US1858067A - Elastic fluid turbine - Google Patents
Elastic fluid turbine Download PDFInfo
- Publication number
- US1858067A US1858067A US490232A US49023230A US1858067A US 1858067 A US1858067 A US 1858067A US 490232 A US490232 A US 490232A US 49023230 A US49023230 A US 49023230A US 1858067 A US1858067 A US 1858067A
- Authority
- US
- United States
- Prior art keywords
- buckets
- tie wire
- tie
- wire
- elastic fluid
- 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
- 238000005452 bending Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 2
- 230000003534 oscillatory effect Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 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
- F01D5/22—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
Definitions
- invention relates to elastic and especially to rotors for ing tie wires between the inner and outer ends 0 of the buckets to strengthen the buckets and increase their stifiness.
- My invention relates especially to tie wires for turbine buckets, and has for its object to provide an improved tie wire construction and arrangement.
- Fig. 1 is a side View of a portion of a turbine rotor, the buckets of which are provided with tie wires embodying my invention
- Fig. 2 is a radial sectional view
- Fig. 3 is a detail view on a larger scale illustrating in somewhat exaggerated form the operation of the tie wire.
- 1 indicates a turbine shaft, 2 a rotor thereon, 3 a row of buckets carried by the rotor, and at a sectional bucket cover for the buckets. Intermediate between their ends the buckets are provided with tie wires 5.
- the openings in the buckets are of a size such that the tie wire makes a reasonably close fit therein and the tie wire is of a length such that when its ends are joined together it is not tight but on the contrary is somewhat loose.
- a turbine wheel expands due to centrifugal force and the tie wire is made loose enough that such expansion of the wheel will not be suflicient to take up all the looseness.
- the parts of the tie wire will be supported by the buckets, and thus the stresses will be low.
- the tie wire comprises preferably a twisted stranded cable formed of a multiplicity of wires or strands, and it is not fastened to the buckets except by the frictional fit in the openings through which it extends.
- My improved tie wire construction has the further advantage that if the buckets tend to vibrate tangentially out of phase one with the other, they will have to work and bend the segments of the tie wire in between the different buckets or else slip on the tie-wire, and in either case this will absorb the energy to such an extent that resonant vibration cannot be set up. Furthermore, the tendency of the tie wire will be to damp out nodal axial vibration inasmuch as it will be necessary for a wave to travel along the cable for it to conform the cable to the wave formation. Such bending of the cable will absorb energy and inasmuch as this axial vibration is also a resonant condition the amplitude will be greatly reduced. It will be readily understood that bending of the tie wire causes frictional resistance between the plurality of strands of which the wire is composed. This frictional resistance and also the frictional resistance set up between the tie wire and the blades abstracts oscillatory energy from the wheel.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
y 1932- G. B. WARREN ELASTIC FLUID TURBINE Filed Oct. 21, 1950 a :w ma w n wB .mn
by His Attorhes.
Patented May 10, 1932 UNITED STATES PATENT OFFICE GLENN B. WARREN, F SCHE'NECTADY, NEW YORK ASSIGNOB T0 GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK ELASTIC FLUID TURBINE Application filed October 21, 1930. Serial No. 490,232.
invention relates to elastic and especially to rotors for ing tie wires between the inner and outer ends 0 of the buckets to strengthen the buckets and increase their stifiness.
My invention relates especially to tie wires for turbine buckets, and has for its object to provide an improved tie wire construction and arrangement.
For a consideration of what I consider to be novel and my invention, attention is directed to the following specification and the claims appended thereto.
In the drawings, Fig. 1 is a side View of a portion of a turbine rotor, the buckets of which are provided with tie wires embodying my invention; Fig. 2 is a radial sectional view, and Fig. 3 is a detail view on a larger scale illustrating in somewhat exaggerated form the operation of the tie wire.
Referring to the drawings, 1 indicates a turbine shaft, 2 a rotor thereon, 3 a row of buckets carried by the rotor, and at a sectional bucket cover for the buckets. Intermediate between their ends the buckets are provided with tie wires 5.
According to my invention, I form the tie wire 5 from a wire cable comprising a plurality of strands, the tie wire being threaded through openings in the buckets and being preferably continuous, that is, in one continuous piece suitably fastened together at its ends. The openings in the buckets are of a size such that the tie wire makes a reasonably close fit therein and the tie wire is of a length such that when its ends are joined together it is not tight but on the contrary is somewhat loose. In operation, a turbine wheel expands due to centrifugal force and the tie wire is made loose enough that such expansion of the wheel will not be suflicient to take up all the looseness. As a result, the parts of the tie wire will be supported by the buckets, and thus the stresses will be low. At the same time, however, due to centrifugal force acting on the tie wire, the tie wire will be held tight between ad acent buckets, the tie wire sections between adjacent buckets bowing out wardly as is illustrated in exaggerated form at 6 in Fig. 3. By my invention, therefore, I obtain the advantages of a continuous tie wire but at the same time avoid the disadvantages heretofore met with. The tie wire comprises preferably a twisted stranded cable formed of a multiplicity of wires or strands, and it is not fastened to the buckets except by the frictional fit in the openings through which it extends.
