US2266613A - Double shell elastic fluid turbine - Google Patents

Double shell elastic fluid turbine Download PDF

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Publication number
US2266613A
US2266613A US342980A US34298040A US2266613A US 2266613 A US2266613 A US 2266613A US 342980 A US342980 A US 342980A US 34298040 A US34298040 A US 34298040A US 2266613 A US2266613 A US 2266613A
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stem
casing
cylinder
shell
elastic fluid
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US342980A
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Leland A Richards
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General Electric Co
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General Electric Co
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    • 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
    • F01D25/26Double casings; Measures against temperature strain in casings
    • 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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/047Nozzle boxes
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/57Distinct end coupler
    • Y10T403/5761Interrupted periphery, e.g., split or segmental, etc.
    • Y10T403/5766Axially divided segments

Definitions

  • the present invention relates to double shell elastic fluid turbines such as are used for operation with yelastic uid at an inlet temperature of the order of 900 F. and above.
  • it is customary to provide an inner shell at least with regard to some of the high pressure stages and to connect the space formed between the inner and outer shells to a low pressure stage at which the temperature of the fluid is about one half'of the inlet temperature.
  • the temperature drop across the .inner and outer casing is about one half the total
  • a more specific object of my invention is to provide an improved coupling ⁇ and sealing arrangement for valve-stems whereby such stems are effectively sealed and may be readily assembled and at least partly dismantled without requiring complete dismantling of a turbine casing.
  • FIG. 1 illustrates a sectional view of a double shell turbine embodying my invention
  • Fig. 2 is a section along line 2-2 of Fig. 1
  • Fig. 3 is an enlarged view of a detail of Figs. 1 and 2.
  • the arrangement comprises a rotor having a shaft I and a plurality ofbucket wheels II, I2,
  • the inner shell I4 includes an inner ⁇ shell I4 enclosing the ⁇ high pressure portion of the rotor and an outer shell I5 enclosing the inner shell I4 Yand also the low pressure portion of th'e rotor.
  • the inner shell I4 has an inlet portion forming a valve chest I6 from which elastic fluid may be conducted through a nozzle plate I1 to the first bucket Wheel II.
  • This first stage wheel in the presentI instance has two rows of buckets and elastic fluid discharged from the first row is conducted to the second row by a diaphragm I8 supported on the shell I6.
  • the latter also serves as a support for other diaphragms I9, 20 for conducting y conduit 36 projects into a cylindrical opening or.
  • the diaphragms are sealed to the shaft by means of suitable known type labyrinth packings 25 to prevent leakage of fluid along the shaft between successive stages.
  • End portions of the inner and outer shells are sealed to the shaft I0 by labyrinth packings '26 and 21 respectively to prevent leakage of fluid lalong the shaft to the f atmosphere.
  • the inner shell I4 has brackets 28 guided in slots of the outer shell. Side portions of the inner shell have brackets 29 engaging and supported in recesses of the outer shell.
  • the vinlet chest I 6 is integrally formed with the inner shell I4.
  • the control of elastic fluid from the chest to the first stage nozzle plate I1 is accomplished by four valves 30, 3
  • Each of'these valves is arranged in cooperative relation with a valve seat 34 formed on the chest to control the flow of fluid to one of four sections 35 of the first stage nozzle blade.
  • the arrangement constitutes a partial admission arrangement whereby the flow of fluid to several sections of the first stage is controlled.
  • Elastic fluid is conducte to the chest from a source of fiuid by a cond 36 secured to the outer casing and sealed to an opening in the chest. More specifically the conduit is supported by and fused to a ring 3l fastened to the outer shell by bolts 38.
  • the ring has an inner conical projection 39 with an edge secured to the conduit 36 by a weld 40.
  • the conical projection 39 forms a thin Wall, thus reducing its stiffness to a 'minimum to permit slight movement of the conduit 36 relative to the outer shell.
