US1516607A - Hollow turbine bucket and method of manufacturing same - Google Patents

Hollow turbine bucket and method of manufacturing same Download PDF

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Publication number
US1516607A
US1516607A US654523A US65452323A US1516607A US 1516607 A US1516607 A US 1516607A US 654523 A US654523 A US 654523A US 65452323 A US65452323 A US 65452323A US 1516607 A US1516607 A US 1516607A
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United States
Prior art keywords
bucket
base
wall
turbine bucket
manufacturing same
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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
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US654523A
Inventor
Johanson John
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General Electric Co
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General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US654523A priority Critical patent/US1516607A/en
Priority to FR584517D priority patent/FR584517A/en
Application granted granted Critical
Publication of US1516607A publication Critical patent/US1516607A/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
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades

Definitions

  • Fig. 1 is a. view of a partially completed tur ine bucket embodying my invention
  • Fig. 2 is a vertical sectional view thereof
  • Fig. 3 is a sectional lan view through the base of the bucket
  • Fig. 5 is a view s owing a completed bucket mounted on a rotor.
  • the front and back Walls of the bucket may be formed of two curved pieces of sheet metal suitably united along their edges, 6 being the front wall and 7 the back wall.
  • walls 6 and 7 from Monel metal and they ma lie-united rspective along their edges in any suita 1e manner such as by sol ering, brazing, welding or the like.
  • the back wall 7 extends throughout the length of the bucket while the front wall terminates at the top of the base.
  • base is made up primarily of two main pieces, a front piece 8 and a back piece 9.
  • the front piece 8 has a curved surface 10 which fits the inner surface of back wall 7 and the back piece 9 has a curved surface 11 which fits around the outer surface of wall 7.
  • the lower end of wall 7 is thus held between'the two base pieces 8 and 9.
  • the front base piece 8 has a which projects up between wal s 6 and 7 and thls projecting portion is preferably tapered in accordance with the falling off of the centrifugal stresses. This may be done by cutting a V-shaped notch in the projection as indicated at 13.
  • the projection 12 forms a reinforcing member for giving strength to the inner end of the bucket.
  • the base may be finished to any suitable contour for attachmg it to a rotor or bucket-carrying member.
  • Fig. 5 I have shown it provided with slots 18 to form a dove-tail for engagement with a groove 19 in the rotor this being a well-known form of bucket fastening means.
  • the rotor or bucket carrying member is indicated at 19.
  • pins 14 are so located that when the bucket bases are finished, the pins are removed with the waste material.
  • the holes 15 and pins 14 do not therefore serve in any way to weaken the structure.
  • the 'plate' 16 serves to grip and hold the lower end of inner wall 6.
  • the base member 9 preferabl extends up along the back of wall 7 as indicated at 20 to brace the back of the bucket.
  • lhe bucket may be provided with a suitable tenon 21 for fastening in place a bucket cover 22, the tenon being fixed to the'bucket by welding or. in any other desired manner.
  • a turbine bucket comprising curved front and back walls united along their longitudinal edges, the back wall projecting below the front wall at one end, and a plurality of base pieces between which the projecting end of the back wall is held.
  • a turbine bucket comprising curved front and back walls united along their longitudinal edges, the back wall projecting below the front wall at one end, a front and back base piece between which the projecting end is clamped, and a reinforcing projection on'the front base piece which extends up between said front andback walls.
  • a turbine bucket comprising curved front and back walls united along their longitudinal edges, the back wall projecting below the front wall at one end, a front and back base piece between which the projecting end is clamped, and a tapered reinforcing member which projects from the base piece up between said front and back walls.
  • a turbine bucket comprising curved front and back walls united along their longitudinal edges, and base pieces between which the lower ends of said walls are held, said wallsv and base pieces being united by fused metal.
  • a turbine bucket comprising curved 7 front and back walls united along their longitudinal edges, and a plurality of base pieces between which the lower end of the back wall is held, said wall and back piece being united by fused metal.
  • a turbine bucket comprising curved JOHN JOHANSON.

