US1856820A - Elastic fluid turbine - Google Patents

Elastic fluid turbine Download PDF

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Publication number
US1856820A
US1856820A US540684A US54068431A US1856820A US 1856820 A US1856820 A US 1856820A US 540684 A US540684 A US 540684A US 54068431 A US54068431 A US 54068431A US 1856820 A US1856820 A US 1856820A
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United States
Prior art keywords
buckets
wire
elastic fluid
passages
fluid turbine
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
Application number
US540684A
Inventor
Ernest L Robinson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US540684A priority Critical patent/US1856820A/en
Application granted granted Critical
Publication of US1856820A publication Critical patent/US1856820A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F01D5/26Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • 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
    • F01D5/14Form or construction
    • F01D5/16Form or construction for counteracting blade vibration
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/50Building or constructing in particular ways
    • F05D2230/51Building or constructing in particular ways in a modular way, e.g. using several identical or complementary parts or features
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/23Three-dimensional prismatic
    • F05D2250/231Three-dimensional prismatic cylindrical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/24Three-dimensional ellipsoidal
    • F05D2250/241Three-dimensional ellipsoidal spherical
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/50Vibration damping features

Definitions

  • the present invention relates to elastic fluid turbines and particularly to rotors of such turbines.
  • the object of my invention consists in an improved arrangement for stiffening such bucket wheels and damping vibrations thereof.
  • the hollow space of such wire is nearly filled, according to my invention, with a free- 1y movable means, for instance, short rods or balls which are adapted to cause impact against and friction with the walls of the wire to the effect that undesirable oscillatory movements of the bucket blades of such wheels are considerably diminished.
  • a free- 1y movable means for instance, short rods or balls which are adapted to cause impact against and friction with the walls of the wire to the effect that undesirable oscillatory movements of the bucket blades of such wheels are considerably diminished.
  • Fig. 1 is a side view of a portion of a turbine rotor, embodying my invention
  • Fig. 2 is a radial sectional view of Fig. 1
  • Fig. 3 is a detailed view on a larger scale
  • Fig. 4 illustrates amodification of the parts shown in Fig. 3.
  • 1 indicates a turbine shaft, 2 a rotor thereon, 3 a row of buckets carried by the rotor and a a sectional bucket cover for the buckets.
  • hollow wires 5 and 6 are provided between the buckets extending through passa es 7 and 8 of said buckets and preferably fastened to said buckets by any suitable separately with respect to different sections of the wheel wherebythe open ends of the wires have to beclosed by any'suitable means, for instance by-brazed plugs, not shown in the drawings.
  • any suitable separately with respect to different sections of the wheel wherebythe open ends of the wires have to beclosed by any'suitable means, for instance by-brazed plugs, not shown in the drawings.
  • rodlike members I mayprovi'de balls'10 as indicated in Fig. 4, or any other suitable means 'which'is-capable of causing sufficient impact against and frictional resistance with the inner walls of the wire.
  • the movable members rattle about within said wire, that is, they roll back and forth or move sidewardly so as to hit one another on the walls of the wire thus causing impact and frictional resistance to absorb the oscillatory energy of the buckets, thereby preventing the building up of excessive amplitude of vibration with correspondingly destructive stresses.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Vibration Dampers (AREA)

