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US2781999A - Turbine construction - Google Patents

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US2781999A
US2781999A US532927A US53292755A US2781999A US 2781999 A US2781999 A US 2781999A US 532927 A US532927 A US 532927A US 53292755 A US53292755 A US 53292755A US 2781999 A US2781999 A US 2781999A
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Prior art keywords
blade holder
rotor
stationary
casing
inner casing
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US532927A
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Brennecke Carl
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Siemens Schuckertwerke AG
Siemens Corp
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Siemens Corp
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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
    • F01D25/265Vertically split casings; Clamping arrangements therefor

Definitions

  • This invention relates to turbines utilizing high temperature motive fluid and more particularly to axial flow steam turbines wherein the outer casings and the inner casings are undivided along their longitudinal axes.
  • Turbines using casings which are axially undivided cannot be assembled in a conventional manner. It is first necessary to assemble the rotor, stationary blade holder and axially undivided inner casing outside of the axially undivided outer casing and then to insert the assembled unit into the outer casing. It is therefore an object of this invention to simplify the assembly of such a turbine by providing a preliminarily-assembled unit which can be easily inserted into the undivided outer casing.
  • a more specific object is to provide a support to which the stationary labyrinth rings may be secured prior to their insertion into the outer casing.
  • the single figure is a longitudinal sectional view of a turbine whose outer casing is undivided axially and which embodies the present invention.
  • the reference character 10 indicates, in its entirety, a typical axial flow turbine having an axially undivided outer casing 11 with an end wall 12 at the high pressure end or right-hand end as viewed in the drawing.
  • the outer casing 11 with the end wall 12 and an end cover 13 secured to the low pressure or left-hand end of the outer casing substantially enclose a rotor component, generally indicated 14 and a stationary blade component, generally indicated 16.
  • the axially undivided outer casing 11 has on the lefthand end an access opening 17 to permit entry of the inner casing component 16 and the rotor component 14.
  • the end cover 13 is connected to the outer casing 11 by any desirable means but, for purposes of illustration, a ring 18 having a plurality of threads 19 on its outer periphery, engaging a plurality of threads 21 on the inner periphery of the outer casing, is used.
  • the cover 13 has an opening 22 permitting a portion 23 of the rotor to extend through the cover after the latter is secured to the casing.
  • the end wall 12 projects radially inwardly toward the rotor but an opening 24 is provided to permit a portion 26 of the rotor to extend through the outer casing.
  • These extended nited States Patent 0 2 rotor portions 23 and 26 are rotatably supported in bearings, not shown, disposed outside of the casing 11, in any well known manner.
  • the rotor component 14 comprises a rotor 27 to which a blade holder 28 is secured by a plurality of radial pins 29 which serve to axially locate the blade holder and to transmit torque therefrom to the rotor.
  • the blade holder 28 supports a plurality of rows of rotating blades 31. Integral with the blade holder 28 is a sealing ring portion 32 disposed to the right of the blade holder 28, as viewed in the drawing.
  • the stationary blade component 16 comprises an axially divided stationary blade holder 40 which supports a plurality of rows of stationary blades 41 designed to cooperate with the rotating blades 31.
  • the top and bottom half of the axially divided stationary blade holder 40 are securely connected together by a shrink ring 39, located at the right-hand end thereof, as viewed in the drawing.
  • the stationary blade holder 40 is also secured, by means to be subsequently described, to an axially undivided inner casing 42.
  • the inner casing 42 is provided at its left-hand end, as viewed in the drawing, with a radial inwardly-extending annular projection 43, against whose inner radial surface the stationary blade holder 40 abuts.
  • a shrink ring 44 may also be mounted, at the left-hand end, on the annular projection 43, thereby providing additional strength.
  • casing 42 and the stationary blade holder 40 is provided for by a plurality of radial pins 46 and a plurality of cooperating sliding blocks 47.
  • the inner casing 42 has, at the right-hand end, an annular projection 48 extending axially to the right.
  • the inner periphery of this annular projection 48 defines the outer periphery of the sealing area 38. Therefore, the annular sealing area 38 is bounded by the outer periphery of the sealing ring portion 32, the inner periphery of the extended annular projection 48 and on the right by the end wall 12 of the outer casing while on the left substantially by a radially outwardly extending projection 37 which functions as a rotating labyrinth seal ring and is an integral part of the blade holder 28.
