 410 (shown in Figure 13) defined by the top surface of machine frame 104. More specifically, disc end fixture 402 includes disc end frame 412, screw jack 414, bracket 416, wheels 420, and cap 422, which is designed to closely fit over and around disc end 126 of rotor 106.
  • Coupling end carriage 406 includes support yoke 424, feet 426, and wheels 430; and coupling end fixture 404 includes coupling end frame 306 described above, screw jack 432, and lifting yoke 434, with yoke 434 comprising separable top and bottom halves 436 and 440 (best seen in Figure 12).
  • disc end frame 412 includes feet 442, spaced parallel legs 444, cross beam 446, and braces 450.
  • Feet 442 are supported by wheels 420 which are rotatably connected thereto in any conventional manner.
  • Legs 444 extend upward from feet 442
  • cross beam 446 is supported by and extends between the tops of the legs
  • braces 450 extend between the feet and the cross beam to further support the cross beam.
  • Screw jack 414 is secured to and extends upward from cross beam 446
  • bracket 416 is mounted on screw jack
  • cap 422 is secured to bracket 416 wherein extension and retraction of the screw jack moves bracket 416 and cap 42 upward and downward respectively relative to disc end frame 412.
  • screw jack 432 is mounted on coupling end frame 306, specifically cross member 334 thereof. Screw jack 432 extends downward through cross member 334, and a movable plate 452 of the screw jack is located below the cross member. Lifting yoke 434 is secured to plate 452 in any suitable manner for unitary, vertical movement therewith. With this arrangement, as will be appreciated by those skilled in the art, retraction and extension of screw jack 432 vertically raises and lowers, respectively, lifting yoke 434.
  • disc end fixture 402 is positioned on rail 202 wherein the rails support the disc end fixture for limited movement toward and away from machine 100.
  • a selected one or more wheels 420 of disc end fixture 402 defines recess 454 which cooperates with flange 240 of a selected rail 202 to guide movement of the disc end fixture along the rails.
  • screw jack 414 is adjusted to position cap 422 at a height where it fits over and around disc end 126 of rotor 106.
  • Disc end fixture 402 is then moved along rails 202 toward rotor 106 until cap 422 abuts against and fits over disc end 126 of the rotor.
  • Cap 422 is then disengagably secured to disc end 126 by suitable means, for example bolts 456 extending through cap and into the disc end of rotor 106.
  • Coupling end fixture 404 is assembled. More particularly, bottom half 440 of lifting yoke 434 is annularly slid underneath coupling end 130 of impeller rotor 106, and top half 436 of the lifting yoke is positioned on the impeller rotor surface above the bottom half of the lifting yoke. Halves 440 and 436 of lifting yoke 434 are then joined together, as shown in Figure 12. Screw jack 432 is mounted on frame 306, with movable plate 452 of the screw jack located below cross member 334. Lifting yoke 434 is secured to screw jack 432, specifically plate 452 thereof.
  • Disc end fixture 402 and coupling end fixture 404 are now employed, respectively, to lift disc end 126 and coupling end 130 of impeller rotor 106 from the rotor assembled position shown in Figure 10 to the rotor lifted position shown in Figure 11. More specifically, screw jack 414 of disc end fixture 402 is extended, raising cap 422 and disc end 126 of rotor 106. At the same time, screw jack 432 of coupling end fixture 404 is retracted raising lifting yoke 434 and couplng end 130 of rotor 106.
  • brace 460 (shown in Figures 14 and 16) is connected to cross beam 446 and to cap 422 of disc end fixture 402 to provide additional support for the cap and disc end 126 of rotor 106.
  • Coupling end carriage 406 is positioned on machine frame 104 with support yoke 424 abutting against coupling end 130 of rotor 106.
  • Yoke 424 and, thus, coupling end carriage 406 are disengagably secured to rotor 106 by, for example bolt 462 extending through the support yoke and into coupling end 130 of the rotor.
