US2801074A - Blade retaining means - Google Patents

Blade retaining means Download PDF

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US2801074A
US2801074A US312540A US31254052A US2801074A US 2801074 A US2801074 A US 2801074A US 312540 A US312540 A US 312540A US 31254052 A US31254052 A US 31254052A US 2801074 A US2801074 A US 2801074A
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blade
disc
pin
slot
root
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US312540A
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William H Brown
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Raytheon Technologies Corp
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United Aircraft 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32Locking, e.g. by final locking blades or keys
    • F01D5/323Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49321Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Definitions

  • This invention relates to a device for locking blades in position in a supporting disc and is especially adapted for use with axial flow compressors or turbines.
  • the rotor for a compressor or turbine is generally made up of one or more supporting discs each having a row of radially extending blades with the roots of the blades fitting in axially extending slots provided in the disc.
  • the blade root is usually held in the slot by a blade lock which is preferably so constructed that removal of the blade from the disc will not necessitate damaging of either the blade or the disc.
  • the copending Affin application Serial No. 153,985, filed April 4, 1950, now Patent No. 2,686,656, having the same assignee as this application has a blade lock in the form of a strip extending from end to end of the slot that receives the blade root with notches therein which engage projecting ribs on the underside of the blade root and with tabs bent over at each end to engage the sides of the disc.
  • Blades have been locked in a disc by forming integral tabs on opposite ends of the blade root with one of the tabs in such a position that the blade root may be inserted in the properly formed slot in the disc and the tab subsequently bent down against the side of the disc.
  • the blade root is made more difficult to machine and in many cases the material of the blade does not bend readily and very frequently the tab breaks ofi so that the blade must be scrapped. This is especially true in the event of removal and insertion of the blade since the tab frequently cannot be rebent successfully.
  • An object of this invention is to permit the removal or installation of a blade from one side of the supporting disc while said supporting disc is mounted.
  • Another object of this invention is to eliminate the necessity for a bent tab to project over either the blade root or the side of the supporting disc to hold said blade in place.
  • the bent tab is merely used to prevent the locking member from rotating.
  • a further object of this invention is to provide a looking member which is held in position by a small washer having tabs and in which the centrifugal effect of the disc tends to move the tab cooperating with said locking member in a locking direction. This makes the part which needs to be replaced, if a tab breaks in assembling or disassembling a blade, a very small one.
  • Another object of this invention is to provide a locking member which is locked from the side of the supporting disc from which the blade is inserted. As can be seen from the locking means of the blades enumerated above, it is necessary to lock said means from the side of the supporting disc opposite that from which the blade is inserted.
  • Fig. 1 is an exploded perspective view of a section of the supporting disc, a section of the blade including the blade root, the locking member, and the holding member. The locking member is shown in its locked position if mounted.
  • Fig. 2 is a axial sectional view on a radial plane through the bottom of a blade root and the bottom of a slot in a disc showing the locking member and its holding mem her in locked position.
  • Fig. 3 is a rear end view taken on the line 3-3 of Fig. 2.
  • Fig. 4 is a front end view taken along the line 44 of Fig. 2.
  • the supporting disc 2 has a plurality of slots 4 in its periphery to receive the similarly formed roots 6 of the blades 8.
  • the particular shape of the blade root 6 or of the similarly shaped slot 4 for holding the blade from moving radially with respect to the slot is not critical, and for the purpose of the present invention a slot is shown having a series of ridges 10 extending along the sides of the slot. These ridges extend from the bottom of the slot to the outer periphery of the disc.
  • the blade root is similar in shape having ridges 3, which when the blade root is assembled, slide between the ridges 10 of the disc.
  • the blade locking member 12 is in a form of a rotatable or angularly turnable pin, or rod, 14 having a head at each end.
  • a rear head 16 is constructed and arranged to engage an area of both the side of the blade root and the side of the supporting disc with which it cooperates in all rotative positions.