  • the rotating labyrinth rings 49 and51 are prevented from rotation relative to each other and to the sealing ring portion 32 by a plurality of pins 52 and 53 and aresecured to the sealing ring portion 32 by a locking ring 54.
  • the ring 54 has a pluralityof threads 55 on its inner periphery which engage a plurality of threads 56 on the outer periphery of the sealing ring portion 32.
  • the dowel pins 52 are inserted between the radially.
  • the ring 67 has a plurality of threads 69 on its outer periphery which engage a plurality of mating threads 71 on the inner periphery of the annular projection 48. The ring ,67 bears against the labyrinth ring farthest to the right, as at 68.
  • the above described components are assembled in the following manner: The unit composed of the rotor component 14 and the stationary blade component 16 is assembled prior to insertion in the outer casing 11, the rotating blade holder 28 with its rotating blades 31 being placed on the rotor 27 so as to abut at the shoulder 30.
  • the rotating blade holder 28 is positioned along the rotor 27 by first being disposed along the right hand portion 26 and thereafter moved axially to the left until it abuts the shoulder 30. Since the rotating blade holder 28 is loosely fitted to the rotor 27, any necessary assembly adjustments may be made. Thereafter holes are drilled and reamed for receiving a plurality of radial pins 29 which lock the rotating blade holder 28 to the rotor 27.
  • the two halves of the stationary blade holder 40 are placed in cooperating relation with the rotor component 14 and retained in that relation by the shrink ring 39. Thereafter, the assembled rotor and stationary blade component are positioned in the inner casing 42 and the shrink ring 44 applied.
  • the labyrinth sealing rings are assembled axially as follows:
  • the one piece stationary annular labyrinth ring 60 with its dowel pins 64 is inserted axially into the inner casing 42 through the open right-hand end thereof, the free ends of the pins 64 being received in mating recesses provided in the extended annular shoulders 62, thereby locking the ring 60 against rotation relative to the inner casing 42.
  • the one piece rotating annular labyrinth ring 51 with its dowel pins 52 is next inserted axially and secured to the shoulder 56 by reception of its pins 52 in mating recesses provided in shoulder 56.
  • a ring 26a which may be a portion of an additional sealing ring (not illustrated), may be secured to the rotor portion 26 in any suitable manner, such as by shrinking, threading or pinned thereon.
  • this assembly is placed within the outer casing 11 through the access opening 17 with part of the rotor 26 extending through the outer casing end wall.
  • the inner casing 42 is then secured to the outer casing 11 by radial pins 72.
  • the end cover 13 is assembled to the outer casing 11 and secured by rings 18 and 18a.
  • this invention provides in turbines having axially undivided outer casings a rotor component and an inner casing component, together with their respective labyrinth seals, which may be assembled prior to insertion into the undivided outer casing.
  • An elastic fluid turbine comprising, a rotor, a stationary blade holder which is axially divided, cooperating blading carried by said rotor and said stationary blade holder, an inner casing which is axially undivided enclosing said stationary blade holder, means securing said stationary blade holder to said inner casing, an outer casing which is axially undivided having at one end an access opening to permit entry of said inner casing and at the other end a radially inwardly projecting end wall substantially enclosing said inner casing, means securing said inner casing to said outer casing, a sealing ring portion on said rotor, said inner casing having an annular projection encompassing the said sealing ring portion of said rotor and defining therewith an annular sealing area, and stationary sealing rings distributed along and supported by the annular projection of said inner casing whereby they are disposed within the sealing area.
