US930735A - Device for fixing turbine-blades. - Google Patents

Device for fixing turbine-blades. Download PDF

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Publication number
US930735A
US930735A US47188509A US1909471885A US930735A US 930735 A US930735 A US 930735A US 47188509 A US47188509 A US 47188509A US 1909471885 A US1909471885 A US 1909471885A US 930735 A US930735 A US 930735A
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Prior art keywords
blades
turbine
shaft
blade
tool
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US47188509A
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Johannes Dahl
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BLOHM AND VOSS COMMANDITGESELLSCHAFT AUF ACTIEN
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BLOHM AND VOSS COMMANDITGESELLSCHAFT AUF ACTIEN
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/37—Impeller making apparatus

Definitions

  • This invention rela'testo a device for fixing turbine blades in their blade carrying members and its object is to provide a simple mechanical device for effecting thispurpose.
  • the invention consists in a device comprising a pressing tool mechanically reciprocated in a substantially tangential direction in the groove of the bladed member and means for applying a resistance to the tool or the bladed member or the tool operating parts, this resistance being overcome only at a pressure which is adequate to upset the turbine blade root or distance piece within its retaining groove.
  • the blades and distance pieces may be separately pressed into position or a blade and a distance piece or several blades and a corresponding number of distance pieces may be simultaneously pressed or upset within the groove.
  • the drum is rotatably mounted and a brake or ratchet mechanism applied to prevent the rotation of the drum before the tool presses on the part to be fixed in the groove with a pressure sufiicient to upset the said part or parts.
  • a brake or ratchet mechanism applied to prevent the rotation of the drum before the tool presses on the part to be fixed in the groove with a pressure sufiicient to upset the said part or parts.
  • FIG. 1 is a diagrammatic side view and F ig. 2 is a diagrammatic front elevation of a turbine drum showing the apparatus according to the present invention and illustrating its operation
  • Fig. 3 is an enlarged section of the turbine drum and blades
  • Fig. 4 is a front elevation and Fig. 5 is a plan of the same
  • Fig. 6 is a side elevation
  • Fig. 7 is a plan of a modified form of the apparatus especially applicable to the insertion of large blades
  • Fig. 8 is a sectional elevation
  • Fig. 9 is a sectional side view
  • Fig. 10 a plan of a device suitable for fixing blades in a turbine casing according to the present invention.
  • the turbine drum 25 having several grooves 25' therein is to be provided with blades 70 which are divided from one another by distance pieces g.
  • the axis a of the drum is supported in bearings a and is provided with a brake b, the lever h of which is loaded by means of a weight g.
  • the eccentric pin 6 has pivoted to it a pressing or calking tool 8, the point of which fits in the grooves of the turbine drum and is adapted to press against the blades and distance pieces. These blades and distance pieces may be inserted in the groove by hand.
  • the pressing tool When the shaft w rotates the pressing tool is reciprocated in a substantially tangential direction between the positions 8 and s Fig. 3.. In the position 8' the blades 19 and distance pieces 9 are inserted. During the motion. from the position 8 to the position 8 these blades are firmly pressed by the tool .9. In consequence of the constant braking force exerted on the axis ofthe drum by the brake b, the pressure of the tool .9 is always the same and this pressure may be adjusted by adjusting the brake. In all cases the pressure of the tool 8 on the distance pieces must be suflicientto upset the blade root and distance piece. When this pressure is reached the drum 6 is caused to rotate through a short distance by the further motion of the tool 8. It will be seen that this further rotation is effected by overcoming the resistance which is applied to the drum by means of the brake and that this resistance is at least as great as the pressure necessary to upsetthe parts to be fixed in the groove.
  • a wedge When starting to insert a ring or crown of blades a wedge is inserted in the groove in the usual manner and the first blade butts against the wedge. W hen the crown of blades is almost completed a bent tool may be used for inserting a few of the last blades while the remaining blades are of course inserted by hand in the usual manner.
  • the resistance is preferably constant and that this constant resistance may be secured by various means. Further the resistance may be applied to the tool 8 or its moving mechanism. The invention also may be applied to blades fixed axially or radially.
  • the pressing tool 8 forms the stem of a pneumatic hammer 0 which is pivoted to the pin 0, mounted on a disk 0
  • the disk 0 is fixed to a driven shaft w.
  • this shaft rotates in the direction of the arrow in Fig. G-the stem 8 is moved in a substantially tangential direction to the turbine groove.
  • the method of fixing the parts 7) and (1 in this device is as follows:
  • the axis a is braked for instance in the manner described with reference to Figs. 1 and 2.