  • a front head 18 is constructed and arranged to engage a maximum area of both the other side of the blade root and the other side of the supporting disc in one rotative or angular position, referred to as the locked position and not to engage any portion of the supporting disc in another rotative or angular position 180 degreees from the last mentioned position, referred to as the unlocked position.
  • the length of pin 14 between the inside face 15 of the front head 18 and the inside face 1'7 of the rear head 16 is equal to the width of the disc 2 and blade 8 at this point.
  • the rear head 16 is formed at one end of pin 14- of two integral circular members having different size diameters.
  • the outside circular member 2% of said rear head 16 is formed of a large diameter having a notch 22 therethrough on the outer periphery thereof for a purpose to be hereinafter described.
  • the inside circular member 24 of said rear head 16 is formed of a reduced diameter to receive a holding member or locking means 26.
  • the diameter of the inner circular member 24 is of such a size that when mounted it covers portions of both the blade root and the cooperating slot in the supporting disc.
  • Holding member 26 consists of a Washer member 28 having two tabs 36 and 32, extending from the outer periphery thereof 180 degrees apart. ⁇ Vuile these tabs are placed apart at an angle of degrees it is to be understood that they may be placed at other degrees of angularity.
  • the front head 18 is formed at the other end of pin 14.
  • This head comprises a member having one half thereof semicircular in shape as at 34 and the other half W a 3 shaped so as to slide through the opening formed at the bottom of a slot 4 of supporting disc 2.
  • this other half is formed of three sides 36, 38 and 40, the middle side of the threesides, side 38, being located tangent to the outer periphery of the pin 14 and of a length approximately equal to the diameter of pin 14.
  • This side 33 in the unlocked position of locking member 12 lies in a plane with the bottom 39 of slot 4- ing portions of the root and slot adjacent the bottom of the slot spaced apart in a direction at right angles to the axis of the disc far enough to receive the pin portion of the'locking member and topermit it to turn in the groove.
  • a holding member 26 Before the. mounting of a blade having a locking means such as disclosed herein a holding member 26 has one tab bent so that it extends at an angle of approximately 90 degrees from the plane of the washer portion 28 and the other tab bent so that it extends at an angle of approximately 90 degrees from the plane of the washer member 28 in a direction opposite to that of the other tab (see dotted tab 32 in Fig. 2); In assembling, the holding member 26 is then placed over front head 18 of a blade locking member 12, moved along pin 14, and fitted over the reduced diameter of the inside circular member ,24
  • a supporting disc having an axially extending slot in its periphery, said slot having a bottom, a blade having a root fitting in and engaging in said slot said root having a bottom, said slot and root having interengaging means retaining the blade against radial outward movement relative to the disc, said root and slot having cooperating portions adjacent the bottom spaced apart in a direction at right angles to the axis of the disc to define an axial groove between the root and slot, and means for retaining said blade root in axial position in the slot including a rotatable pin extending through the groove adjacent the bottom of the rooh'said pin having a head at each end, one head being transversely larger than the pin so that it engages an area of both the side 1 7 of the blade root and the side of the supporting disc with locking member and holding member are inserted into a slot in the disc.
  • the locking member When the assembly is fully inserted, with face 17 of rear head 16 against the rear side of the blade' root and disc, the locking member is rotated through 180 degrees to the locked position. The locking member is in its fully locked position when the notch 22 is facing directly downward in this arrangement. This provides a means of visual inspection from the one side of the locking member to determine if the opposite side,
  • the tabs 36 and 32 may be placed in varying degrees of angulan'ty from each other.
  • heads of various other shapes which will either permit the blade and locking member to be inserted in the supporting disc together or permit the locking member to be inserted in the supporting disc wtih the blade 7 his also noted here that locking members may be formed being thereafter inserted.
  • These heads may also be shaped so that they will be moved from an unlocked to a locked position in a varying number of degrees.
  • the type of locking means disclosed in this specification is adapted particularly to installations where one side of the blade and supporting disc is inaccessible when mounted due to an engine part such as indicated at 51L
  • Such an arrangement is shown for example in 'Rubbra 2,594,808 (Fig. 2).