  • An elastic fluid turbine comprising, a rotor, 21 rotating blade holder, means securing said rotating blade holder to said rotor, a stationary blade holder which is axially divided, cooperating blading carried by said rotating blade holder and said stationary blade holder, an inner casing which is axially undivided enclosing said stationary blade holder, means securing said stationary blade holder to said inner casing, an outer casing which is axially undivided having at one end an access opening to permit entry of said inner casing and at the other end a radially inwardly projecting end wall substantially cnclosing said inner casing, means securing said inner casing to said outer casing, a sealing ring portion on said rotating blade holder adjacent the end wall of said outer casing, said inner casing having an annular projection oncompassing the said sealing ring portion of said rotating blade holder and defining therewith an annular sealing area, stationary sealing rings disposed radially inward distributed along and engaging said annular projection,
  • An elastic fluid turbine comprising, a rotor, a rotating blade holder, means securing said rotating blade holder to said rotor, an annular stationary blade holder divided along its longitudinal axis, cooperating blading carried by said rotating blade holder and said stationary blade holder, an annular inner casing undivided along its longitudinal axis enclosing said stationary blade holder, means securing said stationary blade holder to said inner casing, an outer casing which is axially undivided having at one end an access opening to permit entry of said inner casing and at the other end a radially inwardly projecting end wall substantially enclosing said inner casing, means to secure said inner casing to said outer casing, a sealing ring portion on said rotating blade holder between the blading and the end wall of said outer casing, said inner casing having an annular projection encompassing the said sealing ring portion and defining therewith an annular sealing area, said annular projection having at the end farthest removed from the blades
  • An elastic fluid turbine comprising, a rotor, a rotating blade holder, means securing said rotating blade holder to said rotor, said rotating blade holder carrying a plurality of axially spaced circumferential rows of rotating blades on its outer periphery, an annular stationary blade holder divided along its longitudinal axis, said stationary blade holder carrying a plurality of axially spaced circumferential-rows of stationary blades on its inner periphery cooperating with the rotating blades, a sealing ring portion on said rotating blade holder between the blading and the end wall of said outer casing, a first shrink ring fitted to the end of said stationary divided blade holder adjacent said sealing ring portion for maintaining said divided blade holder assembled, an axially undivided annular inner casing enclosing said stationary blade holder, an axially undivided outer casing having at one end an access opening to permit entry of said inner casing and at the other end a radially inwardly projecting end wall substantially enclo

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

TURBINE CONSTRUCTION Carl Brennecke, Mulheim an der Ruhr Saarn, Germany, assignor to Siemens-Schuckertwerke Aktiengesellschaft, Erlangen, Germany, a corporation of Germany Application September 7, 1955, Serial No. 532,927
Claims priority, application Germany September 24, 1954 4 Claims. (Cl. 253-39) This invention relates to turbines utilizing high temperature motive fluid and more particularly to axial flow steam turbines wherein the outer casings and the inner casings are undivided along their longitudinal axes.
Turbines using casings which are axially undivided cannot be assembled in a conventional manner. It is first necessary to assemble the rotor, stationary blade holder and axially undivided inner casing outside of the axially undivided outer casing and then to insert the assembled unit into the outer casing. It is therefore an object of this invention to simplify the assembly of such a turbine by providing a preliminarily-assembled unit which can be easily inserted into the undivided outer casing.
It is another object of this invention to provide an undivided inner casing adapted to reduce the number of separate parts which must be inserted into the undivided outer casing.
A more specific object is to provide a support to which the stationary labyrinth rings may be secured prior to their insertion into the outer casing.
These and other objects are effected by the invention as will be apparent from the following description taken in connection with the accompanying drawing, forming a part of this application:
In the drawing, the single figure is a longitudinal sectional view of a turbine whose outer casing is undivided axially and which embodies the present invention.
Referring to the drawing, the reference character 10 indicates, in its entirety, a typical axial flow turbine having an axially undivided outer casing 11 with an end wall 12 at the high pressure end or right-hand end as viewed in the drawing. The outer casing 11 with the end wall 12 and an end cover 13 secured to the low pressure or left-hand end of the outer casing substantially enclose a rotor component, generally indicated 14 and a stationary blade component, generally indicated 16.
Only the top half of the turbine 10 has been illustrated but it is to be understood that the bottom half is of identical construction and that in the preferred embodiment the turbine is circular in a plane transverse to that illustrated.
The axially undivided outer casing 11 has on the lefthand end an access opening 17 to permit entry of the inner casing component 16 and the rotor component 14.
