US2857134A - Assembly of blades for turbines and the like - Google Patents
Assembly of blades for turbines and the like Download PDFInfo
- Publication number
- US2857134A US2857134A US416868A US41686854A US2857134A US 2857134 A US2857134 A US 2857134A US 416868 A US416868 A US 416868A US 41686854 A US41686854 A US 41686854A US 2857134 A US2857134 A US 2857134A
- Authority
- US
- United States
- Prior art keywords
- packer
- groove
- blades
- blade
- serrations
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
Definitions
- the invention relates to the improvements in and relating to assembly of blades for turbines and the like that is to say to turbine or compressor or fan blades and more specifically to those of the integral root type which are assembled in serrated circumferential grooves in a rotor, said blades being separated from each other in grooves by spacing or packing pieces of similar shape to the roots of the blades.
- Blades of the type described above which have integral blade roots of a lozenge that is parallelepiped shape, are inserted in a circumferential groove turned in the rotor, the sides of the groove being serrated to hold the blades and packing pieces in position against the action of centrifugal force.
- both the blade root and packing piece are of a lozengeshape so chosen that a blade or packing piece may be turned into position in the groove.
- Both blade root and packing piece have serrations machined on their smallest two faces, these serrations matching and intermeshing with serrations on the side of the rotor groove.
- the closing packer When a lantern space is provided the closing packer is dropped into it and slid into position in the blade groove.
- the lantern space is then filled by fitting a steel strip, both sides of which are serrated into the lantern space adjacent to the closing packer, the serrated side in contact with the closing packer, also engaging with short lengths of the serrations of adjacent blades, and then peening copper or other ductile material into the remaining lantern space, the peened-in metal entering into the serrations in the said lantern space and free side of the steel strip so retaining itself in position against the action of centrifugal force.
- the provision of the lantern space has certain disadvantages, in that it involves additional machining of the rotor, the rotor stress is increased due to the increased load on the remainder of the rim, and renewal of the blades is made diflicult.
- the object of the invention is to provide an improved closing packer for turbine or compressor blades of the integral root type which are assembled in serrated circumferential grooves in the rotor, free from the above mentioned disadvantages.
- the invention consists in a closing packer for turbine or compressor blades of the integral root type which are 2,857,134 Patented Oct. 21, 1958 iceassembled in serrated circumferential grooves in the rotor, which is made in two parts in such a way that when the two parts are in position and secured, they form a closing packer identical in shape and outside dimensions with the normal 'blade packing pieces.
- the invention also consists in a closing packer in accordance with the preceding paragraph in which each part has a hole drilled through it so located so that when the two pieces are brought together it is substantially midway between serrated edges, said hole in'the part of the packer which is inserted in the groove first, that is the lower part, being tapped to accommodate a socket screw, the hole in the upper part being a clearance hole countersunk to accommodate the said socket screw and in closing packers as described below.
- Figure 1 is a plan
- Figure 2 an elevation of the lower part of a closing packer according to one form of the present invention
- Figure 3 is an elevation of the upper part of a closing packer for use with Figures 1 and 2;
- Figure 4 shows the arrangement of blades and packing pieces in a typical blade row the last blade to be inserted being 'shown;
- Figure 5 is a section on the line 5-5 of Figure 4 looking in the direction of the arrows;
- Figure 6 shows the assembly of the closing packer in the rotor groove and is a section along a plane through the axis of the rotor.
- the closing packer consists of three parts a, b and c, the latter of which is a socket screw.
- the parts a and b when properly placed together have outside dimensions and shape identical with that of the normal blade packing pieces and the joint d between the two parts is of the form shown in Figure 2, the oblique faces 2 and fof the joint being parallel with the locally approximate plane surfaces of the lower side g of serrations h on one side of the packer and the upper side i of the serrations j on the other side.
- the position of the joint is so chosen that the distance A in Figure 6 is less than the distance B.
- the two halves of the packer are fastened together by means of the socket screw 0, this being tapped into the lower half ,a of the closing packer and passing through a clearance hole m in the upper half b of the packer, the clearance hole m being slightly larger than the diameter of the screw 0 accommodated by it.
- the head of the screw 0 is countersunk into the upper half, the countersink n being of greater diameter than the head of the screw, and the hole m being of greater diameter than the shank of the screw above the threaded portion thereof, thus allowing limited relative movement to take place between the two halves.