My improved tie wire construction has the further advantage that if the buckets tend to vibrate tangentially out of phase one with the other, they will have to work and bend the segments of the tie wire in between the different buckets or else slip on the tie-wire, and in either case this will absorb the energy to such an extent that resonant vibration cannot be set up. Furthermore, the tendency of the tie wire will be to damp out nodal axial vibration inasmuch as it will be necessary for a wave to travel along the cable for it to conform the cable to the wave formation. Such bending of the cable will absorb energy and inasmuch as this axial vibration is also a resonant condition the amplitude will be greatly reduced. It will be readily understood that bending of the tie wire causes frictional resistance between the plurality of strands of which the wire is composed. This frictional resistance and also the frictional resistance set up between the tie wire and the blades abstracts oscillatory energy from the wheel.
In accordance with the provision of the patent statutes, I have described the principle 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.
What 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 continuous tie Wire for the buckets comprising a plurality of strands extending through passages in the buckets, said strands being loose enough that they do not become tight when the wheel eX- 5 pands due to centrifugal force.
2. The combination with a turbine rotor havinga row of buckets, of a continuous tie wire for the buckets comprising a plurality of strands twisted together and extending 10 through passages in the buckets and having a friction fit in such passages for absorbing oscillatory energy of the buckets.
3. The combination with a rotor comprising a disk, a row of blades secured to the 15 disk, the blades having transverse holes in circular relation to the rotor, of a continuous tie wire comprising a plurality of strands twisted together and extending through the holes in said blades and being in frictional 2 engagement with the blade walls defining said holes, said @t-ie wire being loosely arranged :between'adjacent blades whereby dangerous stresses of the tie Wire during operation of the rotor are prevented and circumferential 2 and axial nodal vibrations are dampened .due to frictional resistance set up between the individual strands and between the cable and the walls of the blades.
In witness whereof, I have hereunto set my 39 hand thisQOth .day of Gctober,1930.
GLENN B. WVARREN.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US490232A US1858067A (en) | 1930-10-21 | 1930-10-21 | Elastic fluid turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US490232A US1858067A (en) | 1930-10-21 | 1930-10-21 | Elastic fluid turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1858067A true US1858067A (en) | 1932-05-10 |
Family
ID=23947169
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US490232A Expired - Lifetime US1858067A (en) | 1930-10-21 | 1930-10-21 | Elastic fluid turbine |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1858067A (en) |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2914299A (en) * | 1954-02-05 | 1959-11-24 | Gen Electric Co Ltd | Steam turbines |
| DE1551173B1 (en) * | 1966-06-21 | 1971-07-08 | Rolls Royce | DEVICE FOR VIBRATION DAMPING ON FREE-STANDING BLADES OF FLOW MACHINERY |
| USRE32737E (en) * | 1980-06-30 | 1988-08-23 | Southern California Edison | Continuous harmonic shrouding |
| US20030202883A1 (en) * | 2002-04-26 | 2003-10-30 | Davis Gary A. | Turbine blade assembly with stranded wire cable dampers |
| US20100266400A1 (en) * | 2009-03-30 | 2010-10-21 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and method |
| US9151295B2 (en) | 2008-05-30 | 2015-10-06 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US9335061B2 (en) | 2008-05-30 | 2016-05-10 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US9459020B2 (en) | 2008-05-30 | 2016-10-04 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| USD783795S1 (en) | 2012-05-15 | 2017-04-11 | Airius Ip Holdings, Llc | Air moving device |
| US9631627B2 (en) | 2004-03-15 | 2017-04-25 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US9702576B2 (en) | 2013-12-19 | 2017-07-11 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| USD805176S1 (en) | 2016-05-06 | 2017-12-12 | Airius Ip Holdings, Llc | Air moving device |
| USD820967S1 (en) | 2016-05-06 | 2018-06-19 | Airius Ip Holdings Llc | Air moving device |
| US10024531B2 (en) | 2013-12-19 | 2018-07-17 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US10221861B2 (en) | 2014-06-06 | 2019-03-05 | Airius Ip Holdings Llc | Columnar air moving devices, systems and methods |
| US10487852B2 (en) | 2016-06-24 | 2019-11-26 | Airius Ip Holdings, Llc | Air moving device |
| USD885550S1 (en) | 2017-07-31 | 2020-05-26 | Airius Ip Holdings, Llc | Air moving device |
