US3628884A - Method and apparatus for supporting an inner casing structure - Google Patents

Method and apparatus for supporting an inner casing structure Download PDF

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Publication number
US3628884A
US3628884A US50151A US3628884DA US3628884A US 3628884 A US3628884 A US 3628884A US 50151 A US50151 A US 50151A US 3628884D A US3628884D A US 3628884DA US 3628884 A US3628884 A US 3628884A
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United States
Prior art keywords
inner casing
casing
outer casing
rod member
lever
Prior art date
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Expired - Lifetime
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US50151A
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English (en)
Inventor
George M Mierley Sr
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CBS Corp
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Westinghouse Electric Corp
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Publication date
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Classifications

    • 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
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/10—Centrifugal pumps for compressing or evacuating
    • F04D17/12—Multi-stage pumps
    • F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
    • 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
    • F04D29/62—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
    • F04D29/624—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • 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
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
    • 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
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/644—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins for adjusting the position or the alignment, e.g. wedges or eccenters
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/20—Hydro energy
    • 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
    • Y10T29/49895—Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"]

Definitions

  • a rotary machine such as a turbine, having outer and inner tubular casings encompassing a rotor and divided along a horizontal plane into upper and lower semicylindrical halves.
  • the improvement comprises an arrangement including an annular series of eccentric bushing structures inserted radially through apertures in the outer casing to adjustably fit axially key slots on the periphery of the inner casing to support the inner casing concentrically relative to the axis of rotation of the rotor.
  • external screw means are connected to internal levers to move the inner easing into sealing relation with the outer casing.
  • the invention also involves the method of supporting the inner casing within the outer casing and moving the inner casing relative to the outer casing.
  • WITNESSES RE 08 mv E Vr WE M M e g r 0 e G 4/M4/L/ 4 5 (A METHOD AND APPARATUS FOR SUPPORTING AN INNER CASING STRUCTURE BACKGROUND OF THE INVENTION
  • This invention relates to a rotary machine such as a turbine having outer and inner casings and more particularly to an arrangement and method for supporting the inner casing.
  • the outer and inner casing structures are normally divided into upper and lower halves enclosing a bladed rotor structure and a corresponding stationary blade structure.
  • the inner casing halves are fitted with the stationary blades.
  • the lower half of the inner casing is fitted into the lower outer casing half.
  • the rotor is placed in the lower halves of the casings and the upper half of the inner casing is inverted and secured to the lower half.
  • the upper half of the outer casing is inverted and secured to the lower half.
  • a pair of jackscrews is inserted radially inward from the outer casing to maneuver the inner casing vertically and horizontally in planes normal to the longitudinal axis of the turbine and make it concentric therewith.
  • an arrangement and method must still be provided to move the inner casing axially into sealing relation with the outer casing to prevent leakage of the high-pressure cooling air.
  • the inner casing is positioned during assembly in a backed-off longitudinal position so that the shoulder and the flange do not come into contact as the upper half of the outer casing is lowered into position. This protects the seal surfaces from possible damage.
  • the inner casing must then be shifted back, so that the shoulder and the flange are in sealing relation.
  • the following invention relates to an elastic fluid utilizing machine and more specifically to an arrangement and method for concentrically supporting the inner casing of the machine relative to the axis of rotation of the rotor of the machine.
  • the machine comprises a tubular outer casing and a tubular inner casing disposed within the outer casing.
  • the inner casing encompasses a rotating rotor structure. Hot motive gases, derived from fuel combustion, are expanded as they flow through the machine to drive the rotor structure as well known in the art.
  • a plurality of apertures are radially disposed in the outer casing and a plurality of corresponding key slots are disposed on the periphery of the inner casing.
  • the outer casing has an annular flange extending radially inward and the inner casing has an annular shoulder extending radially outward.
  • the shoulder and flange are in abutment and form a seal between the inner and outer casing.
  • the inner casing is disposed in a backed-off axial position relative to the outer casing. Therefore, when the upper half of the outer casing is lowered onto the lower half of the outer casing and firmly secured thereto, the inner casing must be moved axially into sealing relation with the outer casing.