  • the pin a is moved at the rotation of the shaft in in the direction of the arrow to a point cl and during this time the parts 2) and g to be inserted are laid in the grooves.
  • the rotation of the shaft to is stopped by throwing out a coupling w.
  • the supply of air to the hammer c is then opened by the operator holding the handle 0 of the pneumatic hammer so that the stem 0 makes a series of impacts against the blade 2) or distance piece 9.
  • the pneumatic hammer is then put out of operation and the shaft w allowed to rotate further.
  • the pin 0 then moves from the point (Z to the point 0 and in this motion pushes the drum 6 one stage further against the braking action which is applied to the axis a.
  • the resistance offered by the brake must be sutlicient to prevent the action of the pneumatic hammer causing rotation of the drum.
  • the steady pressure applied from the point (Z to the point 0 finishes the upsetting of the blades and distance pieces 9 in the manner described above with reference to Fig. 1.
  • This form of apparatus is specially suited for large blades and may be applied to the insertion of blades in either the turbine drum or casing.
  • Figs. 8-10 T have shown a form of my invention specially applicable for use in the insertion of turbine blades in. a turbine casing.
  • the turbine casing 11 supports a shaft 12 in bearings 13.
  • the upper cover 14- of the bearings 13 may be tightened down on the shaft 12 for the purpose of giving a braking action.
  • the shaft 12 is provided with a feather way 15 in which a feather or spline 16 is adapted to slide.
  • the spline 1G is carried by an eye 17.
  • On this eye there is mounted a shaft 18 which may be driven by a motor through a flexible shaft.
  • the shaft 18 has mounted on it a cam 19 which cooperates with one arm of a lever 20 which is supported between the cheeks 21 on the eye piece 17.
  • the lever 20 has pivoted to it at 92 the pressing tool 23. Further the lever 20 carries on an arm 24: a spring 25 fixed to a bracket 26 on the eye piece 17.
  • this device is as follows: hen the shaft 18 is rotated the cam 19 causes the pressing tool 223 to be withdrawn to the position shown in dotted lines at 23''. hen the pressing tool is in this position the distance piece and blade are inserted. The shaft 18 then rotates further until the finger on the lever 20 is released by the cam 15) so that the spring draws on the arm 24iand thereby brings the tool 23 sharply against the blade and distance piece. The tension of the spring 25 is suticient to cause the upsetting of the blade and distance piece and also to overcome the resistance applied to the shaft 12 by the covers 1 1. ()wing to the tool 23 being held firmly against the blade or distance piece by the spring 25, this spring pulls on the bracket- 26 and thereby rotates the shaft: 12 through a short distance. It will be understood that if desired the tool 23 might be moved by positive means against the blades and distance pieces for instance in the manner shown in Figs. 1 and 2.
  • a power hammer may be arranged in the manner shown in Figs. 84), to ope *ate on the blades to be fixed on the easing, the essential feature being that the power hammer as in (i and 7 is mechanically moved or guided toward and away from the work.
  • a device of the kind described for ti. ⁇ '- ing turbine blades and the like in their grooves on the blade carrying member comprising, a pressing tool movable in the groove, means for moving said tool substantially tangentially in the groove and means for applying a resistance to one of said re cited parts said resistance being overcome only at a pressure adequate to upset the part to be fastened in the groove substantially as described.
  • a device of the kind described for fixing turbine blades and the like in their grooves on the bladed member comprising, a power hammer having a stem fitting into the turbine groove, means for moving said power hammer and stem substantiallytangentially in said groove and means for applying a resistance to said bladed member to prevent said bladed member moving unforth.
  • a device of the kind described for fixing turbine blades and distance pieces in a blade carrying member of a turbine said member having grooves, comprlsing a rotatable shaft mounted parallel to the axis of said bladed member, a pin carried eccentrically by said shaft, a pressing tool mounted on said pin and reciprocating substantiallytangentially in the grooves of said bladed member and means for applying a brake to said bladed member.
  • a device of the kind described for fixing turbine blades and distance pieces in a blade carrying member of a turbine, said member having grooves comprising a rotatable shaft mounted parallel to the axis of said blade carrying member, a disk carried by said shaft, a pin eccentrically fixed on said disk, a pneumatic hammer mounted on said pin, a stem on said hammer movable in the grooves on the blade carrying member and a brake for said blade carrying member.
  • a device of the kind described for fixing turbine blades and distance pieces in a blade carrying member of a turbine, said member having grooves comprising a rotatable shaft mounted parallel to the axis of said blade carrying member, a coupling adapted to be placed in and out of operation in said shaft, a disk carried by said shaft, a pin eccentrically fixed on said disk, a pneumatic hammer mounted on said pin, a stem on said hammer movable in the grooves on the blade carrying member and a brake for said blade carrying member.

