US950803A - Blading for elastic-fluid turbines. - Google Patents
Blading for elastic-fluid turbines. Download PDFInfo
- Publication number
- US950803A US950803A US44722808A US1908447228A US950803A US 950803 A US950803 A US 950803A US 44722808 A US44722808 A US 44722808A US 1908447228 A US1908447228 A US 1908447228A US 950803 A US950803 A US 950803A
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- US
- United States
- Prior art keywords
- blades
- strip
- blade
- strips
- blading
- 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
Links
- 239000012530 fluid Substances 0.000 title description 3
- 150000001875 compounds Chemical class 0.000 description 6
- 238000005452 bending Methods 0.000 description 2
- 239000012634 fragment Substances 0.000 description 2
- 238000010008 shearing Methods 0.000 description 2
- 244000191502 Chenopodium murale Species 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
Images
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
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
- F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
Definitions
- This invention relates to elastic fluid turbines, and more particularly to blading means for such turbines.
- An object of my invention is the production or" simple and effective means for assembling turbine blades into blade segments.
- Fig ure 1 is a f'agmental longitudinal section of a blade-carrying element of a turbine and illustrates an embodiment of my invention
- Fig. 2 is a section along the line A.-A of Fig. 1 and discloses a section of a rotating blade-carrying element in connection with blades shown partially in section and partially in elevation and mounted in accordance with my invention
- Fig. 3 is a plan view of a fragment of a rotating bladecarrying element with blades mounted in ac- :ordance with my invention
- Fig. 1 is a fragments section of a stationary bladecarrying element in connection with blades shown in section.
- the blademounting element 5 is provided with undercut grooves 6 in each of which a segmental blade ring is secured by component wedges 8.
- Each blade ring is composed of blades 12, the bases of which are secured to a segmental base strip 9, each of which is com-. posed of two strips 10.
- Each strip 10 is curved to conform to the curvature of the Specification of Letters Patent.
- blade mounting slot and is provided, across one face, with radially extending notches 11 so arranged and spaced that the notches in one strip cooperate with the adjacentnotches in the other strip in securing the roots or bases of the blades 12 in place.
- the bases of the blades 12 are swaged or otherwise formed so as to more nearly fit the notches provided for their reception in the blade mounting strips.
- Each blade is also provided with a round hole 13, which extends transversely through its base and through which a cylindrical wire 14 ex tends.
- a slot 15 of semi-circular section is provided in each strip 10 and, extending longitudinally oi the strip, intersects the notches 11 of the strip. The slot 15 of one strip cooperates with the slot 15 of the cooperating strip in receiving and securing in place the wire let.
- One lateral. wall of one of the strips 10, comprised in each compound base strip, is inclined to correspond to the inclination of the undercut walls of the mounting grooves 6.
- the corresponding wall of the other strip is vertical.
- the outer end of each blade provided with a hole 16 which is comma-shaped in crosssection, and through which a wire 17 of comma-shaped cross-section is adapted to extend.
- the blades are first threaded onto the locking wire 14:, which, as has been said, is adapted to extend through the holes 13, and then on the binding wire 17 which is adapted to extend through the holes 16.
- the blades are then spaced along the wires and introduced into the notches 11 of one of the component strips of the base strip 7.
- the blades 12 and the wire 14 are then locked in place within the ring by bringing the notches 11 of the other strip of the base strip into en gagement with the projecting portions of the bases of the blades.
- the two strips are then secured together by means of rivets 18 which are suitably spaced along the ring and located in countersunk holes extending through the strips. The rivets draw the component strips of each base strip together so that the bases of the blades are firmly clamped between them.
- the outer or free ends of the blades, se cured to a base strip, are properly spaced and rigidly secured in their relative posi tions by shearing, adjacent to and on each side of each blade, and bending over, between adjacent blades, a longitudinally extending rib 19 which is formed on the binding wire 17.
- the shearing and bending over of the rib 19 forms separate spacing pieces between adjacent blades which positively lock the blades in their relative positions, and the body portion of the wire 17 acts as a binding wire in holding the separate pieces together and securing the outer ends of the blades together.
- the base strips may be cut to convenient lengths and these secured into the blademounting grooves by any suitable means, but I preferably employ the compound ta pered wedges 8.
- the base strips 7 are so introduced into their mounting groove 6 that their inclined faces contact with one of the undercut walls of the groove.
- the compound tapered wedges 8 are then introduced into the groove between the vertical face of the blade-mounting ring and the other undercut wall of the groove.
- the wedges are arranged in pairs and the two wedges of each pair are so constructed that, when driven home, one beside the other, they form a wedgeshaped key which is efiective in securing the blade-mounting ring in the blademounting groove and which is prevented, by its shape and the shape of its component wedges, from being dislodged from the ing force.
- Thesegments of each ring are so arranged at their ends that they may be located in the blade-mounting grooves end for end without destroying the spacing of the blades.