  • a pair of screws which is secured externally to the outer casing and extends radially therethrough, one on each side, abuts corresponding levers mounted on the inner surface of the outer casing and is positioned axially adjacent the inner casing.
  • the screws rotate the levers.
  • the levers axially move the inner casing, so that the shoulder on the inner casing comes into sealing relation with the flanges on the outer casing.
  • the method of supporting the inner casing within the outer casing and of moving the inner casing into sealing relation with the outer casing comprises the following steps:
  • FIG. I is a side elevational view of an axial flow gas turbine power plant having the invention incorporated therein;
  • FIG. 2 is an enlarged sectional view generally taken along line IlII in FIG. 1;
  • FIG. 3 is an enlarged view of the turbine portion of the power plant shown in FIG. 1, partially exploded and in a jacked-up distorted position;
  • FIG. 4 is an isometric view of a portion of the lower half of the outer and inner casings of the turbine with the rotor structure, rotary blades, and stationary blades removed;
  • FIG. 5 is a plan view of an eccentric bushing structure formed in accordance with the present invention.
  • FIG. 1 there is shown a gas turbine power plant 10 of the axial flow type having the invention embodied therein.
  • this machine includes an air compressor section 12, a fuel combustion section 14, a turbine section 16, an air inlet casing 18 and an exhaust hood 20.
  • an outer casing structure 22 comprising an inlet casing 23, a compressor casing 24, a combustion casing 25, a turbine casing 26, and an outlet casing 27.
  • the above casings are joined to each other and to the inlet casing 18 and exhaust hood 20 by suitable bolted peripheral external flanges and are divided into upper and lower casing halves in a horizontal plane coinciding with the central longitudinal axis of the rotor, the upper and lower casing halves being joined to each other by suitable bolted horizontal flanges, for expediency in manufacture, assembly and disassembly for service, as known in the art.
  • the compressor section 12 includes an inner casing 30, a compressor rotor structure 31, and corresponding alternating annular rows of stationary blades 32 and rotating blades 33 decreasing in height from left to right.
  • the turbine section 16 includes an inner casing .34, a turbine rotor structure 35 and corresponding alternating annular rows of stationary blades 36a and rotating blades 36bincreasing in height from left to right.
  • the stationary blades 36a as shown, are of the hollow type so that they may be air cooled.
  • an annular chamber C is defined by the outer casing 26 and inner casing 34 for the pressurized cooling air for the hollow blades 36a.
  • the compressor rotor structure 31 is drivenly connected to the turbine rotor structure 34 by a connecting shaft 37, the rotor structures 31 and 34 and the shaft 25 being defined as the rotor spindle 38 and being rotatably supported by suitable bearings 38 and 39 at each end.
  • the turbine rotor spindle 38 may be connected to an output shaft 40 for transmitting useful shaft power for driving a load (not shown).
  • the outer casing 26 is divided into upper and lower halves 26a and 26b along a central horizontal plane and joined to each other along horizontal external flanges 41 by suitable bolts 42.
  • the outer turbine casing 26 is also provided with suitable peripheral flanges 43 for connection to the adjacent casings 25 and 27 (FIG. 1).
  • the turbine inner casing 34 is divided into upper and lower halves 34a and 3412 joined together along horizontal flanges 44 by suitable bolts 46.
  • the inner casing 34 is supported from the outer casing 26 by a plurality of eccentric bushing structures 52, as shown in FIGS. 2 and 4, which are radially disposed in openings in the turbine outer casing 26 and extend into axially extending key slots 54 on the periphery of the inner casing 34.
  • a plurality of eccentric bushing structures 52 which are radially disposed in openings in the turbine outer casing 26 and extend into axially extending key slots 54 on the periphery of the inner casing 34.
  • four of the eccentric bushing structures 52 are used to support the inner casing 34, two of which are in a vertical plane passing through the center of the rotor 35, one on the top half of the casing 34a and the other on the bottom half 3412.
  • the other two bushing structures 52 are disposed below the horizontal centerline on the bottom half 34b and are equidistant from the vertical centerline.
  • FIG. 4 for purposes of clarity, the rotor 35, rotary blades 36a, and stationary blades 36b have been removed.
  • Three eccentric bushing structures 52 are shown, with the bushing on the bottom of the figure being partially exploded. Referring to the exploded bushing structure 52, it can be seen that the structure comprises a tubular outer member or bushing member 56 and a rod member 58 disposed in an eccentric opening in the outer member 56. The outer member 56 and the inner rod member 58 can rotate relative to each other.
  • a keyway 59 On the radially inner end of the rod member 58 and integral therewith is a keyway 59 (FIGS. 4 and The key slot 54 corresponds in size to receive the keyway 59, although the slot is longer in an axial direction than the keyway for reasons which will be subsequently explained.
  • a pair of jackscrews 61 (FIGS. 2 and 4) is located on the lower half of the turbine outer casing 26b, one on each side of the vertical centerline, disposed radially inward therefrom.
