US1856820A - Elastic fluid turbine - Google Patents
Elastic fluid turbine Download PDFInfo
- 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
- Authority
- US
- 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
Links
- 239000012530 fluid Substances 0.000 title description 4
- 230000003534 oscillatory effect Effects 0.000 description 6
- 230000010355 oscillation Effects 0.000 description 5
- 239000011796 hollow space material Substances 0.000 description 4
- 230000033001 locomotion Effects 0.000 description 4
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 2
- 238000013016 damping Methods 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method 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
- F01D5/12—Blades
- F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/16—Form or construction for counteracting blade vibration
-
- 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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/24—Blade-to-blade connections, e.g. for damping vibrations using wire or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/50—Building or constructing in particular ways
- F05D2230/51—Building or constructing in particular ways in a modular way, e.g. using several identical or complementary parts or features
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/231—Three-dimensional prismatic cylindrical
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/24—Three-dimensional ellipsoidal
- F05D2250/241—Three-dimensional ellipsoidal spherical
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/50—Vibration 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.
Landscapes
- 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.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US540684A US1856820A (en) | 1931-05-28 | 1931-05-28 | Elastic fluid turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US540684A US1856820A (en) | 1931-05-28 | 1931-05-28 | Elastic fluid turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1856820A true US1856820A (en) | 1932-05-03 |
Family
ID=24156511
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US540684A Expired - Lifetime US1856820A (en) | 1931-05-28 | 1931-05-28 | Elastic fluid turbine |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1856820A (en) |
Cited By (6)
| 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 |
-
1931
- 1931-05-28 US US540684A patent/US1856820A/en not_active Expired - Lifetime
Cited By (6)
| 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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