- Anumber of pairs of wedges are employed to secure each segmentof the ring in a groove, and are preferably so spaced within the grooves that the component wedges of the one pair abut against the corresponding component wedges of the adjacent pairs. Such an arrangement prevents any possibility of the wedges becoming displaced or loosened in the grooves.
- the first and last pairs of wedges introduced into each groove are in some suitable way locked against longitudinal motion and thereby permanently secured into the groove.
- blade in its broadest sense, that is, to include both the rotating and the stationary blades, vanes or buckets of a turbine
- blade-carrying element in its broadest sense, that is, to mean the rotating or i I l i 1 stationary blade or bucket carrying element of a turbine.
- a compound base strip adapted to receive the bases of the blades, and means located between the sepaate parts of said strip extending longitudinally thereof and through holes provided in the blades for positively locking said blades to said strip.
- a compound base strip comprising two separate strips each provided with a plurality of blade-receiving notches and a locking piece extending longitudinally of said strip for positively locking said blades thereto.
- a base strip formed in separate parts and adapted to receive said blades, and means extending through holes provided. in the bases of said blades for positively locking said blades to said strip.
- a blade strip formed in separate groove by centrifugal or any other dislodgparts and adapted to receive said blades between the separate parts and a locking member extending through the blades and secured in place by said strip.
- a base strip comprising two separate strips provided with cooperating notches adapted to receive the bases of blades, a locking member extending through holes provided in the bases of the blades and secured in place between said strips, and means for permanently securing said strips together.
- a segmental blade mounting ring comprising two strips provided with cooperating notches for receiving the bases of said blades and a locking wire secured in place between said strips and extending through holes provided in the bases of said blades.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
J. S. GREEN.
BLADING FOR ELASTIC FLUID TURBINES.
APPLICATION FILED AUG. 6, 190B.
Patented Mar. 1, 19110.
[N VE 1V TOR ll A'Tlldd Th idlt hl 15 MB. Q
JONATHAN S. GREEN, 01 PIT'TSBURG, PENNSYLVANIA, ASSIGNOR TO THE WESTING- HOUSE MACHINE COIVIPANY, A CORPORATION OF PENNSYLVANIA.
BLAJJING FOR ELASTIC-FLUIID TURBINES.
To all whom it may concern:
Be it known that 1', JONATHAN S. GREEN, a citizen of the United. States, and a resident of Pittsburg, in the county of Allegheny and State of Pennsylvania, have made a new and useful Invention in Blading Means for Elastic-Fluid Turbines, of which the following is a specification.
This invention relates to elastic fluid turbines, and more particularly to blading means for such turbines.
An object of my invention is the production or" simple and effective means for assembling turbine blades into blade segments.
In the drawings accompanying this application and forming a part thereof: Fig ure 1 is a f'agmental longitudinal section of a blade-carrying element of a turbine and illustrates an embodiment of my invention; Fig. 2 is a section along the line A.-A of Fig. 1 and discloses a section of a rotating blade-carrying element in connection with blades shown partially in section and partially in elevation and mounted in accordance with my invention; Fig. 3 is a plan view of a fragment of a rotating bladecarrying element with blades mounted in ac- :ordance with my invention; and Fig. 1 is a fragments section of a stationary bladecarrying element in connection with blades shown in section.
In carrying out my invention I contemplate assembling the turbine blades into a segmental blade ring and I accomplish this by providing a compound base strip for the blades, which is composed of two sep arate strips. Each separate strip is notched to receive the blades and one strip cooperates with the other and with a locking wire which extends through holes provided in the blades, in positively securing the blades in place. I also provide means for permanently securing the separate strips of each base strip together and thereby permanently lock the blades in place.
Referring to the drawings: the blademounting element 5 is provided with undercut grooves 6 in each of which a segmental blade ring is secured by component wedges 8. Each blade ring is composed of blades 12, the bases of which are secured to a segmental base strip 9, each of which is com-. posed of two strips 10. Each strip 10 is curved to conform to the curvature of the Specification of Letters Patent.
Application filed August 6, 1908.
Patented Mar. 1, 1916. Serial No. 447,228.
blade mounting slot and is provided, across one face, with radially extending notches 11 so arranged and spaced that the notches in one strip cooperate with the adjacentnotches in the other strip in securing the roots or bases of the blades 12 in place. The bases of the blades 12 are swaged or otherwise formed so as to more nearly fit the notches provided for their reception in the blade mounting strips. Each blade is also provided with a round hole 13, which extends transversely through its base and through which a cylindrical wire 14 ex tends. A slot 15 of semi-circular section is provided in each strip 10 and, extending longitudinally oi the strip, intersects the notches 11 of the strip. The slot 15 of one strip cooperates with the slot 15 of the cooperating strip in receiving and securing in place the wire let. One lateral. wall of one of the strips 10, comprised in each compound base strip, is inclined to correspond to the inclination of the undercut walls of the mounting grooves 6. The corresponding wall of the other strip is vertical. The outer end of each blade provided with a hole 16 which is comma-shaped in crosssection, and through which a wire 17 of comma-shaped cross-section is adapted to extend.