The end cover 13 is connected to the outer casing 11 by any desirable means but, for purposes of illustration, a ring 18 having a plurality of threads 19 on its outer periphery, engaging a plurality of threads 21 on the inner periphery of the outer casing, is used. The cover 13 has an opening 22 permitting a portion 23 of the rotor to extend through the cover after the latter is secured to the casing.
At the right-hand side of the outer casing 11, the end wall 12 projects radially inwardly toward the rotor but an opening 24 is provided to permit a portion 26 of the rotor to extend through the outer casing. These extended nited States Patent 0 2 rotor portions 23 and 26 are rotatably supported in bearings, not shown, disposed outside of the casing 11, in any well known manner.
The rotor component 14 comprises a rotor 27 to which a blade holder 28 is secured by a plurality of radial pins 29 which serve to axially locate the blade holder and to transmit torque therefrom to the rotor. The blade holder 28 supports a plurality of rows of rotating blades 31. Integral with the blade holder 28 is a sealing ring portion 32 disposed to the right of the blade holder 28, as viewed in the drawing.
The stationary blade component 16 comprises an axially divided stationary blade holder 40 which supports a plurality of rows of stationary blades 41 designed to cooperate with the rotating blades 31. The top and bottom half of the axially divided stationary blade holder 40 are securely connected together by a shrink ring 39, located at the right-hand end thereof, as viewed in the drawing. The stationary blade holder 40 is also secured, by means to be subsequently described, to an axially undivided inner casing 42. The inner casing 42 is provided at its left-hand end, as viewed in the drawing, with a radial inwardly-extending annular projection 43, against whose inner radial surface the stationary blade holder 40 abuts. A shrink ring 44 may also be mounted, at the left-hand end, on the annular projection 43, thereby providing additional strength. casing 42 and the stationary blade holder 40 is provided for by a plurality of radial pins 46 and a plurality of cooperating sliding blocks 47. a
The inner casing 42 has, at the right-hand end, an annular projection 48 extending axially to the right. The inner periphery of this annular projection 48 defines the outer periphery of the sealing area 38. Therefore, the annular sealing area 38 is bounded by the outer periphery of the sealing ring portion 32, the inner periphery of the extended annular projection 48 and on the right by the end wall 12 of the outer casing while on the left substantially by a radially outwardly extending projection 37 which functions as a rotating labyrinth seal ring and is an integral part of the blade holder 28.
Supported on the sealing ring portion 32 of the rotating blade holder are a plurality of one piece rotating annular labyrinth sealing rings 49 and 51 which extend radially outward and into the sealing area 38. The rotating labyrinth rings 49 and51 are prevented from rotation relative to each other and to the sealing ring portion 32 by a plurality of pins 52 and 53 and aresecured to the sealing ring portion 32 by a locking ring 54. The ring 54 has a pluralityof threads 55 on its inner periphery which engage a plurality of threads 56 on the outer periphery of the sealing ring portion 32. The dowel pins 52 are inserted between the radially. outwardly extending shoulder 56 adjacent the one piece labyrinthsealing ring farthest to the left and dowel pins 53 between adjacent one piece se'aling rings. ring 49 farthest to the right has a radial inwardly extending flange 57 which is forced to abutagainst a shoulder 58 on the sealing ring portion 32. The ring 54 bears against the labyrinth ring farthest to the right, as at 58a, and this force is thus transmitted from one labyrinth ring to another and ultimately, upon expansion of the jection 48 are a plurality of radially inwardly extending Relative expansion between inner.
The labyrinth shoulders 62 and 63 to which are attached the labyrinth rings 60 and 61 by a plurality of dowel pins 64 and 66 and a second locking ring 67. The ring 67 has a plurality of threads 69 on its outer periphery which engage a plurality of mating threads 71 on the inner periphery of the annular projection 48. The ring ,67 bears against the labyrinth ring farthest to the right, as at 68.
The above described components are assembled in the following manner: The unit composed of the rotor component 14 and the stationary blade component 16 is assembled prior to insertion in the outer casing 11, the rotating blade holder 28 with its rotating blades 31 being placed on the rotor 27 so as to abut at the shoulder 30. The rotating blade holder 28 is positioned along the rotor 27 by first being disposed along the right hand portion 26 and thereafter moved axially to the left until it abuts the shoulder 30. Since the rotating blade holder 28 is loosely fitted to the rotor 27, any necessary assembly adjustments may be made. Thereafter holes are drilled and reamed for receiving a plurality of radial pins 29 which lock the rotating blade holder 28 to the rotor 27.