| USD886275S1 (en) | 2017-01-26 | 2020-06-02 | Airius Ip Holdings, Llc | Air moving device |
| USD887541S1 (en) | 2019-03-21 | 2020-06-16 | Airius Ip Holdings, Llc | Air moving device |
| US11598539B2 (en) | 2019-04-17 | 2023-03-07 | Airius Ip Holdings, Llc | Air moving device with bypass intake |
-
1930
- 1930-10-21 US US490232A patent/US1858067A/en not_active Expired - Lifetime
Cited By (43)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2914299A (en) * | 1954-02-05 | 1959-11-24 | Gen Electric Co Ltd | Steam turbines |
| DE1551173B1 (en) * | 1966-06-21 | 1971-07-08 | Rolls Royce | DEVICE FOR VIBRATION DAMPING ON FREE-STANDING BLADES OF FLOW MACHINERY |
| USRE32737E (en) * | 1980-06-30 | 1988-08-23 | Southern California Edison | Continuous harmonic shrouding |
| US20030202883A1 (en) * | 2002-04-26 | 2003-10-30 | Davis Gary A. | Turbine blade assembly with stranded wire cable dampers |
| US6685435B2 (en) * | 2002-04-26 | 2004-02-03 | The Boeing Company | Turbine blade assembly with stranded wire cable dampers |
| US9631627B2 (en) | 2004-03-15 | 2017-04-25 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US11053948B2 (en) | 2004-03-15 | 2021-07-06 | Airius Ip Holdings, Llc | Temperature destratification systems |
| US11365743B2 (en) | 2004-03-15 | 2022-06-21 | Airius Ip Holdings, Llc | Temperature destratification systems |
| US9714663B1 (en) | 2004-03-15 | 2017-07-25 | Airius Ip Holdings, Llc | Temperature destratification systems |
| US11703062B2 (en) | 2004-03-15 | 2023-07-18 | Airius Ip Holdings, Llc | Temperature destratification systems |
| US10487840B2 (en) | 2004-03-15 | 2019-11-26 | Airius Ip Holdings, Llc | Temperature destratification systems |
| US12085084B2 (en) | 2004-03-15 | 2024-09-10 | Airius Ip Holdings, Llc | Temperature destratification systems |
| US9459020B2 (en) | 2008-05-30 | 2016-10-04 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US9335061B2 (en) | 2008-05-30 | 2016-05-10 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US9151295B2 (en) | 2008-05-30 | 2015-10-06 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US9970457B2 (en) | 2008-05-30 | 2018-05-15 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US20140314560A1 (en) * | 2009-03-30 | 2014-10-23 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and method |
| US8616842B2 (en) * | 2009-03-30 | 2013-12-31 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and method |
| US20100266400A1 (en) * | 2009-03-30 | 2010-10-21 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and method |
| US10184489B2 (en) | 2011-06-15 | 2019-01-22 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| USD926963S1 (en) | 2012-05-15 | 2021-08-03 | Airius Ip Holdings, Llc | Air moving device |
| USD783795S1 (en) | 2012-05-15 | 2017-04-11 | Airius Ip Holdings, Llc | Air moving device |
| US10024531B2 (en) | 2013-12-19 | 2018-07-17 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US10641506B2 (en) | 2013-12-19 | 2020-05-05 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US10655841B2 (en) | 2013-12-19 | 2020-05-19 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US11221153B2 (en) | 2013-12-19 | 2022-01-11 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US9702576B2 (en) | 2013-12-19 | 2017-07-11 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US11092330B2 (en) | 2013-12-19 | 2021-08-17 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US10221861B2 (en) | 2014-06-06 | 2019-03-05 | Airius Ip Holdings Llc | Columnar air moving devices, systems and methods |
| US10724542B2 (en) | 2014-06-06 | 2020-07-28 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| US11236766B2 (en) | 2014-06-06 | 2022-02-01 | Airius Ip Holdings Llc | Columnar air moving devices, systems and methods |
| US11713773B2 (en) | 2014-06-06 | 2023-08-01 | Airius Ip Holdings, Llc | Columnar air moving devices, systems and methods |
| USD820967S1 (en) | 2016-05-06 | 2018-06-19 | Airius Ip Holdings Llc | Air moving device |
| USD805176S1 (en) | 2016-05-06 | 2017-12-12 | Airius Ip Holdings, Llc | Air moving device |
| US11421710B2 (en) | 2016-06-24 | 2022-08-23 | Airius Ip Holdings, Llc | Air moving device |
| US11105341B2 (en) | 2016-06-24 | 2021-08-31 | Airius Ip Holdings, Llc | Air moving device |
| US10487852B2 (en) | 2016-06-24 | 2019-11-26 | Airius Ip Holdings, Llc | Air moving device |
| USD886275S1 (en) | 2017-01-26 | 2020-06-02 | Airius Ip Holdings, Llc | Air moving device |
| USD885550S1 (en) | 2017-07-31 | 2020-05-26 | Airius Ip Holdings, Llc | Air moving device |
| USD887541S1 (en) | 2019-03-21 | 2020-06-16 | Airius Ip Holdings, Llc | Air moving device |
| US11598539B2 (en) | 2019-04-17 | 2023-03-07 | Airius Ip Holdings, Llc | Air moving device with bypass intake |
| US11781761B1 (en) | 2019-04-17 | 2023-10-10 | Airius Ip Holdings, Llc | Air moving device with bypass intake |
| US12259156B2 (en) | 2019-04-17 | 2025-03-25 | Airius Ip Holdings, Llc | Air moving device with bypass intake |
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