In assembling the blades and base strips into segmental blade rings, the blades are first threaded onto the locking wire 14:, which, as has been said, is adapted to extend through the holes 13, and then on the binding wire 17 which is adapted to extend through the holes 16. The blades are then spaced along the wires and introduced into the notches 11 of one of the component strips of the base strip 7. The blades 12 and the wire 14 are then locked in place within the ring by bringing the notches 11 of the other strip of the base strip into en gagement with the projecting portions of the bases of the blades. The two strips are then secured together by means of rivets 18 which are suitably spaced along the ring and located in countersunk holes extending through the strips. The rivets draw the component strips of each base strip together so that the bases of the blades are firmly clamped between them.
The outer or free ends of the blades, se cured to a base strip, are properly spaced and rigidly secured in their relative posi tions by shearing, adjacent to and on each side of each blade, and bending over, between adjacent blades, a longitudinally extending rib 19 which is formed on the binding wire 17. The shearing and bending over of the rib 19 forms separate spacing pieces between adjacent blades which positively lock the blades in their relative positions, and the body portion of the wire 17 acts as a binding wire in holding the separate pieces together and securing the outer ends of the blades together.
The base strips may be cut to convenient lengths and these secured into the blademounting grooves by any suitable means, but I preferably employ the compound ta pered wedges 8. The base strips 7 are so introduced into their mounting groove 6 that their inclined faces contact with one of the undercut walls of the groove. The compound tapered wedges 8 are then introduced into the groove between the vertical face of the blade-mounting ring and the other undercut wall of the groove. The wedges are arranged in pairs and the two wedges of each pair are so constructed that, when driven home, one beside the other, they form a wedgeshaped key which is efiective in securing the blade-mounting ring in the blademounting groove and which is prevented, by its shape and the shape of its component wedges, from being dislodged from the ing force. Thesegments of each ring are so arranged at their ends that they may be located in the blade-mounting grooves end for end without destroying the spacing of the blades. Anumber of pairs of wedges are employed to secure each segmentof the ring in a groove, and are preferably so spaced within the grooves that the component wedges of the one pair abut against the corresponding component wedges of the adjacent pairs. Such an arrangement prevents any possibility of the wedges becoming displaced or loosened in the grooves. The first and last pairs of wedges introduced into each groove are in some suitable way locked against longitudinal motion and thereby permanently secured into the groove.
Throughout the specification and claims I have utilized the word blade in its broadest sense, that is, to include both the rotating and the stationary blades, vanes or buckets of a turbine, and I have also employed the term blade-carrying element in its broadest sense, that is, to mean the rotating or i I l i 1 stationary blade or bucket carrying element of a turbine.
I11 accordance with the provisions of the patent statutes, I have described the principle of my invention, together with the apparatus which I now consider to representthe best embodiment thereof, but I desire to have it understood that the apparatus shown is only illustrative and that the iitvention can be carried out by other means.
hat. I claim is:
1. In combination with a plurality of blades, a compound base strip adapted to receive the bases of the blades, and means located between the sepaate parts of said strip extending longitudinally thereof and through holes provided in the blades for positively locking said blades to said strip.
2. In combination with a plurality of blades, a compound base strip comprising two separate strips each provided with a plurality of blade-receiving notches and a locking piece extending longitudinally of said strip for positively locking said blades thereto.
3. In combination with a plurality of blades, a base strip formed in separate parts and adapted to receive said blades, and means extending through holes provided. in the bases of said blades for positively locking said blades to said strip.
4-. In combination with a plurality of blades, a blade strip formed in separate groove by centrifugal or any other dislodgparts and adapted to receive said blades between the separate parts and a locking member extending through the blades and secured in place by said strip.
5. A base strip comprising two separate strips provided with cooperating notches adapted to receive the bases of blades, a locking member extending through holes provided in the bases of the blades and secured in place between said strips, and means for permanently securing said strips together.
(3. In combination with a plurality of blades, a segmental blade mounting ring comprising two strips provided with cooperating notches for receiving the bases of said blades and a locking wire secured in place between said strips and extending through holes provided in the bases of said blades.
In testimony whereof, I have hereunto subscribed my name this 4th day of August. 1908.
JNO. S. GREEN.
IVitnesses BIRNEY Hixas, G120. IV. \Vamten.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US44722808A US950803A (en) | 1908-08-06 | 1908-08-06 | Blading for elastic-fluid turbines. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US44722808A US950803A (en) | 1908-08-06 | 1908-08-06 | Blading for elastic-fluid turbines. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US950803A true US950803A (en) | 1910-03-01 |
Family
ID=3019216
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US44722808A Expired - Lifetime US950803A (en) | 1908-08-06 | 1908-08-06 | Blading for elastic-fluid turbines. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US950803A (en) |
-
1908
- 1908-08-06 US US44722808A patent/US950803A/en not_active Expired - Lifetime
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