The two halves of the stationary blade holder 40 are placed in cooperating relation with the rotor component 14 and retained in that relation by the shrink ring 39. Thereafter, the assembled rotor and stationary blade component are positioned in the inner casing 42 and the shrink ring 44 applied.
The labyrinth sealing rings are assembled axially as follows: The one piece stationary annular labyrinth ring 60 with its dowel pins 64 is inserted axially into the inner casing 42 through the open right-hand end thereof, the free ends of the pins 64 being received in mating recesses provided in the extended annular shoulders 62, thereby locking the ring 60 against rotation relative to the inner casing 42. The one piece rotating annular labyrinth ring 51 with its dowel pins 52 is next inserted axially and secured to the shoulder 56 by reception of its pins 52 in mating recesses provided in shoulder 56. By alternately assembling a stationary and then a rotating ring any desired number of such rings can be assembled. After the last sealing ring has been placed in position, the threaded locking rings 54 and 67 are assembled. Thereafter a ring 26a, which may be a portion of an additional sealing ring (not illustrated), may be secured to the rotor portion 26 in any suitable manner, such as by shrinking, threading or pinned thereon.
After the rotor component and the stationary component have been assembled in the manner described above, this assembly is placed within the outer casing 11 through the access opening 17 with part of the rotor 26 extending through the outer casing end wall. The inner casing 42 is then secured to the outer casing 11 by radial pins 72. Thereafter the end cover 13 is assembled to the outer casing 11 and secured by rings 18 and 18a.
From the foregoing it will be seen that this invention provides in turbines having axially undivided outer casings a rotor component and an inner casing component, together with their respective labyrinth seals, which may be assembled prior to insertion into the undivided outer casing.
While the invention has been shown in but one form, it will be obvious to those skilled in the art that it is not so limited, but is susceptible of various changes and modifications without departing from the spirit thereof.
What is claimed is:
1. An elastic fluid turbine comprising, a rotor, a stationary blade holder which is axially divided, cooperating blading carried by said rotor and said stationary blade holder, an inner casing which is axially undivided enclosing said stationary blade holder, means securing said stationary blade holder to said inner casing, an outer casing which is axially undivided having at one end an access opening to permit entry of said inner casing and at the other end a radially inwardly projecting end wall substantially enclosing said inner casing, means securing said inner casing to said outer casing, a sealing ring portion on said rotor, said inner casing having an annular projection encompassing the said sealing ring portion of said rotor and defining therewith an annular sealing area, and stationary sealing rings distributed along and supported by the annular projection of said inner casing whereby they are disposed within the sealing area.
2. An elastic fluid turbine comprising, a rotor, 21 rotating blade holder, means securing said rotating blade holder to said rotor, a stationary blade holder which is axially divided, cooperating blading carried by said rotating blade holder and said stationary blade holder, an inner casing which is axially undivided enclosing said stationary blade holder, means securing said stationary blade holder to said inner casing, an outer casing which is axially undivided having at one end an access opening to permit entry of said inner casing and at the other end a radially inwardly projecting end wall substantially cnclosing said inner casing, means securing said inner casing to said outer casing, a sealing ring portion on said rotating blade holder adjacent the end wall of said outer casing, said inner casing having an annular projection oncompassing the said sealing ring portion of said rotating blade holder and defining therewith an annular sealing area, stationary sealing rings disposed radially inward distributed along and engaging said annular projection, and means for securing said stationary sealing rings to said annular projection.