  • Each valve 30 to 33 and 23 has a stem consisting of two parts, a lower or inner stem 42 securely fastened to the valve disk and an outer stem portion 43 in substantial alignment with the inner stem and connected to the inner stem 42 by a coupling device 44.
  • the inner stem is guided and sealed to the inner shell by aligned sleeves 45 and 46 held within a bushing 41, which latter is screwed into an opening 43 of the inner shell and has an upper portion concentrically spaced from a bore in the outer shell l to permit relative movement between them.
  • a bushing 41 which latter is screwed into an opening 43 of the inner shell and has an upper portion concentrically spaced from a bore in the outer shell l to permit relative movement between them.
  • two sleeves 45, 46 are provided which are inserted from opposite ends into the bushing 41.
  • Each sleeve has a anged end portion 49 seated in a recessed end portion 56 of the bushing 41 .and in the present instance held in position by peening over the end portions 50 of the bushing 41.
  • the upper stem 43 is similarly guided by guide and packing sleeves 5l and 52 securely held in a iianged cylinder 53. The latter projects into and is secured to the upper end of a clamp and guide casing 54 which has a lower iianged portion fastened to the outer shell by bolts 55.
  • the clamp or coupling device 44 for connecting the lower and upper stems comprises a clamping cylinder having two halves 56 and 51 engaging each other along a plane, through the center oi the stems.
  • the lower portion of the cylinder 56, 51 has an inwardly turned ilange 58 projecting into an inner groove 59 in the upper end portion of the lower stem 42 and an outwardly turned flange 60 projecting towards the wall 'of the clamp casing 54.
  • the cylinder 56, 51 is surrounded by another cylinder 6I resting on the outer ilange 60.
  • are secured together by a pin 62.
  • diametrically opposite portions of the cylinder 54 are provided with plugs or closing members 63 and 64 respectively. These plugs ordinarily prevent sidewise movement of the pin 62 and upon remoyal of the plugs 63, 64 the pin 62 may be driven'out whereby the upper stem may be lifted and removed from the lower stem.
  • the groove 59 in the upper part of the lower stem 42 denes shoulders engaged by the annular yprojectiion 58 of the cylinder 56, 51.
  • An end portion 65 of the upper stem rests on the annular flange 58 acting as a support for the lower stem and the valve disk attached thereto.
  • the end portion 65 and the necked-in portion of the lower stem 42 have slight radial clearance with the adjacent ⁇ portions of the cylinder 56, 51 and substantially tight t in axial direction, thus permitting angular displacement between the lower and upper stems 42, 43 respectively but substantially connect the clamping device with the upper stem 43. Thereupon the plugs are screwed into the clamp casing 54.
  • the by-pass valve 23 projects through and has a lower stem 66 and an upper stem 61 connected by a coupling device 68 corresponding to the coupling device 44 for the inlet valves 30 to 33. 'Ihe lower stem projects through a bushing 69 corresponding to the bushing 41 for the valves 30 to 33.
  • the upper ends of the inlet valves and the by-pass valve may be controlled in known manner by any suitable control mechanism, not shown.
  • the clamping device for connecting the valve stems broadly constitutes an arrangement for connecting two substantially aligned stems or shafts within a casing whereby one stem may be connected to and disconnected from the other stem without requiring removal of the other stem and the clamping device from the casing. 'I'he only element of the clamping device that is to be removed is the crosspin projecting through openings in the split cylinder, the holding cylinder, and one of the stems. The other stem forms a shoulder engaging a projection on the split cylinder.
  • upper stem being slidable into the split cylinder, a holding cylinder surrounding the split cylinder and engaging the outer ange, and a pin connecting the upper stem to the split cylinder and the'outer cylinder, disassembly of the pin permitting removal of the upper stem without necessitating disassembly of the holding and split cylinders.
  • a casing having an opening, two stems having aligned end portions enclosed within the casing, and coupling means enclosed within the' 5 casing to connect the stems and to permit dismantling of one of them without requiring dismantling of the other and the casing, said means comprising a split cylinder having an inturned ilange engaging a shoulder formed on one of the A10