- the top half b of the packer can then he slid into positiomalong theplane vaferentialu.groove,; the .groove ehaving circumferentially of-the oblique-"faces e a'nd f'of the packer joint as in Figure 6-its-serrations sliding-into-mesh--with-the-groove serrations.
- the screw 0 is then placed in position and tightened. In doing this, due to the clearance which exists between; the, screw iandstthe upper. half a b (of ;-the packer in directions; radialatotathe; scvewa theatwo halves wand 12: of: the packet 103D?
- "013 ,38 is :preferred, byz eexpedienuo tdrillingl, ansm'all -blindt hole x :in' the optautfa ofzthe closingmackenadjacent(to-the counters nking anduswagingi-ithe ithin; wall (of: metal-separating the blindlholet-frorn the countersinkeinto/ithe knurls. It is :arranged itha'tjwhen'; the twot parts.- are securely locked together -agsmall gapais vdeft rbetween the opposite .faces, o t a h-w rt (on!
- a packer comprising two parts having oppositely facing serrated edges for fitting the serrated side walls of the said groove of the rotor, the serrations of the said edges on one of the two said parts having substantially parallel surfaces, the two said parts having cooperating surfaces for-fitting-together, the said cooperating surfaces,.,-beipg rparallel-Jo the first said parallel sur- 10 faces, whereby one of the said 'parts may be placed in position in the said rotor groove and the other slid into position therein, and meansforholding the two said parts of I the packer together in-assembled position ',within the said groove with the serrations on the edges of the said iwsmar stpfi theipackeneneage i n thes r at c of walls of the said groove.
- a packer according toclaim 1,-'-in which the means holding the two said parts together comprises a screw passing through one of them and countersunk therein and-threadably-engagedwinthe'othcr.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
Oct. 21, 1958 G. F. ARKLESS ASSEMBLY OF BLADES FOR TURBINES AND THE LIKE Filed March 17. 1954 United States Patent Ci 2,857,134 ASSEMBLY OF BLADES FOR TURBINES AND THE LIKE Application March 17, 1954, Serial No. 416,868
3 Claims. (Cl. 253-77) The invention relates to the improvements in and relating to assembly of blades for turbines and the like that is to say to turbine or compressor or fan blades and more specifically to those of the integral root type which are assembled in serrated circumferential grooves in a rotor, said blades being separated from each other in grooves by spacing or packing pieces of similar shape to the roots of the blades.
Blades of the type described above which have integral blade roots of a lozenge that is parallelepiped shape, are inserted in a circumferential groove turned in the rotor, the sides of the groove being serrated to hold the blades and packing pieces in position against the action of centrifugal force. In plan view both the blade root and packing piece are of a lozengeshape so chosen that a blade or packing piece may be turned into position in the groove. Both blade root and packing piece have serrations machined on their smallest two faces, these serrations matching and intermeshing with serrations on the side of the rotor groove.
With such an arrangement the completing or final packing piece, that is to say what may be called the closing packer of a row, cannot be inserted in the same manner as its predecessors. It is common practice to provide a milled-out pocket in the rotor adjacent to the groove and opposite to the position to be occupied by the closing packer and which enters into the circumferential blade groove. The depth of this pocket, or lantern space as it is comomnly termed, is the same as that of the blade groove: its width is also similar to that-of the blade groove and its length in the peripheral direction is somewhat greater than one blade root pitch. Its three walls are serrated in a similar fashion to the blade groove.
When a lantern space is provided the closing packer is dropped into it and slid into position in the blade groove. The lantern space is then filled by fitting a steel strip, both sides of which are serrated into the lantern space adjacent to the closing packer, the serrated side in contact with the closing packer, also engaging with short lengths of the serrations of adjacent blades, and then peening copper or other ductile material into the remaining lantern space, the peened-in metal entering into the serrations in the said lantern space and free side of the steel strip so retaining itself in position against the action of centrifugal force.
The provision of the lantern space has certain disadvantages, in that it involves additional machining of the rotor, the rotor stress is increased due to the increased load on the remainder of the rim, and renewal of the blades is made diflicult.
