US1378464A - Elastic-fluid turbine - Google Patents

Elastic-fluid turbine Download PDF

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Publication number
US1378464A
US1378464A US420502A US42050220A US1378464A US 1378464 A US1378464 A US 1378464A US 420502 A US420502 A US 420502A US 42050220 A US42050220 A US 42050220A US 1378464 A US1378464 A US 1378464A
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United States
Prior art keywords
elastic
buckets
bucket
adjacent
fluid turbine
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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
US420502A
Inventor
Junggren Oscar
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General Electric Co
Original Assignee
General Electric Co
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Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US420502A priority Critical patent/US1378464A/en
Application granted granted Critical
Publication of US1378464A publication Critical patent/US1378464A/en
Priority to FR542869D priority patent/FR542869A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F01D5/225Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • F05D2250/70Shape
    • F05D2250/75Shape given by its similarity to a letter, e.g. T-shaped

Definitions

  • the present invention relates to elastic fluid turbines and particularly to rotor structures which comprise a ring o'f buckets fastened to a disk or drum at their inner ends and having their outer ends connected together by a sectional bucket cover.
  • Figure 1 is a side elevation partly in section of a part of a tur' bine rotor embodying my invention
  • FIG. 1 is a top plan view of several adjacent buckets;
  • Fig. 3 is a perspective view of a tie plate; and
  • Figs. 4, 5 and 6 are views similar to Figs. 1, 2 and 3 of another form of the invention.
  • 5 indicates a rot-or and 6 a ring of buckets fastened thereto at their bases and having their outer ends connected to ether by bucket cover sections 7, the uckets being provided with integral tenons 8 by means of which the bucket cover sections are fastened in posi tion.
  • This divides the ring of buckets into groups, the buckets of each group having Specification of Letters Patent.
  • the outer ends of the buckets are some distance apart. I may use either the arrangement shown in Figs. 1, 2 and 3 or ⁇ I may use that shown in Figs. il, 5 and 6 wherein the flexible connections 12 are riveted directly. to the adjacent ends of the bucket cover sections by rivets as indicated at 13. 'In this case the flexible connection as shown in Fig. 6 has' its ends shaped' to conform to the contour of the adjacent bucket surfaces.
  • connections While being flexible enough to lpermit of expansion and contraction ⁇ are sufficiently stiff to tie the' bucket groups togetherso as to prevent their vibration.
  • An elastic i'luid turbine having a. rotor with ak ring of buckets thereon termed inte groops by a sectional bucket cover characterized by the factl that the bucket groups thus formed are tied together by connections in the forni of plates located directif; beneath the adjacent ends o bucket cefer aangeeft sections and reversely bent to render them iexibie.

Description

l). UNGGREN.
LSIC FLUID TURBINE.
:.Pvucmmu min 001.23* 1920.
l,378,464. Patented May 17, 192L Inventor". OscarJungcgVe-an l-liSAttomeg. y
FFICE.
OSCAR JUNGG-REN, OF SCHENECTADY, NEW YRK, ASSIGNOR TO GENERAL ELECTRIC CMPANY, A. CORPORATION F NEW YORK.
ELASTICI-FLUID TURBINE.
To all wiz-om. t may concern.:
Be it known that I. @SCAR JUNGGREN, a citizen of the United States, residing at Schenectady, county of Schenectady, State of New York, have inventedcertain nenv and useful Improvements in Elastic-Fluid Turbines, of which the following is a speci'- cation.
The present invention relates to elastic fluid turbines and particularly to rotor structures which comprise a ring o'f buckets fastened to a disk or drum at their inner ends and having their outer ends connected together by a sectional bucket cover. In
such structures each bucket cover section their natural period or due to inequalities,
of elastic iuid pressure'. Such vibrations may cause failure of buckets and the object of vmy present invention is. to provide an improved structure and arrangement for preventing their occurrence. Y
For a consideration of what I believe to be novel and my invention, attention is directed to the accompanying description andthe claims appended thereto.V Y Y In the drawing, Figure 1 is a side elevation partly in section of a part of a tur' bine rotor embodying my invention; Fig. 2
is a top plan view of several adjacent buckets; Fig. 3 is a perspective view of a tie plate; and Figs. 4, 5 and 6 are views similar to Figs. 1, 2 and 3 of another form of the invention.
Referring -to the drawing, 5 indicates a rot-or and 6 a ring of buckets fastened thereto at their bases and having their outer ends connected to ether by bucket cover sections 7, the uckets being provided with integral tenons 8 by means of which the bucket cover sections are fastened in posi tion. This divides the ring of buckets into groups, the buckets of each group having Specification of Letters Patent.
Patented May 17, 1921.
their outer ends fastened together by a bucket cover section. 1how, according' to my invention, I tie adjacent bucket groups together bv lmeans of flexible connections or tie plates such connectlons being located beneath the bucket cover 'so as not to be in a position Where they might fret worn oli.' or Where they will impair the clearances. In the arrangement shoivn in Figs. l, 2 and 3 the flexible connections are in the form of at plates 9 reversely bent to form a U-shaped part 10. In the plates are openings 11 through which the tenons on adjacent buckets pass. The flexible connections are thus riveted in place directly beneath the bucket,F cover sections by the same tenons which hold the bucket cover sections. ThisA arrangement is well adapted for use Where the outer ends of the buckets are comparatively close 'together'.
XVir-hen the outer ends of the buckets are some distance apart. I may use either the arrangement shown in Figs. 1, 2 and 3 or` I may use that shown in Figs. il, 5 and 6 wherein the flexible connections 12 are riveted directly. to the adjacent ends of the bucket cover sections by rivets as indicated at 13. 'In this case the flexible connection as shown in Fig. 6 has' its ends shaped' to conform to the contour of the adjacent bucket surfaces.
With either of the arrangements shown,
the connections While being flexible enough to lpermit of expansion and contraction` are sufficiently stiff to tie the' bucket groups togetherso as to prevent their vibration.
By arranging the yieldable connections directly beneath the bucket cover,- the periphery of the bucket ring may have the desired clearance with the turbine shell, the connections in n0 Way interfering as they would were they on the outside. Furthermore, there is no danger of the connections lubbing, thereby getting worn or coming oose. v
In accordance with the provisions 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 te secure by Letters Patent of the nited States? is 1. In an elastic nid turbine, the combination with a ring of buckets, and a setional cover tying them together into groups, of means forming Hexible eonnecticns between adjacent groups, said means being located directly beneath the adjacent ends of bucketcover sections.
2. An elastic i'luid turbine having a. rotor with ak ring of buckets thereon termed inte groops by a sectional bucket cover characterized by the factl that the bucket groups thus formed are tied together by connections in the forni of plates located directif; beneath the adjacent ends o bucket cefer aangeeft sections and reversely bent to render them iexibie. Y
3. in elastic Huid turbine having a rotor with a ring of buckets thereon formed into groups by a, sectional bucket cover fastened inte place by tenons on the ends of the buckets, characterized by the fact that the bucket groups thus formed are tied together by flexible strips 'located beneath the adjacent ends of bucket cover sections and fastened by the tenons of the adjacent buciiets.
in Witness whereof, have hereunto set my hand tins 28th day of October, 1920.
OSCAR JUXGGREN.
US420502A 1920-10-29 1920-10-29 Elastic-fluid turbine Expired - Lifetime US1378464A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US420502A US1378464A (en) 1920-10-29 1920-10-29 Elastic-fluid turbine
FR542869D FR542869A (en) 1920-10-29 1921-10-28 Elastic fluid turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US420502A US1378464A (en) 1920-10-29 1920-10-29 Elastic-fluid turbine