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Valve Housings (AREA)

Description

Dec. 16,` 1941. L. A. RICHARDS DOUBLE SHELL ELASTIC FLUID TURBINE Filed June 28, 1940 fr mn Oa P .Eh O nMw WRA HAE@ fw e L yw b,
Patented Dec. 16, 1941 DOUBLE .SHELL ELAs'rIc FLUID TURBINE Leland A. Richards, Schenectady, N. Y., assignor to General Electric Company, acorporation of Application June 28, 1940, ySerial No. 342,980
3 Claims.
The present invention relates to double shell elastic fluid turbines such as are used for operation with yelastic uid at an inlet temperature of the order of 900 F. and above. In such arrangements it is customary to provide an inner shell at least with regard to some of the high pressure stages and to connect the space formed between the inner and outer shells to a low pressure stage at which the temperature of the fluid is about one half'of the inlet temperature. In this manner the temperature drop across the .inner and outer casing is about one half the total A more specific object of my invention is to provide an improved coupling `and sealing arrangement for valve-stems whereby such stems are effectively sealed and may be readily assembled and at least partly dismantled without requiring complete dismantling of a turbine casing.
For a consideration of what I believe to be novel and my invention, attention is directed to the following description and the claims appended thereto inl connection with the accompanying l drawing.
In the drawing Fig. 1 illustrates a sectional view of a double shell turbine embodying my invention; Fig. 2 is a section along line 2-2 of Fig. 1; and Fig. 3 is an enlarged view of a detail of Figs. 1 and 2.
The arrangement comprises a rotor having a shaft I and a plurality ofbucket wheels II, I2,
- I3 with disks integrally formed with the shaft I 0. The rotor is enclosed within a casing which..y
includes an inner `shell I4 enclosing the `high pressure portion of the rotor and an outer shell I5 enclosing the inner shell I4 Yand also the low pressure portion of th'e rotor. The inner shell I4 has an inlet portion forming a valve chest I6 from which elastic fluid may be conducted through a nozzle plate I1 to the first bucket Wheel II. -This first stage wheel in the presentI instance has two rows of buckets and elastic fluid discharged from the first row is conducted to the second row by a diaphragm I8 supported on the shell I6. The latter also serves as a support for other diaphragms I9, 20 for conducting y conduit 36 projects into a cylindrical opening or. I
elastic fluid to the stages I2, I3, etc.
Not all of the uid discharged from the double row first Istage wheel II isv conducted through the diaphragm I9 to the second bucket wheel I2 but part of the fluid discharged from the first or high pressure stage may be bypassed through a channel 2l formed by the inner shell to a low pressure, in the present instance the third stage diaphragm 22. The bypassing of fluid through the `channel 2| is controlled by a valve 23 havinga movable element in cooperative relation with a valve seat 24 formed on or secured to the inner shell I4. Details of the sealing arrangement and the design ofthe valve 23 will be described hereinafter.
The diaphragms are sealed to the shaft by means of suitable known type labyrinth packings 25 to prevent leakage of fluid along the shaft between successive stages. End portions of the inner and outer shells are sealed to the shaft I0 by labyrinth packings '26 and 21 respectively to prevent leakage of fluid lalong the shaft to the f atmosphere. The inner shell I4 has brackets 28 guided in slots of the outer shell. Side portions of the inner shell have brackets 29 engaging and supported in recesses of the outer shell.
The vinlet chest I 6 is integrally formed with the inner shell I4. The control of elastic fluid from the chest to the first stage nozzle plate I1 is accomplished by four valves 30, 3|, 32 and 33. Each of'these valves is arranged in cooperative relation with a valve seat 34 formed on the chest to control the flow of fluid to one of four sections 35 of the first stage nozzle blade. Thus the arrangement constitutes a partial admission arrangement whereby the flow of fluid to several sections of the first stage is controlled. Elastic fluid is conducte to the chest from a source of fiuid by a cond 36 secured to the outer casing and sealed to an opening in the chest. More specifically the conduit is supported by and fused to a ring 3l fastened to the outer shell by bolts 38. The ring has an inner conical projection 39 with an edge secured to the conduit 36 by a weld 40. The conical projection 39 forms a thin Wall, thus reducing its stiffness to a 'minimum to permit slight movement of the conduit 36 relative to the outer shell. An inner end portion of the bore in the chest I6 and is sealed thereto by a lknown type of packing 4I comprising a stack of a pluralitypf pairs of rings adjacent each other with one ring of each pair engaging'the wall of the chest and forming a clearance with the conduit and the other ring of each pair engaging the conduit and forming a clearance with the wall or bore in the chest.
Each valve 30 to 33 and 23 has a stem consisting of two parts, a lower or inner stem 42 securely fastened to the valve disk and an outer stem portion 43 in substantial alignment with the inner stem and connected to the inner stem 42 by a coupling device 44. The inner stem is guided and sealed to the inner shell by aligned sleeves 45 and 46 held within a bushing 41, which latter is screwed into an opening 43 of the inner shell and has an upper portion concentrically spaced from a bore in the outer shell l to permit relative movement between them. As the inner stem 42 is of considerable length and in view of the diiiiculty to form such long packing and guide sleeves, two sleeves 45, 46 are provided which are inserted from opposite ends into the bushing 41. Each sleeve has a anged end portion 49 seated in a recessed end portion 56 of the bushing 41 .and in the present instance held in position by peening over the end portions 50 of the bushing 41. The upper stem 43 is similarly guided by guide and packing sleeves 5l and 52 securely held in a iianged cylinder 53. The latter projects into and is secured to the upper end of a clamp and guide casing 54 which has a lower iianged portion fastened to the outer shell by bolts 55. The clamp or coupling device 44 for connecting the lower and upper stems comprises a clamping cylinder having two halves 56 and 51 engaging each other along a plane, through the center oi the stems. The lower portion of the cylinder 56, 51 has an inwardly turned ilange 58 projecting into an inner groove 59 in the upper end portion of the lower stem 42 and an outwardly turned flange 60 projecting towards the wall 'of the clamp casing 54. The cylinder 56, 51 is surrounded by another cylinder 6I resting on the outer ilange 60. The cylinder 56, 51 andthe upper stem 43 and the cylinder 6| are secured together by a pin 62. In