The object of the invention is to provide an improved closing packer for turbine or compressor blades of the integral root type which are assembled in serrated circumferential grooves in the rotor, free from the above mentioned disadvantages.
The invention consists in a closing packer for turbine or compressor blades of the integral root type which are 2,857,134 Patented Oct. 21, 1958 iceassembled in serrated circumferential grooves in the rotor, which is made in two parts in such a way that when the two parts are in position and secured, they form a closing packer identical in shape and outside dimensions with the normal 'blade packing pieces.
The invention also consists in a closing packer in accordance with the preceding paragraph in which each part has a hole drilled through it so located so that when the two pieces are brought together it is substantially midway between serrated edges, said hole in'the part of the packer which is inserted in the groove first, that is the lower part, being tapped to accommodate a socket screw, the hole in the upper part being a clearance hole countersunk to accommodate the said socket screw and in closing packers as described below.
Referring to the accompanying diagrammatic drawings:
Figure 1 isa plan, and
Figure 2 an elevation of the lower part of a closing packer according to one form of the present invention;
Figure 3 is an elevation of the upper part of a closing packer for use with Figures 1 and 2;
Figure 4 shows the arrangement of blades and packing pieces in a typical blade row the last blade to be inserted being 'shown;'
Figure 5 is a section on the line 5-5 of Figure 4 looking in the direction of the arrows;
Figure 6 shows the assembly of the closing packer in the rotor groove and is a section along a plane through the axis of the rotor.
Referring to the aforesaid accompanying diagrammatic drawings which illustrate the preferred form of the present invention, the closing packer consists of three parts a, b and c, the latter of which is a socket screw. The parts a and b when properly placed together have outside dimensions and shape identical with that of the normal blade packing pieces and the joint d between the two parts is of the form shown in Figure 2, the oblique faces 2 and fof the joint being parallel with the locally approximate plane surfaces of the lower side g of serrations h on one side of the packer and the upper side i of the serrations j on the other side. The position of the joint is so chosen that the distance A in Figure 6 is less than the distance B. This admits of the lower half a of the packer being dropped into a groove k and its serrations meshed with those I of the groove, the serrations of the two ends of the packer fitting into the circumferential serrations l of the side walls of the groove k as shown in the drawing.
The two halves of the packer are fastened together by means of the socket screw 0, this being tapped into the lower half ,a of the closing packer and passing through a clearance hole m in the upper half b of the packer, the clearance hole m being slightly larger than the diameter of the screw 0 accommodated by it. The head of the screw 0 is countersunk into the upper half, the countersink n being of greater diameter than the head of the screw, and the hole m being of greater diameter than the shank of the screw above the threaded portion thereof, thus allowing limited relative movement to take place between the two halves.
To assemble, when a row has been fitted with blades indicated by the reference letter 0 in Figure 4 the packing pieces indicated by the reference letter p except for the final or closing packer, one or both of the obtuse corners of the last blade root being rounded off to permit of turning of this blade into position as shown in Figure 4, if necessary, the first blade inserted in the row having the reference letter q and the last blade having the reference letter r, the lower half a of the closing packer is dropped into the vacant space in the groove and pulled back so that its serrated side meshes with the serrations in the groove as shown in Figure 6. The top half b of the packer; can then he slid into positiomalong theplane vaferentialu.groove,; the .groove ehaving circumferentially of-the oblique-"faces e a'nd f'of the packer joint as in Figure 6-its-serrations sliding-into-mesh--with-the-groove serrations. The screw 0 is then placed in position and tightened. In doing this, due to the clearance which exists between; the, screw iandstthe upper. half a b (of ;-the packer in directions; radialatotathe; scvewa theatwo halves wand 12: of: the packet 103D? slide (slightly on .one: another and rtightem themsclves/into-the, groove-serrationsz z Finally the screw can be locked, either; bytsimplyhpeening the metal-.tsurrounding thenhead-linto knurls provided on .-the side. of the. head rof \the; :sQcket-l screw. "013 ,38 is :preferred, byz eexpedienuo tdrillingl, ansm'all -blindt hole x :in' the optautfa ofzthe closingmackenadjacent(to-the counters nking anduswagingi-ithe ithin; wall (of: metal-separating the blindlholet-frorn the countersinkeinto/ithe knurls. It is :arranged itha'tjwhen'; the twot parts.- are securely locked together -agsmall gapais vdeft rbetween the opposite .faces, o t a h-w rt (on! ithfl'usidesiOfH-fllflnSOCkGf' screw 0, the planes of which areratrightaangles to theusockebserew c; t t iS QsSWr'bfilfifififlifiCfl:deaf-part a and the corresponding face of part b, to allow fort-ietfective tightening and wedge; action :on-; the diagonaltfaees.inacontact.
whilst the invention is described with reference to-an axial flowjpompresson the closing, packen may -be-.used in axial flow turbinesn-whereathe:root circumferential Pitch o lt e blades .is ;s.ufiici ent;to accommodateit.