3. An elastic fluid turbine comprising, a rotor, a rotating blade holder, means securing said rotating blade holder to said rotor, an annular stationary blade holder divided along its longitudinal axis, cooperating blading carried by said rotating blade holder and said stationary blade holder, an annular inner casing undivided along its longitudinal axis enclosing said stationary blade holder, means securing said stationary blade holder to said inner casing, an outer casing which is axially undivided having at one end an access opening to permit entry of said inner casing and at the other end a radially inwardly projecting end wall substantially enclosing said inner casing, means to secure said inner casing to said outer casing, a sealing ring portion on said rotating blade holder between the blading and the end wall of said outer casing, said inner casing having an annular projection encompassing the said sealing ring portion and defining therewith an annular sealing area, said annular projection having at the end farthest removed from the blades a plurality of threads on its inner periphery, stationary labyrinth sealing rings engaging said annular projection between the bladed end and the threaded end of said inner easing, a first ring having a plurality of threads on its outer periphery engaging said threads on the inner periphery of said annular projection whereby said stationary labyrinth sealing rings are secured to said inner casing, rotating labyrinth sealing rings distributed along and supported by said sealing ring portion, said sealing ring portion having threads on its outer periphery at the end farthest removed from the blades, and a second ring having threads on its inner periphery engaging the threads on the outer periphery of said sealing ring portion whereby said rotating labyrinth rings are secured to said rotor.
4. An elastic fluid turbine comprising, a rotor, a rotating blade holder, means securing said rotating blade holder to said rotor, said rotating blade holder carrying a plurality of axially spaced circumferential rows of rotating blades on its outer periphery, an annular stationary blade holder divided along its longitudinal axis, said stationary blade holder carrying a plurality of axially spaced circumferential-rows of stationary blades on its inner periphery cooperating with the rotating blades, a sealing ring portion on said rotating blade holder between the blading and the end wall of said outer casing, a first shrink ring fitted to the end of said stationary divided blade holder adjacent said sealing ring portion for maintaining said divided blade holder assembled, an axially undivided annular inner casing enclosing said stationary blade holder, an axially undivided outer casing having at one end an access opening to permit entry of said inner casing and at the other end a radially inwardly projecting end wall substantially enclosing said inner casing, means securing said inner casing to said outer casing, said inner casing being spaced from said stationary blade holder throughout a major portion of its lengthand being provided at the end farthest removed from said sealing ring portion with a radially inward annular projection engaging said stationary blade holder, a second shrink ring fitted to said annular projection, additional connecting means between said stationary blade holder and said inner casing providing for relative expansion, said inner casing having a labyrinth sealing ring support structure projecting axially therefrom and encompassing the said sealing ring portion and defining therewith an annular sealing area, said stationary sealing ring support having a plurality of threads on the inner periphery at the end farthest removed from the blades, stationary labyrinth sealing rings supported between the bladed end and the threaded end of said stationary sealing ring support, a locking ring having a plurality of threads on its outer periphery engaging the threads on the inner periphery of said labyrinth sealing ring support, thereby securing said stationary labyrinth sealing rings to said stationary sealing ring support, rotating labyrinth sealing rings distributed along and supported by said sealing ring portion, said sealing ring portion having a plurality of threads on its outer periphery at the end farthest removed from the blades, and a second ring having a plurality of threads on its inner periphery engaging the threads on the outer periphery of said sealing ring portion, thereby securing said rotating labyrinth rings to said sealing ring portion.
No references cited.
US532927A 1954-09-24 1955-09-07 Turbine construction Expired - Lifetime US2781999A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3043559A (en) * 1954-10-22 1962-07-10 Maschf Augsburg Nuernberg Ag Gas turbine
US4648790A (en) * 1983-06-29 1987-03-10 Bbc Brown, Boveri & Company, Limited Axial turbine for exhaust gas turbochargers
US20140178183A1 (en) * 2011-09-28 2014-06-26 Mitsubishi Heavy Industries Compressor Corporation Rotation mechanism and internal unit of rotation mechanism

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3043559A (en) * 1954-10-22 1962-07-10 Maschf Augsburg Nuernberg Ag Gas turbine
US4648790A (en) * 1983-06-29 1987-03-10 Bbc Brown, Boveri & Company, Limited Axial turbine for exhaust gas turbochargers
US20140178183A1 (en) * 2011-09-28 2014-06-26 Mitsubishi Heavy Industries Compressor Corporation Rotation mechanism and internal unit of rotation mechanism
US10077783B2 (en) * 2011-09-28 2018-09-18 Mitsubishi Heavy Industries Compressor Corporation Rotation mechanism and internal unit of rotation mechanism

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