Description

y 1932- E. L. ROBINSON 1,856,820
ELASTIC FLUID TURBINE Filed May 28. 1931 Fig. 2.
Inventor:
bg His Abbor'neg.
Ernest. LRobihsofi,
Patented May 3, 1932 UNITED STATES PATENT OFFICE I ERNEST L. ROBINSON, on SGHENECTADY, NEW YORK, ASSIGNOR T GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK ELASTIC FLUID TURBINE Application filed May 28, 1931. Serial No. 540;'684.
The present invention relates to elastic fluid turbines and particularly to rotors of such turbines.
It is known to those skilled in the art that the bucket wheels are subjected to oscillations during the operation of the turbine.
These oscillations very often cause damage to the buckets, particularly of those of the lower stages, in view of their considerable diameter. It has been proposed heretofore to stiffen the bucket wheels of turbines and to absorb their oscillatory energy by the provision of wires extending through passages in the buckets.
The object of my invention consists in an improved arrangement for stiffening such bucket wheels and damping vibrations thereof.
This is achieved according to my invention by the provision of a hollow Wirelike member extending through passages in the buckets and preferably fastened to said buckets.
The hollow space of such wire is nearly filled, according to my invention, with a free- 1y movable means, for instance, short rods or balls which are adapted to cause impact against and friction with the walls of the wire to the effect that undesirable oscillatory movements of the bucket blades of such wheels are considerably diminished.
For a better understanding of what I believe to be novel and my invention, attention is directed to the following description and claims in connection with the drawings appended hereto.
In the drawings, Fig. 1 is a side view of a portion of a turbine rotor, embodying my invention; Fig. 2 is a radial sectional view of Fig. 1; Fig. 3 is a detailed view on a larger scale and Fig. 4 illustrates amodification of the parts shown in Fig. 3.
Referring to the drawings, 1 indicates a turbine shaft, 2 a rotor thereon, 3 a row of buckets carried by the rotor and a a sectional bucket cover for the buckets. According to my invention, as shown in the present instance, hollow wires 5 and 6 are provided between the buckets extending through passa es 7 and 8 of said buckets and preferably fastened to said buckets by any suitable separately with respect to different sections of the wheel wherebythe open ends of the wires have to beclosed by any'suitable means, for instance by-brazed plugs, not shown in the drawings. Inside of the wireI may. provide short sections of wire or other xro'dlike members 9 having small radialand axial clearance and being freely movable within the hollow wire as shown in Fig. 3. Instead of rodlike members I mayprovi'de balls'10 as indicated in Fig. 4, or any other suitable means 'which'is-capable of causing sufficient impact against and frictional resistance with the inner walls of the wire.
During oscillations of the bucket wheels the movable members rattle about within said wire, that is, they roll back and forth or move sidewardly so as to hit one another on the walls of the wire thus causing impact and frictional resistance to absorb the oscillatory energy of the buckets, thereby preventing the building up of excessive amplitude of vibration with correspondingly destructive stresses.
Thus, it will be seen that my improved arrangement for stiffening bucket wheels and dampening oscillations thereof is equally effective with respect to Oscillations of any kind, particularly in any direction.
In accordance with the provisions of the patent statutes I have described the method of operation of my invention, together with the apparatus which I now consider to represent the best embodiment thereof, but I desire to have it understood that the apparatus shown is only illustrative and that the invention may be carried out by other means.
N hat I claim as new and desire to secure by Letters Patent of the United States, is:
1. The combination with a turbine rotor having a row of buckets, of a tubelike member extending through passages in said buckets, and means provided within the hollow space of said tubelike member, said means being freely movable within said spaces whereby it is adapted to dampen vibration of said buckets.
2. The combination with a turbine rotor having a row of buckets provided with passages which are arranged concentrically with the axis of said rotor, of a. hollow wire extending through said passages, and short sections of wire provided within the hollow space of said wire which are freely movable to cause dampening of oscillatory movements of said buckets.
3. The combination with a turbine rotor having a row of buckets provided with passages, of a hollow wire extending through said passages and fastened to said buckets, and balls provided within the hollow space of said wire and adapted to dampen oscillatory movements of said buckets.
4c. The combination with a turbine rotor having a row of buckets provided with passages, of a continuous hollow wire extending through said passages and fastened to said buckets and having its ends connected to each other, freely movable members provided within said wire to cause impact between each other or against the inner wall of said Wire and frictional resistance within said wire whereby the oscillatory energy of said buckets is absorbed by the relative move ments of said members.
ERNEST L. ROBINSON.
US540684A 1931-05-28 1931-05-28 Elastic fluid turbine Expired - Lifetime US1856820A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2771240A (en) * 1952-08-27 1956-11-20 Peter J Gurin Automatic dynamic balancer
US2862686A (en) * 1954-08-19 1958-12-02 Thompson Prod Inc Hollow vane with internal vibration dampener
US2999669A (en) * 1958-11-21 1961-09-12 Westinghouse Electric Corp Damping apparatus
US4662824A (en) * 1984-10-01 1987-05-05 Ortolano Ralph J Sleeve connectors for turbines
US6547526B2 (en) * 2001-03-05 2003-04-15 The Boeing Company Article having dampening member installed into an imbedded cavity
EP2573327A1 (en) * 2011-09-20 2013-03-27 Siemens Aktiengesellschaft Damping wire, corresponding rotor blade stage, steam turbine and producing method

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2771240A (en) * 1952-08-27 1956-11-20 Peter J Gurin Automatic dynamic balancer
US2862686A (en) * 1954-08-19 1958-12-02 Thompson Prod Inc Hollow vane with internal vibration dampener
US2999669A (en) * 1958-11-21 1961-09-12 Westinghouse Electric Corp Damping apparatus
US4662824A (en) * 1984-10-01 1987-05-05 Ortolano Ralph J Sleeve connectors for turbines
US6547526B2 (en) * 2001-03-05 2003-04-15 The Boeing Company Article having dampening member installed into an imbedded cavity
EP2573327A1 (en) * 2011-09-20 2013-03-27 Siemens Aktiengesellschaft Damping wire, corresponding rotor blade stage, steam turbine and producing method

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