orderI to permit dismantling of the clamping de' vice, diametrically opposite portions of the cylinder 54 are provided with plugs or closing members 63 and 64 respectively. These plugs ordinarily prevent sidewise movement of the pin 62 and upon remoyal of the plugs 63, 64 the pin 62 may be driven'out whereby the upper stem may be lifted and removed from the lower stem.
The groove 59 in the upper part of the lower stem 42 denes shoulders engaged by the annular yprojectiion 58 of the cylinder 56, 51. An end portion 65 of the upper stem rests on the annular flange 58 acting as a support for the lower stem and the valve disk attached thereto. The end portion 65 and the necked-in portion of the lower stem 42 have slight radial clearance with the adjacent `portions of the cylinder 56, 51 and substantially tight t in axial direction, thus permitting angular displacement between the lower and upper stems 42, 43 respectively but substantially connect the clamping device with the upper stem 43. Thereupon the plugs are screwed into the clamp casing 54.
For the purpose of dismantling. as pointed out above, the plugs are removed and the pin 82 is driven out of the clamping device. Upon removal of the bolts 55 the clamp casing together with the upper stem may be lifted and removed from the lower stem and the clamping device. Thus, with this improved coupling device it is no longer necessary completely to disassemble the entire valve arrangement to permit dismantling of the outer turbine casing. This is important in an arrangement as in the present instance in which the valve and the valve chest are associated with the inner shell of the turbine.
The by-pass valve 23 projects through and has a lower stem 66 and an upper stem 61 connected by a coupling device 68 corresponding to the coupling device 44 for the inlet valves 30 to 33. 'Ihe lower stem projects through a bushing 69 corresponding to the bushing 41 for the valves 30 to 33. The upper ends of the inlet valves and the by-pass valve may be controlled in known manner by any suitable control mechanism, not shown.
The clamping device for connecting the valve stems broadly constitutes an arrangement for connecting two substantially aligned stems or shafts within a casing whereby one stem may be connected to and disconnected from the other stem without requiring removal of the other stem and the clamping device from the casing. 'I'he only element of the clamping device that is to be removed is the crosspin projecting through openings in the split cylinder, the holding cylinder, and one of the stems. The other stem forms a shoulder engaging a projection on the split cylinder.
Having described the method of operation of my invention, together with the apparatus which I now consider to represent the best embodiment thereof, I desire to have it understood that the apparatus shown is only illustrative and that the invention may be carried out by other means.
, the recessed end portion of the lower stem, the
upper stem being slidable into the split cylinder, a holding cylinder surrounding the split cylinder and engaging the outer ange, and a pin connecting the upper stem to the split cylinder and the'outer cylinder, disassembly of the pin permitting removal of the upper stem without necessitating disassembly of the holding and split cylinders.
2. A casing, two stems having aligned end portions enclosed within the casing, and means enclosed within the casing to connect the stems and ,to permit dismantling of one of them without requiring dismantling of the other and the casing, said means comprising a split cylinder havthe flanged cylinder 53 are nsertedinto and se cured to the clamp casing 54 by inserting the holding pin 62 ,through the plug openings :to
ing an inturned flange engaging a shoulder formed on one of the stems and forming an opening for receiving the other stem, a holding cylinder surrounding the split cylinder, a. crosspin securing the other stem to the split cylinder and to the holding cylinder, and closing members in the casing which upon removal permit insertion and removal of the pin.
3. A casing having an opening, two stems having aligned end portions enclosed within the casing, and coupling means enclosed within the' 5 casing to connect the stems and to permit dismantling of one of them without requiring dismantling of the other and the casing, said means comprising a split cylinder having an inturned ilange engaging a shoulder formed on one of the A10
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2619798A (en) * 1943-12-23 1952-12-02 Strub Rene Semiclosed circuit type gas turbine plant having extraction controlled by circuit turbine governor
DE1085539B (en) * 1952-01-22 1960-07-21 Siemens Ag High pressure overpressure turbine
DE1140947B (en) * 1954-04-28 1962-12-13 Siemens Ag Steam turbine with pot housing, multi-stage guide vane carrier and with holding body for this

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2619798A (en) * 1943-12-23 1952-12-02 Strub Rene Semiclosed circuit type gas turbine plant having extraction controlled by circuit turbine governor
DE1085539B (en) * 1952-01-22 1960-07-21 Siemens Ag High pressure overpressure turbine
DE1140947B (en) * 1954-04-28 1962-12-13 Siemens Ag Steam turbine with pot housing, multi-stage guide vane carrier and with holding body for this

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