  • Fig. 2 the blade 8 can be removed and replaced from the one side without having to remove the entire supporting disc assembly from the engine. This is advantageous in the field where a minimum of tools are available and the need has been found to replace a blade.
  • a supporting disc having. axially extending slots in its periphery, a number of blades, each blade having a root fitting in and engaged in one of said slots of said disc, each root and the cooperating slot shaving adjacent portions spaced apart radially and forming therebetween an axially extending groove, and means for retaining each of said blade roots in axial'position in its slot including a rotatable pin in said groove having a head at each end, one head being transversely larger-than the pin and engaging an area of both the side of the blade root and the side of the'supporting disc with which it cooperates in all rotative positions, the other head being eccentric to the pin and projecting beyond the pin surface except on one side thereof which is tangential to the surface of the pin and being smaller than the'slot in the disc so that in one angular position it will permit said root to pass through.
  • said slot and in another angular
  • a rotor including a disc having axially extending slots in its periphery, a number of blades having roots,
  • a rotatable pin extending' through' said passageway, said pin having a head at each end, the head at one end being larger than the passageway in transverse section to overlap a part of the blade root and a part of the disc, the head at the other end being smaller in transverse section than the disc slot to' overlap a part of the blade root only in one position of the pin, said second named 'head being eccentrically arranged on the pin to overlap both a part of the blade root and a part of the disc in another angular position of said'pin, and pin locking means engaging said pin and for locking said pin against rotation in the passageway.
  • a rotor including a disc having an axially extending slot in its periphery, a blade having a root, with said root fitting in and engaged in said slot, the cooperating slot and blade root having means retaining the blade'against radial outward movement relative to the disc and 'said.
  • a rotatable pin extending through said passageway, said pin having a head at each end, the head at one end being smaller in transverse section than said slot and eccentric to the axis of the pin to overlap only a portion of the blade root in one angular position of the pin and to overlap a part of the blade root and also a part of the disc at another 5 angular position of said pin, the head at the other end of the pin being larger in transverse section than the passageway to overlap both a part of the blade root and a part of the disc at least in said another angular position of said pin, and pin locking means engaging said pin for 10 looking said pin against rotation in the passageway;

Description

July 30, 1957 W. H. BROWN BLADE RETAINING MEANS Filed Oct. .1, 1952 INVENT WILLIAM H. ER
United States Patent BLADE RETAINTNG MEANS William H. Brown, Manchester, Conn, assignor to United Aircraft Corporation, East Hartford, Conn, 21 corporation of Delaware Application October 1, 1952, Serial No. 312,540
4 Claims. (Cl. 253- l7) This invention relates to a device for locking blades in position in a supporting disc and is especially adapted for use with axial flow compressors or turbines.
The rotor for a compressor or turbine is generally made up of one or more supporting discs each having a row of radially extending blades with the roots of the blades fitting in axially extending slots provided in the disc. During operation of the compressor or turbine it become necessary to prevent axial movement of the blade relative to the disc because of the axial thrust exerted on the blade. The blade root is usually held in the slot by a blade lock which is preferably so constructed that removal of the blade from the disc will not necessitate damaging of either the blade or the disc.
The copending Ledwith application Serial No. 153,795, filed April 4, 1950, having the same assignee as this application, has a blade lock in the form of a strip extending from end to end of the slot that receives the blade root with tabs bent over at each end to engage the ends of the blade root and the sides of the disc. The copending Abild application Serial No. 153,985, filed April 4, 1950, now Patent No. 2,686,656, having the same assignee as this application, has a blade lock in the form of a strip extending from end to end of the slot that receives the blade root with notches therein which engage projecting ribs on the underside of the blade root and with tabs bent over at each end to engage the sides of the disc. These arrangements are generally satisfactory. The present invention presents an alternative arrangement which is equally elfective and in many cases easier to assemble.