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US1378464A true US1378464A (en) 1921-05-17

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2606741A (en) * 1947-06-11 1952-08-12 Gen Electric Gas turbine nozzle and bucket shroud structure
US2610823A (en) * 1947-02-11 1952-09-16 Gen Electric Turbine bucket damping arrangement
US2661147A (en) * 1949-01-19 1953-12-01 Ingersoll Rand Co Blower blade fastening device
US2695767A (en) * 1951-03-23 1954-11-30 Elliott Co Turbocharger
US2873087A (en) * 1952-05-20 1959-02-10 Parsons & Marine Eng Turbine Means for cooling gas turbines
US3048365A (en) * 1959-12-22 1962-08-07 Curtiss Wright Corp Rotor blade shroud and vibration damping structure
US3056582A (en) * 1960-08-26 1962-10-02 Gen Electric Turbine stator construction
US4386887A (en) * 1980-06-30 1983-06-07 Southern California Edison Company Continuous harmonic shrouding
US4734010A (en) * 1985-05-31 1988-03-29 Bbc Brown, Boveri & Company, Limited Damping element for independent turbomachine blades
USRE32737E (en) * 1980-06-30 1988-08-23 Southern California Edison Continuous harmonic shrouding
US4936749A (en) * 1988-12-21 1990-06-26 General Electric Company Blade-to-blade vibration damper
US4986737A (en) * 1988-12-29 1991-01-22 General Electric Company Damped gas turbine engine airfoil row
US5011374A (en) * 1987-11-17 1991-04-30 General Electric Company Method and apparatus for balancing turbine rotors
US20080063522A1 (en) * 2006-09-07 2008-03-13 Rolls-Royce Plc Array of components
US11105209B2 (en) * 2018-08-28 2021-08-31 General Electric Company Turbine blade tip shroud

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2318059C3 (en) * 1973-04-06 1979-03-01 Kraftwerk Union Ag, 4330 Muelheim Multiple rotor blades for steam turbines with axial flow

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2610823A (en) * 1947-02-11 1952-09-16 Gen Electric Turbine bucket damping arrangement
US2606741A (en) * 1947-06-11 1952-08-12 Gen Electric Gas turbine nozzle and bucket shroud structure
US2661147A (en) * 1949-01-19 1953-12-01 Ingersoll Rand Co Blower blade fastening device
US2695767A (en) * 1951-03-23 1954-11-30 Elliott Co Turbocharger
US2873087A (en) * 1952-05-20 1959-02-10 Parsons & Marine Eng Turbine Means for cooling gas turbines
US3048365A (en) * 1959-12-22 1962-08-07 Curtiss Wright Corp Rotor blade shroud and vibration damping structure
US3056582A (en) * 1960-08-26 1962-10-02 Gen Electric Turbine stator construction
US4386887A (en) * 1980-06-30 1983-06-07 Southern California Edison Company Continuous harmonic shrouding
USRE32737E (en) * 1980-06-30 1988-08-23 Southern California Edison Continuous harmonic shrouding
US4734010A (en) * 1985-05-31 1988-03-29 Bbc Brown, Boveri & Company, Limited Damping element for independent turbomachine blades
US5011374A (en) * 1987-11-17 1991-04-30 General Electric Company Method and apparatus for balancing turbine rotors
US4936749A (en) * 1988-12-21 1990-06-26 General Electric Company Blade-to-blade vibration damper
US4986737A (en) * 1988-12-29 1991-01-22 General Electric Company Damped gas turbine engine airfoil row
US20080063522A1 (en) * 2006-09-07 2008-03-13 Rolls-Royce Plc Array of components
US11105209B2 (en) * 2018-08-28 2021-08-31 General Electric Company Turbine blade tip shroud

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Publication number Publication date
FR542869A (en) 1922-08-23

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