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

Description

J; DAFL.
DEVICE FOR FIXING TURBINE BLADES.
APPLICATION IILED J-AN. 12, 1909.
930,735. I PafentedA .0,1909.
3 SH SHEET -1.
Jy ijAHL. DEVICE FOR Pfxmu TURBINE BLADES.
APPLICATION FILED JAN. 12, 1909. 930,735, Patented Aug. 10, 1909.
3 SHEETS-SHEET 2.
W jimmmja/ mmzaw4 B. anmm co FNOYO-LFTHOGRAPHERS. wnsnmafou. a c.
J. DAHL. DEVICE FOR FIXING TURBINE BLADES.
APPLIUATION FILED JAN,12, 1909.
Patented Aug. 10, 1909.
3 SHEETS-SHEET 3.
wa /Ila @hmg: 04/ I g) [5/0 rng,
NIT ED srnras "ATE FFEQFZ.
.TOHANNES DAHL, OF' GROSS-FLOTTBEK, NEAR HAMBURG, GERMANY, ASSIGNOR TO BLOHM AND VOSS, COMMANDITGESELLSCHAFT AUF ACTIEN, OF HAMBURG, GERMANY, A
FIRM.
DEVICE FOR FTXING TURBINE-BLADES.
Patented Aug. 10, 1909.
Application filed January 121, 1909. Serial No. 471,885.
To all whom it may concern:
Be it known that I, JOHANNES DAHL, a citizen of the free town of Hamburg, and resident of GrossFlottbek, near the free town of Hamburg, Germany, engineer, have invented a new and useful Device for Fixing Turbine-Blades, of which the following is a specification.
This invention rela'testo a device for fixing turbine blades in their blade carrying members and its object is to provide a simple mechanical device for effecting thispurpose.
To this end the invention consists in a device comprising a pressing tool mechanically reciprocated in a substantially tangential direction in the groove of the bladed member and means for applying a resistance to the tool or the bladed member or the tool operating parts, this resistance being overcome only at a pressure which is adequate to upset the turbine blade root or distance piece within its retaining groove. \Vith this arrangement of device the turbine blades are all evenly set and upset within the groove so that no subsequent rectifying of the blades is necessary. Such rectifying has always been necessary when the turbine blades have been inserted and calked in place by hand. Further a very important effect obtained is that no side calking strip is required while at the same time I have found that a rectangular groove may be employed. The turbine blade roots and distance pieces fit loosely within this groove and are inserted by hand. The mechanically reciprocated pressing tool then upsets these turbine blade roots and distance pieces to cause them to grip tightly within their grooves. Experiments with a comparatively small size of blade have shown that with a fixing of this kind a force of 600 kg. was necessary to draw the blades from their carrying members and the finished crown of blades did not require any subsequent rectifying to bring them accurately into one plane.
The blades and distance pieces may be separately pressed into position or a blade and a distance piece or several blades and a corresponding number of distance pieces may be simultaneously pressed or upset within the groove. In the case of fixing blades on a drum, the drum is rotatably mounted and a brake or ratchet mechanism applied to prevent the rotation of the drum before the tool presses on the part to be fixed in the groove with a pressure sufiicient to upset the said part or parts. It will be understood that the shape of the grooves forms no importantpart of this invention as it may be applied to blade carrying grooves which are rectangular in shape or which are provided with undercut parts.
The invention is illustrated somewhat diagrammatically in the accompanying drawings, in which Figure 1 is a diagrammatic side view and F ig. 2 is a diagrammatic front elevation of a turbine drum showing the apparatus according to the present invention and illustrating its operation, Fig. 3 is an enlarged section of the turbine drum and blades, Fig. 4 is a front elevation and Fig. 5 is a plan of the same, Fig. 6 is a side elevation, and Fig. 7 is a plan of a modified form of the apparatus especially applicable to the insertion of large blades, Fig. 8 is a sectional elevation, Fig. 9 is a sectional side view and Fig. 10 a plan of a device suitable for fixing blades in a turbine casing according to the present invention.