  • At least one of wheels 430 of carriage 406 extends into groove 410 to guide movement of the carriage and coupling end 130 of rotor 106 along machine frame 104.
  • screw jack 432 is disengaged from lifting yoke 434 and from coupling end frame 306 and removed from machine 100.
  • disc end fixture 402 is moved along rail 202 away from machine 100 to the position shown in Figure 16, pulling rotor 106 along the top of machine frame 104, through fluid casing 112, and into the disassembled position illustrated in Figure 16 wherein the rotor is easily accessible to a worker and to other rotor handling equipment.
  • rotor 106 is simply and conveniently moved into a disassembled position where the rotor and rotor blades 114 may be inspected or repaired, or wherefrom the rotor and blades may be moved, after being disengaged from disc end fixture 402, to another location specifically equipped for rotor inspection or repair.
  • the axial orientation thereof is maintained as the rotor moves between the assembled and disassembled positions. That is, as impeller rotor 106 moves between the assembled and disassembled positions, the axis of the rotor is maintained substantially parallel to the axis thereof when assembled in machine 100.
  • Coupling end carriage 406 is secured to coupling end 130 of rotor 106, lifting yoke 434 is fitted around the rotor, and the rotor is positioned, for example by an overhead crane, as shown in Figure 16, with carriage 406 resting on machine frame 104 and a selected one of wheel 430 extending into groove 410.
  • Disc end fixture 402, including brace 460, is mounted on rails 202 and secured to disc end 126 of rotor 106 via cup 422. Any equipment employed to move rotor 106 into the position shown in Figure 16 is then disconnected from the rotor and removed therefrom.
  • Disc end fixture 402 is then moved along rails 202 toward machine 100, pushing rotor 106 thereinto, with flange 240 of rail 202 and groove 410 of machine frame 104 guiding movement of the impeller rotor and maintaining the axial orientation thereof.
  • screw jack 432 is mounted on coupling end frame 306 and connected to lifting yoke 434, coupling end carriage 406 is removed, and brace 460 is removed from disc end fixture 402.
  • Disc end screw jack 414 is retracted and coupling end screw jack 434 is extended, lowering rotor 106 into its assembled position.
  • cap 422 is disengaged from disc end 126 of the rotor and screw jack 432 is disengaged from lifting yoke 434.
  • Disc end fixture 402, screw jack 432 and lifting yoke 434 are then all removed from machine 100.
  • disc end bracket 304 is secured to radial flange 162 of fluid casing 112, and coupling end bracket 310 is secured to coupling end frame 306.
  • the forward end of carrier rod 302 is inserted . through hole 340 of coupling end bracket 310.
  • Bearing means 324, with turnbuckle 312 and disc end bearing 132 connected thereto, is first slipped over the forward end of carrier rod 302, and then the forward end of the carrier rod is inserted through bearing means 322, with rotor seal 124 connected thereto.
  • Carrier rod 302 is then axially inserted within fluid casing 112 and through hole 326 of disc end bracket 304.
  • Rotor seal 124 and disc end bearing 132 are then moved along carrier rod 302 to their lifted positions shown in Figures 6 and 7.
  • Turnbuckle 312 is extended, lowering disc end bearing 132 into its assembled position.
  • Disc end bearing 132 is secured to machine frame 104, and turnbuckle 312 is retracted to disengage the disc end bearing therefrom.
  • Threaded pull rods 352 are threaded through vertical openings defined by rotor seal 124. Pull rods 352 are threaded downward into abutting contact with the top surface of machine frame 104 to support rotor seal 124 independent of carrier rod 302.
  • Carrier rod 302, bearing means 324, and turnbuckle 312 are then axially retracted and removed from machine 100.