Blades have been locked in a disc by forming integral tabs on opposite ends of the blade root with one of the tabs in such a position that the blade root may be inserted in the properly formed slot in the disc and the tab subsequently bent down against the side of the disc. In this instance the blade root is made more difficult to machine and in many cases the material of the blade does not bend readily and very frequently the tab breaks ofi so that the blade must be scrapped. This is especially true in the event of removal and insertion of the blade since the tab frequently cannot be rebent successfully.
An object of this invention is to permit the removal or installation of a blade from one side of the supporting disc while said supporting disc is mounted.
Another object of this invention is to eliminate the necessity for a bent tab to project over either the blade root or the side of the supporting disc to hold said blade in place. In this invention the bent tab is merely used to prevent the locking member from rotating.
A further object of this invention is to provide a looking member which is held in position by a small washer having tabs and in which the centrifugal effect of the disc tends to move the tab cooperating with said locking member in a locking direction. This makes the part which needs to be replaced, if a tab breaks in assembling or disassembling a blade, a very small one.
Another object of this invention is to provide a locking member which is locked from the side of the supporting disc from which the blade is inserted. As can be seen from the locking means of the blades enumerated above, it is necessary to lock said means from the side of the supporting disc opposite that from which the blade is inserted.
Other objects and advantages will be apparent from the specification and claims and from the accompanying drawings which illustrate an embodiment of the invention.
Fig. 1 is an exploded perspective view of a section of the supporting disc, a section of the blade including the blade root, the locking member, and the holding member. The locking member is shown in its locked position if mounted.
Fig. 2 is a axial sectional view on a radial plane through the bottom of a blade root and the bottom of a slot in a disc showing the locking member and its holding mem her in locked position.
Fig. 3 is a rear end view taken on the line 3-3 of Fig. 2.
Fig. 4 is a front end view taken along the line 44 of Fig. 2.
In the arrangement shown the supporting disc 2 has a plurality of slots 4 in its periphery to receive the similarly formed roots 6 of the blades 8. The particular shape of the blade root 6 or of the similarly shaped slot 4 for holding the blade from moving radially with respect to the slot is not critical, and for the purpose of the present invention a slot is shown having a series of ridges 10 extending along the sides of the slot. These ridges extend from the bottom of the slot to the outer periphery of the disc. The blade root is similar in shape having ridges 3, which when the blade root is assembled, slide between the ridges 10 of the disc.
As best shown in Fig. 2, the blade locking member 12 is in a form of a rotatable or angularly turnable pin, or rod, 14 having a head at each end. A rear head 16 is constructed and arranged to engage an area of both the side of the blade root and the side of the supporting disc with which it cooperates in all rotative positions. A front head 18 is constructed and arranged to engage a maximum area of both the other side of the blade root and the other side of the supporting disc in one rotative or angular position, referred to as the locked position and not to engage any portion of the supporting disc in another rotative or angular position 180 degreees from the last mentioned position, referred to as the unlocked position. The length of pin 14 between the inside face 15 of the front head 18 and the inside face 1'7 of the rear head 16 is equal to the width of the disc 2 and blade 8 at this point.
The rear head 16 is formed at one end of pin 14- of two integral circular members having different size diameters. The outside circular member 2% of said rear head 16 is formed of a large diameter having a notch 22 therethrough on the outer periphery thereof for a purpose to be hereinafter described. The inside circular member 24 of said rear head 16 is formed of a reduced diameter to receive a holding member or locking means 26. The diameter of the inner circular member 24 is of such a size that when mounted it covers portions of both the blade root and the cooperating slot in the supporting disc. Holding member 26 consists of a Washer member 28 having two tabs 36 and 32, extending from the outer periphery thereof 180 degrees apart. \Vuile these tabs are placed apart at an angle of degrees it is to be understood that they may be placed at other degrees of angularity.