In carrying the invention into elfect according to the form shown in Figs. 15 the turbine drum 25 having several grooves 25' therein is to be provided with blades 70 which are divided from one another by distance pieces g. The axis a of the drum is supported in bearings a and is provided with a brake b, the lever h of which is loaded by means of a weight g. Parallel to the axis of the drum there is supported a shaft to which at one end is provided with a disk carrying an eccentric pin 6. The eccentric pin 6 has pivoted to it a pressing or calking tool 8, the point of which fits in the grooves of the turbine drum and is adapted to press against the blades and distance pieces. These blades and distance pieces may be inserted in the groove by hand.
When the shaft w rotates the pressing tool is reciprocated in a substantially tangential direction between the positions 8 and s Fig. 3.. In the position 8' the blades 19 and distance pieces 9 are inserted. During the motion. from the position 8 to the position 8 these blades are firmly pressed by the tool .9. In consequence of the constant braking force exerted on the axis ofthe drum by the brake b, the pressure of the tool .9 is always the same and this pressure may be adjusted by adjusting the brake. In all cases the pressure of the tool 8 on the distance pieces must be suflicientto upset the blade root and distance piece. When this pressure is reached the drum 6 is caused to rotate through a short distance by the further motion of the tool 8. It will be seen that this further rotation is effected by overcoming the resistance which is applied to the drum by means of the brake and that this resistance is at least as great as the pressure necessary to upsetthe parts to be fixed in the groove.
When starting to insert a ring or crown of blades a wedge is inserted in the groove in the usual manner and the first blade butts against the wedge. W hen the crown of blades is almost completed a bent tool may be used for inserting a few of the last blades while the remaining blades are of course inserted by hand in the usual manner.
It will be understood that the resistance is preferably constant and that this constant resistance may be secured by various means. Further the resistance may be applied to the tool 8 or its moving mechanism. The invention also may be applied to blades fixed axially or radially.
According to the form shown in Figs. 6 and 7 the pressing tool 8 forms the stem of a pneumatic hammer 0 which is pivoted to the pin 0, mounted on a disk 0 The disk 0 is fixed to a driven shaft w. When this shaft rotates in the direction of the arrow in Fig. G-the stem 8 is moved in a substantially tangential direction to the turbine groove.
The method of fixing the parts 7) and (1 in this device is as follows: The axis a is braked for instance in the manner described with reference to Figs. 1 and 2. The pin a is moved at the rotation of the shaft in in the direction of the arrow to a point cl and during this time the parts 2) and g to be inserted are laid in the grooves. In the position 65 the rotation of the shaft to is stopped by throwing out a coupling w. The supply of air to the hammer c is then opened by the operator holding the handle 0 of the pneumatic hammer so that the stem 0 makes a series of impacts against the blade 2) or distance piece 9. The pneumatic hammer is then put out of operation and the shaft w allowed to rotate further. The pin 0 then moves from the point (Z to the point 0 and in this motion pushes the drum 6 one stage further against the braking action which is applied to the axis a. The resistance offered by the brake must be sutlicient to prevent the action of the pneumatic hammer causing rotation of the drum. The steady pressure applied from the point (Z to the point 0 finishes the upsetting of the blades and distance pieces 9 in the manner described above with reference to Fig. 1. This form of apparatus is specially suited for large blades and may be applied to the insertion of blades in either the turbine drum or casing.
In Figs. 8-10 T have shown a form of my invention specially applicable for use in the insertion of turbine blades in. a turbine casing. In this device the turbine casing 11 supports a shaft 12 in bearings 13. The upper cover 14- of the bearings 13 may be tightened down on the shaft 12 for the purpose of giving a braking action. The shaft 12 is provided with a feather way 15 in which a feather or spline 16 is adapted to slide. The spline 1G is carried by an eye 17. On this eye there is mounted a shaft 18 which may be driven by a motor through a flexible shaft. The shaft 18 has mounted on it a cam 19 which cooperates with one arm of a lever 20 which is supported between the cheeks 21 on the eye piece 17. The lever 20 has pivoted to it at 92 the pressing tool 23. Further the lever 20 carries on an arm 24: a spring 25 fixed to a bracket 26 on the eye piece 17.