  • the screws 61 are initially used to position the inner casing 34 concentrically relative to the axis of rotation RR of the ro I01.
  • a second pair of jackscrews 63 is disposed radially through the lower half of the outer casing 26b and is located below the horizontal centerline equidistant from the vertical centerline, as shown in FIG. 2 (only one is shown in FIG. 3).
  • Each jackscrew 63 is in abutting relation with a lever 64 (FIG. 4).
  • the lever 64 is mounted on the inner surface of the lower half of the outer casing 26b and is secured to a fulcrum 66 by a pin 67.
  • the turbine section 16 is shown in a jacked-up position with the upper half of the outer casing 260 removed.
  • the inner casing 34 is comprised of a frustoconical portion 34a and a cylindrical portion 34b.
  • Projecting radially outward from the inner casing 34 is an annular shoulder 69 separating the frustoconical and cylindrical portions.
  • Projecting radially inward from the turbine casing 26 is an annular flange 71.
  • the right-hand surface of shoulder 69 and the left-hand surface of flange 71 abut each other in sealing relation as best seen in FIGS. 1 and 4.
  • four bushing structures 52 are shown supporting the inner casing 43, more or less can be used.
  • the lower outer casing half 26b is axially aligned with a taut wire or laser beam representing the axis of rotation of the rotor RR' (FIGS. 2 and 4).
  • the inner casing halves 34a and 3417 are fitted with stationary blades 36b.
  • the lower half of the inner casing 34b is then lowered into the lower half of the outer casing 26b and is supported on the jackscrews 61.
  • the upper half of the inner casing 34b is inserted so that it is then in a backed-off position meaning that the annular shoulder 69 and the annular flange 71 do not come into contact with each other.
  • the inner casing 34 can be moved vertically and horizontally to make it concentric with the axis of rotation R-R'.
  • the tubular outer member 56 of bushing structure 52 can turn, moving the keyway 59 either to the right or the left, as shown by the dash-dot lines.
  • the keyway 59 is kept aligned with the key slot 54 as the outer member 56 rotates around the rod member 58.
  • By moving the keyway 59 the axial position of the keyway is changed, requiring the key slot 54 to be axially longer. This provides the versatility needed to easily line up the inner casing 34, properly position it relative to the axis of rotation RR, and to support the inner casing.
  • the rod member 58 and tubular outer member 56 are securely fastened together by any suitable means such as by welding (not shown).
  • the bushing structures 52 are then secured to the outer casing 26 by any suitable means.
  • a jacking device 73 is placed between ground and the lower half of the outer casing 26b, about midway between the flanges 43, although two jacks can be used, one being placed under each of the flanges 43.
  • Raising the jack 73 causes a slight bowing in the upward direction causing small axial clearances indicated by letter C between peripheral flanges 43 in the upper half of the turbine casing 26a (the bottom half still being bolted).
  • the bowing will also cause a slight clearance space d between the flanges 69 and 71.
  • This clearance d protects the mating seal surfaces on flanges 69 and 70 from damage when the upper turbine casing 26a is either lifted off of the bottom half of casing 26b or when it is replaced.
  • a rotary machine comprising a tubular outer casing structure
  • said lever being positioned axially adjacent by the inner casing structure so that when said lever is actuated by said screw, said lever will abut the shoulder on the inner casing structure and move the structure axially into sealing relation with the flange on the outer casing structure.
  • each of the eccentric bushing structures comprise a tubular outer member having an eccentric opening therein
  • said outer and rod members being rotatable relative to one another enabling said rod member to move into a position to be inserted into the corresponding slot on the inner casing structure.
  • lever means secured to the inside surface of the outer casing structure and in abutment with said screw means
  • lever means being axially adjacent the shoulder of the inner casing and said lever means being adjusted by said screw means so that said shoulder of the inner casing is in sealing relation with said annular flange of the outer casing.
  • each of the eccentric bushing structures comprises a tubular outer member having an eccentric opening therein, I a rod member rotatably inserted within said openings,
  • said keyway being insertable in said key slot to support the inner casing relative to the outer casing
  • fastening means to secure each of said outer members and said rod members together.
  • a method of supporting an inner casing of a rotary body within an outer casing of a rotary body comprising steps of:
US50151A 1970-06-26 1970-06-26 Method and apparatus for supporting an inner casing structure Expired - Lifetime US3628884A (en)

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US5015170A 1970-06-26 1970-06-26

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US (1) US3628884A (de)
JP (1) JPS5421601Y2 (de)
BE (1) BE769109A (de)
CH (1) CH539197A (de)
DE (1) DE2128245A1 (de)
FR (1) FR2096514B1 (de)
GB (1) GB1303573A (de)
NL (1) NL7108852A (de)

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Also Published As

Publication number Publication date
BE769109A (fr) 1971-11-03
CH539197A (de) 1973-07-15
GB1303573A (de) 1973-01-17
FR2096514B1 (de) 1976-03-19
DE2128245A1 (de) 1971-12-30
JPS5421601Y2 (de) 1979-07-31
NL7108852A (de) 1971-12-28
FR2096514A1 (de) 1972-02-18
JPS53106502U (de) 1978-08-26

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