The front head 18 is formed at the other end of pin 14. This head comprises a member having one half thereof semicircular in shape as at 34 and the other half W a 3 shaped so as to slide through the opening formed at the bottom of a slot 4 of supporting disc 2. In the embodiment shown this other half is formed of three sides 36, 38 and 40, the middle side of the threesides, side 38, being located tangent to the outer periphery of the pin 14 and of a length approximately equal to the diameter of pin 14. This side 33 in the unlocked position of locking member 12 lies in a plane with the bottom 39 of slot 4- ing portions of the root and slot adjacent the bottom of the slot spaced apart in a direction at right angles to the axis of the disc far enough to receive the pin portion of the'locking member and topermit it to turn in the groove.
Before the. mounting of a blade having a locking means such as disclosed herein a holding member 26 has one tab bent so that it extends at an angle of approximately 90 degrees from the plane of the washer portion 28 and the other tab bent so that it extends at an angle of approximately 90 degrees from the plane of the washer member 28 in a direction opposite to that of the other tab (see dotted tab 32 in Fig. 2); In assembling, the holding member 26 is then placed over front head 18 of a blade locking member 12, moved along pin 14, and fitted over the reduced diameter of the inside circular member ,24
of rear head 16. Pin 14 of this blade locking member is now placed in a groove 44 of a blade root 6 of a blade with the tab 30 extending inwardly from holding member 20 being positioned in hole 48. The blade lock is rotated to its unlocked position and the assembled blade root,
invention is capable of various modifications and adaptations within the scope of the appended claims.
I claim:
1. In combination, a supporting disc having an axially extending slot in its periphery, said slot having a bottom, a blade having a root fitting in and engaging in said slot said root having a bottom, said slot and root having interengaging means retaining the blade against radial outward movement relative to the disc, said root and slot having cooperating portions adjacent the bottom spaced apart in a direction at right angles to the axis of the disc to define an axial groove between the root and slot, and means for retaining said blade root in axial position in the slot including a rotatable pin extending through the groove adjacent the bottom of the rooh'said pin having a head at each end, one head being transversely larger than the pin so that it engages an area of both the side 1 7 of the blade root and the side of the supporting disc with locking member and holding member are inserted into a slot in the disc. When the assembly is fully inserted, with face 17 of rear head 16 against the rear side of the blade' root and disc, the locking member is rotated through 180 degrees to the locked position. The locking member is in its fully locked position when the notch 22 is facing directly downward in this arrangement. This provides a means of visual inspection from the one side of the locking member to determine if the opposite side,
is correctly positioned. The tab 32 is then bent over into the notch 22. The locking member 12 now holds the blade in place and the holding member 26 now prevents the locking member from rotating.
'As referred to hereinbefore, the tabs 36 and 32 may be placed in varying degrees of angulan'ty from each other.
having heads of various other shapes which will either permit the blade and locking member to be inserted in the supporting disc together or permit the locking member to be inserted in the supporting disc wtih the blade 7 his also noted here that locking members may be formed being thereafter inserted. These heads may also be shaped so that they will be moved from an unlocked to a locked position in a varying number of degrees.
The type of locking means disclosed in this specification is adapted particularly to installations where one side of the blade and supporting disc is inaccessible when mounted due to an engine part such as indicated at 51L Such an arrangement is shown for example in 'Rubbra 2,594,808 (Fig. 2). As can be seen from Fig. 2 the blade 8 can be removed and replaced from the one side without having to remove the entire supporting disc assembly from the engine. This is advantageous in the field where a minimum of tools are available and the need has been found to replace a blade.
,Although a specific blade locking means has been shown and described herein for purpose of illustration,
itgwill be evident to those skilled in the art that the which it cooperates in all rotative positions, the other head being eccentric to the pin and smaller than the portion of the slot adjacent the bottom so that in one position thereof it will pass through said slot when said pin is in said groove and in another position it will engage an area of both the endof the blade root and the side of the supporting disc with which it cooperates.