The operation of this device is as follows: hen the shaft 18 is rotated the cam 19 causes the pressing tool 223 to be withdrawn to the position shown in dotted lines at 23''. hen the pressing tool is in this position the distance piece and blade are inserted. The shaft 18 then rotates further until the finger on the lever 20 is released by the cam 15) so that the spring draws on the arm 24iand thereby brings the tool 23 sharply against the blade and distance piece. The tension of the spring 25 is suticient to cause the upsetting of the blade and distance piece and also to overcome the resistance applied to the shaft 12 by the covers 1 1. ()wing to the tool 23 being held firmly against the blade or distance piece by the spring 25, this spring pulls on the bracket- 26 and thereby rotates the shaft: 12 through a short distance. It will be understood that if desired the tool 23 might be moved by positive means against the blades and distance pieces for instance in the manner shown in Figs. 1 and 2.
It will be understood that many modifications may be made in the device above described. Thus a power hammer may be arranged in the manner shown in Figs. 84), to ope *ate on the blades to be fixed on the easing, the essential feature being that the power hammer as in (i and 7 is mechanically moved or guided toward and away from the work.
I claim 1. A device of the kind described for ti.\'- ing turbine blades and the like in their grooves on the blade carrying member comprising, a pressing tool movable in the groove, means for moving said tool substantially tangentially in the groove and means for applying a resistance to one of said re cited parts said resistance being overcome only at a pressure adequate to upset the part to be fastened in the groove substantially as described.
2. A device of the kind described for fixing turbine blades and the like in their grooves on the bladed member comprising, a power hammer having a stem fitting into the turbine groove, means for moving said power hammer and stem substantiallytangentially in said groove and means for applying a resistance to said bladed member to prevent said bladed member moving unforth. I
4. A device of the kind described for fixing turbine blades and distance pieces in a blade carrying member of a turbine, said member having grooves, comprlsing a rotatable shaft mounted parallel to the axis of said bladed member, a pin carried eccentrically by said shaft, a pressing tool mounted on said pin and reciprocating substantiallytangentially in the grooves of said bladed member and means for applying a brake to said bladed member.
5. A device of the kind described for fixing turbine blades and distance pieces in a blade carrying member of a turbine, said member having grooves, comprising a rotatable shaft mounted parallel to the axis of said blade carrying member, a disk carried by said shaft, a pin eccentrically fixed on said disk, a pneumatic hammer mounted on said pin, a stem on said hammer movable in the grooves on the blade carrying member and a brake for said blade carrying member.
6. A device of the kind described for fixing turbine blades and distance pieces in a blade carrying member of a turbine, said member having grooves, comprising a rotatable shaft mounted parallel to the axis of said blade carrying member, a coupling adapted to be placed in and out of operation in said shaft, a disk carried by said shaft, a pin eccentrically fixed on said disk, a pneumatic hammer mounted on said pin, a stem on said hammer movable in the grooves on the blade carrying member and a brake for said blade carrying member.
In witness whereof I have hereunto set my hand in the presence of two witnesses.
JOHANNES DAHL.
Witnesses:
ERNEST H. L. MUMMENHOFF, Orr'ro W. HnLLMRIoH.
US47188509A 1909-01-12 1909-01-12 Device for fixing turbine-blades. Expired - Lifetime US930735A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4078290A (en) * 1976-11-08 1978-03-14 Nasa Stator rotor tools
US4096614A (en) * 1975-09-02 1978-06-27 General Electric Company Method and apparatus for removing stator vanes

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4096614A (en) * 1975-09-02 1978-06-27 General Electric Company Method and apparatus for removing stator vanes
US4078290A (en) * 1976-11-08 1978-03-14 Nasa Stator rotor tools

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