US791743A - Elastic-fluid turbine. - Google Patents

Elastic-fluid turbine. Download PDF

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Publication number
US791743A
US791743A US25082005A US1905250820A US791743A US 791743 A US791743 A US 791743A US 25082005 A US25082005 A US 25082005A US 1905250820 A US1905250820 A US 1905250820A US 791743 A US791743 A US 791743A
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Prior art keywords
blades
vanes
strip
binding
elastic
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US25082005A
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Edwin E Arnold
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Westinghouse Machine Co
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Westinghouse Machine Co
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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
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/24Blade-to-blade connections, e.g. for damping vibrations using wire or the like

Definitions

  • This invention relates to elastic-fluid turbines, and more particularly to tying or binding means for the blades or vanes thereof.
  • Fig. 3 is a fragmentary view similar to Fig. 1 and illustrates the method and means of caring for the blades or vanes adjacent to the ends of the binder wires or strips which are utilized.
  • Fig. 4 is a modificatlon of this method of caring for the blades therefor, the blades or vanes may be of a'ny desired contour in cross-section, of any desired length, or formed of any desired material in any desired manner.
  • the blades or vanes may be secured to the rotors or stators in any desired manner; but they are preferably secured to their holding member-that is, either the rotors or stators-as illustrated and described in said -Letters Patent No. 639,608..
  • the rotor or stator member which may be represented by 6, is provided with an annular or circumferentially-extending slot or channel, within which the inner ends of the blades or vanes 7 are secured by means of calling or spacing elements or pieces 8, as is now common.
  • Each of the blades atits outer end, as at 9, is rovided with an elongated or rectangular hol)e or opening through which is inserted 4'a binding-strip 10, having a rectangular or ⁇ elongated cross-section.
  • the holes or slots in the blades or vanes are so formed that the long sides of the binder-strip at its portion lyinoP within the same will be substantially parallel to the edges of the blades or vanes.
  • this binding-strip may be cut into lengths sufficient to embrace onlyafew blades or vanes, or it may extend through an entire row.
  • the strip l0 is inserted through the holes 9. After the strip is in position and the blades or vanes are locked to their carrying member it is distorted or twisted, as shown in the drawings. This distortion of the binding-strip locks the blades or vanes together and secures them against movement toward or away from one another circumferentially, as well as against movement out of the plane of the row.
  • a joint between two groups of blades is shown.
  • the ends of the bindingstrips 10 terminate between adjacent blades or vanes, as at 14, and both ends are distorted or twisted.
  • Fig. 4 a modification of the expansionjoint is shown.
  • the ends of the primary binding-strjps l0 terminate at either side of an interme iate blade or vane, and a supplemental binding-strip, which extends through the holes 11, as described, is distorted on either side of the intermediate blade or vane.
  • this method secures the blades or vanes against lateral motion.
  • the distorting or twisting of the binding-strip may be accomplished in various ways and that any method will fall within the scope of this invention in which the outer ends of a plurality of blades or vanes are locked together by means of a locking or binding strip which is elongated or rectangular in cross-section and which between adjacent blades and vanes is distorted.
  • annular row of blades or vanes and means for preventing relative movement of said blades or vanes consisting of a binder-strip of elongated cross-section which asses through substantially alined holes tierein and which between adjacent blades or vanes is distorted.
  • a plurality of blades or vanes arranged in an annular row, -and a locking-strip oi elongated cross-section passing through the outer ends of said blades or vanes and which, between adjacent blades or vanes, is distorted.