2. In combination, a supporting disc having. axially extending slots in its periphery, a number of blades, each blade having a root fitting in and engaged in one of said slots of said disc, each root and the cooperating slot shaving adjacent portions spaced apart radially and forming therebetween an axially extending groove, and means for retaining each of said blade roots in axial'position in its slot including a rotatable pin in said groove having a head at each end, one head being transversely larger-than the pin and engaging an area of both the side of the blade root and the side of the'supporting disc with which it cooperates in all rotative positions, the other head being eccentric to the pin and projecting beyond the pin surface except on one side thereof which is tangential to the surface of the pin and being smaller than the'slot in the disc so that in one angular position it will permit said root to pass through. said slot and in another angular,
position it will engage an areaof both the end of the blade root and the side of the supporting disc with which it cooperates.
3. A rotor including a disc having axially extending slots in its periphery, a number of blades having roots,
with each root fitting in and engaged in one of the slots,
extending passageway between the surfaces of said "coopcrating portions, a rotatable pin extending' through' said passageway, said pin having a head at each end, the head at one end being larger than the passageway in transverse section to overlap a part of the blade root and a part of the disc, the head at the other end being smaller in transverse section than the disc slot to' overlap a part of the blade root only in one position of the pin, said second named 'head being eccentrically arranged on the pin to overlap both a part of the blade root and a part of the disc in another angular position of said'pin, and pin locking means engaging said pin and for locking said pin against rotation in the passageway. i
4. A rotor including a disc having an axially extending slot in its periphery, a blade having a root, with said root fitting in and engaged in said slot, the cooperating slot and blade root having means retaining the blade'against radial outward movement relative to the disc and 'said.
slot and root having adjacent portions radially spaced apart thereby forming an axially extending passageway between the surfaces of said adjacent portions, a rotatable pin extending through said passageway, said pin having a head at each end, the head at one end being smaller in transverse section than said slot and eccentric to the axis of the pin to overlap only a portion of the blade root in one angular position of the pin and to overlap a part of the blade root and also a part of the disc at another 5 angular position of said pin, the head at the other end of the pin being larger in transverse section than the passageway to overlap both a part of the blade root and a part of the disc at least in said another angular position of said pin, and pin locking means engaging said pin for 10 looking said pin against rotation in the passageway;
References Cited in the file of this patent UNITED STATES PATENTS Kasley Mar. 1, 1927 Gibbons Aug. 16, 1932, Gwinn et al. Sept. 12, 1939 Poupitch Dec. 9, 1952 FOREIGN PATENTS Great Britain of 1908 Belgium Jan. 15, 1951 Great Britain Mar. 31, 1949
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Cited By (27)

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US3001759A (en) * 1958-06-11 1961-09-26 Gen Motors Corp Rotor blade lock
US3057598A (en) * 1960-07-01 1962-10-09 Ass Elect Ind Locking means for turbine or compressor blading
US3076634A (en) * 1959-06-12 1963-02-05 Ass Elect Ind Locking means for compressor and turbine blades
US3395891A (en) * 1967-09-21 1968-08-06 Gen Electric Lock for turbomachinery blades
US3632228A (en) * 1970-07-29 1972-01-04 Gen Electric Device for locking turbomachinery blades