  • Pull rods 352 are then rethreaded through the vertical apertures of rotor seal 124, lowering the rotor seal onto machine frame 104. These pull rods may then be removed. Similarly, bearing 322 and any means connecting this bearing to rotor seal 124 may also be removed. Rotor seal 124 is then axially moved along machine frame 104 into its assembled position. Guide rods may be extended through aligned axial apertures of rotor seal 124 and radial flange 162 of fluid casing 112 to guide axial movement of the rotor seal into its assembled position. Rotor seal 124 is secured to the machine frame 104 and to radial flange 162.
  • a plate is employed to cover opening 314 of seal 124, an this plate is secured to the rotor seal.
  • Coupling end frame 306, with coupling end bracket 310 secured thereto, is disengaged and removed from machine 100.
  • Intermediate bearing housing 134 and coupling end bearing 136 are replaced in any conventional fashion.
  • Screw jacks 204 are then extended, lifting lower stator housing section 144 and lower diaphragm section 150 off rails 202. Wheels 214, 216, and 220 are removed from lower stator housing section 144. Screw jacks 204 are further extended, raising stator housing section 144 into its assembled position and bringing radial flanges 222 into abutting contact with top flanges 224.
  • Flanges 222 and 224 are joined together, guide rods 212 are removed, and lower stator housing section 142 is secured to fluid casing 112.
  • Rails 202 may now be removed.
  • Upper diaphragm section 146 and upper stator housing section 142 are returned to their assembled positions, for example by an overhead crane, and secured to, respectively, lower diaphragm section 150 and fluid casing 112.
  • Caps 160 and dowels 152 associated with upper diaphragm section 146 and upper stator housing section 142 are replaced.
  • inlet duct 164 is resecured to stator housing 122.
  • support means (not shown) is secured to inlet duct 164 to support the inlet duct and to provide additional support for stator housing 122 and the forward end of fluid casing 112.
  • additional support flanges 224 of posts 206 are disengaged from flanges 222 of stator housing 122, and the posts and screw jacks 204 are removed from machine 100.
  • Machine 100 is now reassembled and ready for operation.
  • machine 100 is disassembled and reassembled comparatively quickly and simply.
  • guiding elements such as rails 202, groove 410, and carrier rod 302 to maintain axial orientation of various parts of machine 100 as these parts move between assembled and disassembled positions substantially facilitates realigning these many parts, significantly reducing the amount of human labor needed to realign the parts.

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Claims (5)

1. Appareil d'assemblage et de désassemblage utilisable avec une machine tournante comportant un rotor de propulsion (106) pouvant tourner et s'étendant axialement, un carter à fluide (112) s'étendant annulairement autour du rotor (106), et un bâti de machine (104) supportant le rotor et le carter, caractérisé par un support d'extrémité de disque (402), relié de façon séparable à l'extrémité de disque (126) d'un rotor de propulsion (106) pour déplacer verticalement l'extrémité de disque (126) entre une position d'assemblage de rotor et une position de soulèvement de rotor et pour déplacer horizontalement le rotor (106) au travers du carter à fluide (112) entre la position de soulèvement de rotor et une position de désassemblage de rotor; un support d'extrémité d'accouplement (404) pour déplacer verticalement une extrémité d'accouplement (130) du rotor de propulsion (106) entre les positions d'assemblage et de levage de rotor; et un chariot d'extrémité d'accouplement (406) supporté par le bâti de machine (104) et supportant l'extrémité d'accouplement (130) du rotor (106), lorsque le rotor (106) se déplace entre les positions de soulèvement et de désassemblage de rotor.
2. Appareil selon la revendication 1, caractérisé en outre par des rails (202) placés dans des positions adjacentes à la machine tournante (100) et sensiblement parallèles à l'axe du rotor pour guider le mouvement du support d'extrémité de disque (402) vers et à partir de la machine tournante (100), et une rainure (410) définie par une surface du bâti de machine (104) et s'étendant sensiblement parallèlement à l'axe de rotor pour guider le mouvement du chariot d'extrémité d'accouplement (406) le long du bâti de machine (104).