I-claim:
1. In a turbine or compressor rotor having a circumserrated side walls, and fan blades and packers fitted in -the--said-groove, a packer comprising two parts having oppositely facing serrated edges for fitting the serrated side walls of the said groove of the rotor, the serrations of the said edges on one of the two said parts having substantially parallel surfaces, the two said parts having cooperating surfaces for-fitting-together, the said cooperating surfaces,.,-beipg rparallel-Jo the first said parallel sur- 10 faces, whereby one of the said 'parts may be placed in position in the said rotor groove and the other slid into position therein, and meansforholding the two said parts of I the packer together in-assembled position ',within the said groove with the serrations on the edges of the said iwsmar stpfi theipackeneneage i n thes r at c of walls of the said groove.
2. A packer according toclaim 1,-'-in which the means holding the two said parts together comprises a screw passing through one of them and countersunk therein and-threadably-engagedwinthe'othcr.
-3. -A -paoker--according' to=claim 2, in which each of the two-said parts have also-anengaging surface adjacent to'andsubstantially at right'angles to the said screw.
:Gre t Br. .t nr,--.---.- J ne 28, 1950 .Cirea t., Britain V Oct. 24, 11951
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US416868A US2857134A (en) | 1954-03-17 | 1954-03-17 | Assembly of blades for turbines and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US416868A US2857134A (en) | 1954-03-17 | 1954-03-17 | Assembly of blades for turbines and the like |
Publications (1)
Publication Number | Publication Date |
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US2857134A true US2857134A (en) | 1958-10-21 |
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Application Number | Title | Priority Date | Filing Date |
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US416868A Expired - Lifetime US2857134A (en) | 1954-03-17 | 1954-03-17 | Assembly of blades for turbines and the like |
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3778191A (en) * | 1970-01-21 | 1973-12-11 | Daimler Benz Ag | Blade mounting |
DE2514050A1 (en) * | 1975-01-30 | 1976-08-05 | Bbc Sulzer Turbomaschinen | LOCKING OF PARTS ATTACHED TO THE ROTOR BODY OF TURBO MACHINERY |
US6299411B1 (en) * | 1999-02-12 | 2001-10-09 | Abb Alstom Power (Schweiz) Ag | Fastening of moving blades of a fluid-flow machine |
US20040179944A1 (en) * | 2003-03-11 | 2004-09-16 | Rene Bachofner | Rotor end piece |
US20060062674A1 (en) * | 2003-03-26 | 2006-03-23 | Hans Wettstein | Axial-flow thermal turbomachine |
EP1803900A1 (en) * | 2006-01-02 | 2007-07-04 | Siemens Aktiengesellschaft | Closure unit for the remaining space between the first and the last blades of a bladed ring inserted in a circumferencial slot of a turbomachine, and corresponding turbomachine |
US20080003098A1 (en) * | 2004-12-21 | 2008-01-03 | Alstom Technology Ltd. | Method for modification of a turbocompressor |
US20110027090A1 (en) * | 2009-08-03 | 2011-02-03 | General Electric Company | Locking spacer assembly for a circumferential dovetail rotor blade attachment system |
US20150101347A1 (en) * | 2013-10-16 | 2015-04-16 | General Electric Company | Locking spacer assembly |
US20150101346A1 (en) * | 2013-10-16 | 2015-04-16 | General Electric Company | Locking spacer assembly |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB639320A (en) * | 1948-10-22 | 1950-06-28 | Frank Rosslyn Harris | Improvements in or relating to the mounting of turbine, compressor or like blades |
GB659592A (en) * | 1948-09-17 | 1951-10-24 | Sulzer Ag | Improvements relating to rotors for turbines or axial flow compressors |