US3728042A (en) * 1971-08-27 1973-04-17 Westinghouse Electric Corp Axial positioner and seal for cooled rotor blade
US3748060A (en) * 1971-09-14 1973-07-24 Westinghouse Electric Corp Sideplate for turbine blade
US3832092A (en) * 1973-10-19 1974-08-27 Gen Electric Device for locking turbomachinery blades
US3986779A (en) * 1974-05-27 1976-10-19 Brown Boveri-Sulzer Turbomaschinen Aktiengesellschaft Locking device for releasably fastening parts to rotors of fluid flow machines
US4836749A (en) * 1988-02-19 1989-06-06 Westinghouse Electric Corp. Pre-load device for a turbomachine rotor
US5860787A (en) * 1996-05-17 1999-01-19 Rolls-Royce Plc Rotor blade axial retention assembly
US6190131B1 (en) * 1999-08-31 2001-02-20 General Electric Co. Non-integral balanced coverplate and coverplate centering slot for a turbine
US6416286B1 (en) * 2000-12-28 2002-07-09 General Electric Company System and method for securing a radially inserted integral closure bucket to a turbine rotor wheel assembly having axially inserted buckets
EP1306522A1 (en) * 2001-10-29 2003-05-02 ABB Turbo Systems AG Locking device for axial turbomachine blades
US6575704B1 (en) * 1999-06-07 2003-06-10 Siemens Aktiengesellschaft Turbomachine and sealing element for a rotor thereof
US20050265846A1 (en) * 2004-06-01 2005-12-01 Przytulski James C Balance assembly for rotary turbine component and method for installing and/or adjusting balance weight
US20060073021A1 (en) * 2004-10-06 2006-04-06 Siemens Westinghouse Power Corporation Remotely accessible locking system for turbine blades
JP2009024698A (en) * 2007-07-19 2009-02-05 General Electric Co <Ge> Pushing plate seal
US20100068063A1 (en) * 2007-05-31 2010-03-18 Richard Hiram Berg Methods and apparatus for assembling gas turbine engines
US20100284805A1 (en) * 2009-05-11 2010-11-11 Richard Christopher Uskert Apparatus and method for locking a composite component
EP2386721A1 (en) * 2010-05-14 2011-11-16 Siemens Aktiengesellschaft Fastening assembly for blades of axial fluid flow turbo machines and procedure for producing the same
US20150037161A1 (en) * 2013-07-30 2015-02-05 MTU Aero Engines AG Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
US20150078907A1 (en) * 2013-09-13 2015-03-19 General Electric Company Turbomachine including a non-destructive fastener element for joining components
JP2015098848A (en) * 2013-11-20 2015-05-28 三菱重工業株式会社 Turbine rotor assembly, blade stop plate in turbine rotor assembly, and blade stop plate assembly method
US20180266260A1 (en) * 2017-03-16 2018-09-20 Doosan Heavy Industries & Construction Co., Ltd Apparatus for axial locking of bucket and bucket assembly and gas turbine having the same
US11339674B2 (en) * 2018-08-14 2022-05-24 Rolls-Royce North American Technologies Inc. Blade retainer for gas turbine engine
JP7217330B1 (en) 2021-11-18 2023-02-02 三菱重工業株式会社 Turbine rotor and manufacturing method thereof

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US3001759A (en) * 1958-06-11 1961-09-26 Gen Motors Corp Rotor blade lock
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US3057598A (en) * 1960-07-01 1962-10-09 Ass Elect Ind Locking means for turbine or compressor blading
US3395891A (en) * 1967-09-21 1968-08-06 Gen Electric Lock for turbomachinery blades
US3632228A (en) * 1970-07-29 1972-01-04 Gen Electric Device for locking turbomachinery blades
US3728042A (en) * 1971-08-27 1973-04-17 Westinghouse Electric Corp Axial positioner and seal for cooled rotor blade
US3748060A (en) * 1971-09-14 1973-07-24 Westinghouse Electric Corp Sideplate for turbine blade
US3832092A (en) * 1973-10-19 1974-08-27 Gen Electric Device for locking turbomachinery blades
US3986779A (en) * 1974-05-27 1976-10-19 Brown Boveri-Sulzer Turbomaschinen Aktiengesellschaft Locking device for releasably fastening parts to rotors of fluid flow machines
US4836749A (en) * 1988-02-19 1989-06-06 Westinghouse Electric Corp. Pre-load device for a turbomachine rotor
US5860787A (en) * 1996-05-17 1999-01-19 Rolls-Royce Plc Rotor blade axial retention assembly