3. Appareil selon la revendication 2, caractérisé en ce que le support d'extrémité de disque (402) comprend un châssis d'extrémité de disque (412) déplaçable de façon à être rapproché et éloigné de la machine tournante (100), un chapeau de liaison (422) relié de façon séparable à l'extrémité de disque (126) du rotor de propulsion (106), et des moyens réglables (414, 416) joignant le chapeau de liaison (422) avec le châssis d'extrémité de disque (412) pour régler le hauteur du chapeau de liaison (422) et de l'extrémité de disque (126) du rotor de propulsion (106).
4. Appareil selon la revendication 1, caractérisé en ce que le support d'extrémité d'accouplement (404) comprend un châssis d'extrémité d'accouplement (306) supporté par le bâti de machine (104), un étrier de levage (434) entourant l'extrémité d'accouplement (130) du rotor de propulsion (106), et un moyen de levage (432) reliant l'étrier de levage (434) avec le châssis d'extrémité d'accouplement (306) pour déplacer verticalement l'étrier de levage (434) et l'extrémité d'accouplement (130) du rotor de propulsion (106).
5. Appareil selon la revendication 1, caractérisé en ce que le chariot d'extrémité d'accouplement (406) comporte une pluralité de pieds espacés (426), un étrier porteur (424) relié à et s'étendant entre les pieds (426), des moyens (462) pour relier de façon séparable l'étrier porteur (424) avec l'extrémité d'accouplement (130) du rotor du propulsion (106), et une pluralité de roues (430) reliées de façon tournante aux pieds (426) et supportées par et mobiles le long du bâti de machine (104).
EP19810108316 1980-10-27 1981-10-14 Appareil et méthode pour l'assemblage et le désassemblage Expired EP0051178B1 (fr)

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* Cited by examiner, † Cited by third party
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Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03118019U (fr) * 1990-03-19 1991-12-05
US6224332B1 (en) * 1999-05-14 2001-05-01 General Electric Co. Apparatus and methods for installing, removing and adjusting an inner turbine shell section relative to an outer turbine shell section
JP5729909B2 (ja) * 2010-02-25 2015-06-03 三菱重工業株式会社 ポンプの内部部材抜き出し/組み込み装置及び方法
CN103370499B (zh) 2011-02-09 2015-11-25 西门子公司 用于将支承体从燃气轮机的转子拆卸的方法以及管状的轴延长部
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CN111614219B (zh) * 2020-06-09 2023-03-21 安徽机电职业技术学院 一种电机端盖自动装配设备
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CN114915116B (zh) * 2022-01-21 2024-04-02 阳江核电有限公司 核电发电机转子抬轴盘轴方法及其抬轴支撑装置

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1991761A (en) * 1933-09-28 1935-02-19 Ingersoll Rand Co Pumping mechanism
FR802529A (fr) * 1936-03-03 1936-09-07 Beaudrey Bergeron Pompe à draguer
GB1317435A (en) * 1969-06-05 1973-05-16 Turnbull Marine Design Ship propeller shaft stern bearing arrangements
JPS5426957Y2 (fr) * 1975-02-05 1979-09-04
JPS5312262A (en) * 1976-07-21 1978-02-03 Hitachi Netsu Kigu Kk Control device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104024583A (zh) * 2011-12-30 2014-09-03 西门子公司 拉出和/或插入涡轮机轴承的方法以及执行该方法的设备
CN104024583B (zh) * 2011-12-30 2016-02-17 西门子公司 拉出和/或插入涡轮机轴承的方法以及执行该方法的设备
US9512723B2 (en) 2011-12-30 2016-12-06 Siemens Aktiengesellschaft Method for removing and/or installing a turbine bearing and a device for carrying out the method

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DE3175117D1 (en) 1986-09-18
EP0051178A1 (fr) 1982-05-12
JPS57114334A (en) 1982-07-16
JPS6327130B2 (fr) 1988-06-01

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