-
1954
- 1954-03-17 US US416868A patent/US2857134A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB659592A (en) * | 1948-09-17 | 1951-10-24 | Sulzer Ag | Improvements relating to rotors for turbines or axial flow compressors |
GB639320A (en) * | 1948-10-22 | 1950-06-28 | Frank Rosslyn Harris | Improvements in or relating to the mounting of turbine, compressor or like blades |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3778191A (en) * | 1970-01-21 | 1973-12-11 | Daimler Benz Ag | Blade mounting |
DE2514050A1 (en) * | 1975-01-30 | 1976-08-05 | Bbc Sulzer Turbomaschinen | LOCKING OF PARTS ATTACHED TO THE ROTOR BODY OF TURBO MACHINERY |
US6299411B1 (en) * | 1999-02-12 | 2001-10-09 | Abb Alstom Power (Schweiz) Ag | Fastening of moving blades of a fluid-flow machine |
US20040179944A1 (en) * | 2003-03-11 | 2004-09-16 | Rene Bachofner | Rotor end piece |
US7048508B2 (en) * | 2003-03-11 | 2006-05-23 | Alstom Technology Ltd. | Rotor end piece |
US20060062674A1 (en) * | 2003-03-26 | 2006-03-23 | Hans Wettstein | Axial-flow thermal turbomachine |
US7037079B2 (en) * | 2003-03-26 | 2006-05-02 | Alstom Technology Ltd. | Axial-flow thermal turbomachine |
US20080003098A1 (en) * | 2004-12-21 | 2008-01-03 | Alstom Technology Ltd. | Method for modification of a turbocompressor |
US20090016889A1 (en) * | 2006-01-02 | 2009-01-15 | Joachim Krutzfeldt | Locking Sub-Assembly for Closing The Remaining Gap Between The First and The Last blade of a Blade Ring Which Are Inserted in a Circumferential Groove of a Turbomachine, and Corresponding Turbomachine |
WO2007077183A1 (en) * | 2006-01-02 | 2007-07-12 | Siemens Aktiengesellschaft | Closing assembly for closing the gap remaining between the first and last blade of a blade ring that is inserted into the peripheral groove of turbomachinery and corresponding turbomachinery |
EP1803900A1 (en) * | 2006-01-02 | 2007-07-04 | Siemens Aktiengesellschaft | Closure unit for the remaining space between the first and the last blades of a bladed ring inserted in a circumferencial slot of a turbomachine, and corresponding turbomachine |
US8157530B2 (en) | 2006-01-02 | 2012-04-17 | Siemens Aktiengesellschaft | Locking sub-assembly for closing the remaining gap between the first and the last of a blade ring which are inserted in a circumferential groove of a turbomachine, and corresponding turbomachine |
US20110027090A1 (en) * | 2009-08-03 | 2011-02-03 | General Electric Company | Locking spacer assembly for a circumferential dovetail rotor blade attachment system |
US8176598B2 (en) * | 2009-08-03 | 2012-05-15 | General Electric Company | Locking spacer assembly for a circumferential dovetail rotor blade attachment system |
US20150101346A1 (en) * | 2013-10-16 | 2015-04-16 | General Electric Company | Locking spacer assembly |
US20150101347A1 (en) * | 2013-10-16 | 2015-04-16 | General Electric Company | Locking spacer assembly |
JP2015078692A (en) * | 2013-10-16 | 2015-04-23 | ゼネラル・エレクトリック・カンパニイ | Locking spacer assembly |
CN104675448A (en) * | 2013-10-16 | 2015-06-03 | 通用电气公司 | Locking spacer assembly |
CN104675449A (en) * | 2013-10-16 | 2015-06-03 | 通用电气公司 | Locking spacer assembly |
US9416670B2 (en) * | 2013-10-16 | 2016-08-16 | General Electric Company | Locking spacer assembly |
US9512732B2 (en) * | 2013-10-16 | 2016-12-06 | General Electric Company | Locking spacer assembly inserted between rotor blades |
CN104675449B (en) * | 2013-10-16 | 2017-11-03 | 通用电气公司 | Lockout interval component |
CN104675448B (en) * | 2013-10-16 | 2017-11-28 | 通用电气公司 | Lockout interval component |
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