US6575704B1 (en) * 1999-06-07 2003-06-10 Siemens Aktiengesellschaft Turbomachine and sealing element for a rotor thereof
US6190131B1 (en) * 1999-08-31 2001-02-20 General Electric Co. Non-integral balanced coverplate and coverplate centering slot for a turbine
US6416286B1 (en) * 2000-12-28 2002-07-09 General Electric Company System and method for securing a radially inserted integral closure bucket to a turbine rotor wheel assembly having axially inserted buckets
WO2002053875A1 (en) * 2000-12-28 2002-07-11 General Electric Company Assembly method and jig for integrally covered axially inserted bucket blades
EP1306522A1 (en) * 2001-10-29 2003-05-02 ABB Turbo Systems AG Locking device for axial turbomachine blades
WO2003038240A1 (en) * 2001-10-29 2003-05-08 Abb Turbo Systems Ag Securing device for the moving blades of axial flow turbomachines
US20050265846A1 (en) * 2004-06-01 2005-12-01 Przytulski James C Balance assembly for rotary turbine component and method for installing and/or adjusting balance weight
US20060073021A1 (en) * 2004-10-06 2006-04-06 Siemens Westinghouse Power Corporation Remotely accessible locking system for turbine blades
US7264448B2 (en) 2004-10-06 2007-09-04 Siemens Power Corporation, Inc. Remotely accessible locking system for turbine blades
US20100068063A1 (en) * 2007-05-31 2010-03-18 Richard Hiram Berg Methods and apparatus for assembling gas turbine engines
US8016565B2 (en) * 2007-05-31 2011-09-13 General Electric Company Methods and apparatus for assembling gas turbine engines
JP2009024698A (en) * 2007-07-19 2009-02-05 General Electric Co <Ge> Pushing plate seal
US8425194B2 (en) 2007-07-19 2013-04-23 General Electric Company Clamped plate seal
US20100284805A1 (en) * 2009-05-11 2010-11-11 Richard Christopher Uskert Apparatus and method for locking a composite component
US8439635B2 (en) 2009-05-11 2013-05-14 Rolls-Royce Corporation Apparatus and method for locking a composite component
EP2386721A1 (en) * 2010-05-14 2011-11-16 Siemens Aktiengesellschaft Fastening assembly for blades of axial fluid flow turbo machines and procedure for producing the same
WO2011141514A1 (en) * 2010-05-14 2011-11-17 Siemens Aktiengesellschaft Fastening assembly for blades of turbomachines having axial flow and method for producing such an assembly
US20150037161A1 (en) * 2013-07-30 2015-02-05 MTU Aero Engines AG Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
US20150078907A1 (en) * 2013-09-13 2015-03-19 General Electric Company Turbomachine including a non-destructive fastener element for joining components
JP2015098848A (en) * 2013-11-20 2015-05-28 三菱重工業株式会社 Turbine rotor assembly, blade stop plate in turbine rotor assembly, and blade stop plate assembly method
WO2015075970A1 (en) * 2013-11-20 2015-05-28 三菱重工業株式会社 Turbine rotor assembly, blade stop plate for turbine rotor assembly, and method for assembling blade stop plate
CN105473824A (en) * 2013-11-20 2016-04-06 三菱重工业株式会社 Turbine rotor assembly, blade stop plate for turbine rotor assembly, and method for assembling blade stop plate
US20180266260A1 (en) * 2017-03-16 2018-09-20 Doosan Heavy Industries & Construction Co., Ltd Apparatus for axial locking of bucket and bucket assembly and gas turbine having the same
EP3375979B1 (en) * 2017-03-16 2020-06-10 Doosan Heavy Industries & Construction Co., Ltd. Apparatus for axial locking of bucket and bucket assembly and gas turbine having the same
US10934864B2 (en) * 2017-03-16 2021-03-02 DOOSAN Heavy Industries Construction Co., LTD Apparatus for axial locking of bucket and bucket assembly and gas turbine having the same
US11339674B2 (en) * 2018-08-14 2022-05-24 Rolls-Royce North American Technologies Inc. Blade retainer for gas turbine engine
JP7217330B1 (en) 2021-11-18 2023-02-02 三菱重工業株式会社 Turbine rotor and manufacturing method thereof
JP2023074610A (en) * 2021-11-18 2023-05-30 三菱重工業株式会社 Turbine rotor and manufacturing method of the same

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