Description

UNITED STATES Patented J une 6, 1905.
PATENT OEEICE.
EDWIN E. ARNOLD, WIILKINSBIIRG, PENNSYLVANIA, ASSIGN OR TO THE WESTINGI-IOUSE MACHINE COMPANY, A CORPORATION OF PENNSYLVANIA.
ELAsvrlc-FLUID TURBINE.
SPECIFICATION forming part of VLetters Patent No. 791,743, dated June 6, 1905. Application filed March 18, 1905. Serial No. 250,820.
To a/ZZ whom it may concern.-
Be it known that I, EDWIN EL ARNOLD, a citizen of the United States, and a resident of Wilkinsburg, in the county of Allegheny and State of Pennsylvania, have invented a new and useful Im rovement in Elastic-Fluid Turbines, of v.y ich the following is a specification.
This invention relates to elastic-fluid turbines, and more particularly to tying or binding means for the blades or vanes thereof.
It is now common in elastic-Huid turbines in which the vanes and blades thereof are arranged in annularly-,extending rows to secure the outer ends of the blades or vanes comprised in one such row together, and, as shown by Patent N o. 689,608 of December 19, 1899, attempts have been made to this end by soldering or brazing the blades comprised in a row to a binder strip or wire assing through openings therefor in said b ades or vanes. In practice it has been found that the results secured by the method described and illustrated'in said patent are not as satisfactory as might be desired and to the end of reducin the cost of manufacture by reducing botli the cost ofllabor and material, to the securing of a stronger construction, as well as numerous other results, which will readily appear to one skilled in the art to which this invention ertains, my invention consists in the method hereinafter described and the means illustrated in the drawings accompanyinfr this application and forming al part thereo In the drawings, Figure 1 is a view in side elevation of a plurality of turbine blades or vanes, the outer or free ends of which are shown bound or tied together by my method. Fig. 2 is a plan view of the said blades or vanes, showing the arrangement of the binding member. Fig. 3 is a fragmentary view similar to Fig. 1 and illustrates the method and means of caring for the blades or vanes adjacent to the ends of the binder wires or strips which are utilized. Fig. 4 is a modificatlon of this method of caring for the blades therefor, the blades or vanes may be of a'ny desired contour in cross-section, of any desired length, or formed of any desired material in any desired manner. vThe blades or vanes may be secured to the rotors or stators in any desired manner; but they are preferably secured to their holding member-that is, either the rotors or stators-as illustrated and described in said -Letters Patent No. 639,608.. Y
As illustrated in the drawings, the rotor or stator member, which may be represented by 6, is provided with an annular or circumferentially-extending slot or channel, within which the inner ends of the blades or vanes 7 are secured by means of calling or spacing elements or pieces 8, as is now common.
For the sake of clearly describing this method lit willbe understood that the side walls of these channels or slots are roughened or undercut and that by means of suitable calkingirons or other tools the spacing pieces or blocks Spare caused to spread transversely to the applied pressure and to grip the walls of the channels and the vanes or blades, whereby said vanes or blades are securely held to the stator or rotor, as the case may be.
Each of the blades atits outer end, as at 9, is rovided with an elongated or rectangular hol)e or opening through which is inserted 4'a binding-strip 10, having a rectangular or` elongated cross-section. The holes or slots in the blades or vanes are so formed that the long sides of the binder-strip at its portion lyinoP within the same will be substantially parallel to the edges of the blades or vanes. If desired, this binding-strip may be cut into lengths sufficient to embrace onlyafew blades or vanes, or it may extend through an entire row.
After the blades have been secured to the rotor and the vanes to the stator, or during the operation of mounting them, the strip l0 is inserted through the holes 9. After the strip is in position and the blades or vanes are locked to their carrying member it is distorted or twisted, as shown in the drawings. This distortion of the binding-strip locks the blades or vanes together and secures them against movement toward or away from one another circumferentially, as well as against movement out of the plane of the row.
In Fig. 3 a joint between two groups of blades is shown. The ends of the bindingstrips 10 terminate between adjacent blades or vanes, as at 14, and both ends are distorted or twisted. Extending through a second series of holes or openings 11, provided in several of the blades below the holes or openings 9, is another binding strip or member l2, and between the blades or vanes adjacent to the ends of the binder strip or wire l0 this supplemental binding-strip is distorted or twisted, as shown in Fig. 3. By this method it will be seen that the two blades or vanes adjacent to the separated ends of the primary binder-strip l() may be prevented from moving laterally out of the plane of the row, and an expansion-joint is provided between the adjacent groups ol. blades or vanes.
In Fig. 4 a modification of the expansionjoint is shown. The ends of the primary binding-strjps l0 terminate at either side of an interme iate blade or vane, and a supplemental binding-strip, which extends through the holes 11, as described, is distorted on either side of the intermediate blade or vane. As in the previous case, this method secures the blades or vanes against lateral motion.
It will be seen that the distorting or twisting of the binding-strip may be accomplished in various ways and that any method will fall within the scope of this invention in which the outer ends of a plurality of blades or vanes are locked together by means of a locking or binding strip which is elongated or rectangular in cross-section and which between adjacent blades and vanes is distorted.
Having thus described my invention, what I claim as new and useful, and desire to secure by Letters Patent, is-.
l. In combination with an annular row of turbine blades or vanes, a locking-strip elongated in cross-section passing through said blades or vanes and which between adjacent blades or vanes is distorted.
2. In a turbine, an annular row oi' blades or vanes and a rectangular binding-strip passing through substantially alined holes therein and which between adjacent blades or vanes is distorted.
3. In a turbine, an annular row of blades or vanes and means for preventing relative movement of said blades or vanes consisting of a binder-strip of elongated cross-section which asses through substantially alined holes tierein and which between adjacent blades or vanes is distorted.
4. In combination with a turbine blade or vane holding element, a plurality of blades or vanes arranged in an annular row, and a rectangular locking-stri) )assing through the outer ends of said b a( es or vanes and which, between adjacent blades or vanes, is distorted.
5. In combination with a turbine blade or vane holding element, a plurality of blades or vanes arranged in an annular row, -and a locking-strip oi elongated cross-section passing through the outer ends of said blades or vanes and which, between adjacent blades or vanes, is distorted.
In testimony whereof I have hereunto subscribed my name this 16th day ol March, 1905.
E. E. ARNOLD.
Witnesses:
DAVID VVILLIAns, JNO. S. GREEN.
US25082005A 1905-03-18 1905-03-18 Elastic-fluid turbine. Expired - Lifetime US791743A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2914299A (en) * 1954-02-05 1959-11-24 Gen Electric Co Ltd Steam turbines
US20110274549A1 (en) * 2010-05-06 2011-11-10 General Electric Company Blade having asymmetrical mid-span structure portions and related bladed wheel structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2914299A (en) * 1954-02-05 1959-11-24 Gen Electric Co Ltd Steam turbines
US20110274549A1 (en) * 2010-05-06 2011-11-10 General Electric Company Blade having asymmetrical mid-span structure portions and related bladed wheel structure

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