Description

Nov.'25, 1,516,607
J.JOHANSON HOLLOW TURBINE BUCKET AND METHOD OF MANUFACTURING SAME Filed July 30, 1925 Inventor: John Johanson,
- Hisw t' or eg- 20 with such buckets has been to provide a Patented Nov. 25, 1924. V
'NITED STATES r 1,516,607 PATENT OFFICE.
JOHN JOHANSON, OT SGHENEOTADY, NEW YORK, ASSIGN OR TO GENERAL ELECTRIC I COMPANY, A CORPORATION OF NEW YORK.
' nor-now rumamn BUcxE'r Arm marnon or MANUFACTURING sum.
Application filed Iuly 80, 1928. Serial No. 654,528.
To all whom it may concern:
Be it known that 1, JOHN JOHANSON, a citizen of the United States, residing at Schenectad in the county of Schenectady, State of Nie w York, have invented certain new and useful Improvements in Hollow Turbine Buckets and Methods of Manufacturing Same, of which the following is a specification.
It has heretofore been proposed to make turbine buckets hollow in order to reduce their weight and thereby decrease the centrifugal stresses but even with hollow buckets of light wei ht the centrifugalstresses become of consi erable value asthe buckets increase in length. The stresses" are-highest of course, at the roots of the buckets and gradually decrease toward the tips, the greatest stress being in the basesof the buckets. One of the problems in connection practical structure having su'fiicient strength at its base or inner end to withstand the centrifugal stresses met with in modern turbine practice and the object of my invention is to provide an improved hollow turbine bucket structure which will meet this condition and an improved method of manufacturing thesame.
For a consideration of what believe to be novel and my invention, attention is dirooted to the accompanying description and the claims appended thereto.
In the drawing, Fig. 1 is a. view of a partially completed tur ine bucket embodying my invention; Fig. 2 is a vertical sectional view thereof; Fig. 3 is a sectional lan view through the base of the bucket; ig. 41s an exploded view of the parts used in manufacturmglmy improved bucket, and Fig. 5 is a view s owing a completed bucket mounted on a rotor. Y
The front and back Walls of the bucket may be formed of two curved pieces of sheet metal suitably united along their edges, 6 being the front wall and 7 the back wall. I may with advantage form. walls 6 and 7 from Monel metal and they ma lie-united rspective along their edges in any suita 1e manner such as by sol ering, brazing, welding or the like. The back wall 7 extends throughout the length of the bucket while the front wall terminates at the top of the base. The
base is made up primarily of two main pieces, a front piece 8 and a back piece 9.
The front piece 8 has a curved surface 10 which fits the inner surface of back wall 7 and the back piece 9 has a curved surface 11 which fits around the outer surface of wall 7. The lower end of wall 7 is thus held between'the two base pieces 8 and 9. The front base piece 8 has a which projects up between wal s 6 and 7 and thls projecting portion is preferably tapered in accordance with the falling off of the centrifugal stresses. This may be done by cutting a V-shaped notch in the projection as indicated at 13. The projection 12 forms a reinforcing member for giving strength to the inner end of the bucket.
ortion 12 In constructing a bucket embodying my invention'I take a front and back wall 6 and 7 which have been suitably united to each other along their edges and put the front base piece 8 in position as best shown in Figs. 1 and 2, slipping the reinforcing projection 12 up between walls 6- and 7. I then put back wall piece 9 in position around the lower end of back wall 7 and fasten the parts together in what may be termed an initial or temporary manner by means of pins 14 which may be driven into holes 15. Or, the parts may be fastened in any other suitable manner. When thusassembled the lower edge of inner wall 6 takes 7 against the flat top surface of base piece 8. I then apply to such to surfacea holding plate 16 which may be astened in position temporarily by any suitable means such as by means of the pin- 17.
After the parts have been this assembled- I then unite themto form-a unitary struc ,parts and eflect a. union of them, forming" in substance a unitary structure.
' After the assembled parts have been thus united into a unitary structure, the base may be finished to any suitable contour for attachmg it to a rotor or bucket-carrying member. In Fig. 5 I have shown it provided with slots 18 to form a dove-tail for engagement with a groove 19 in the rotor this being a well-known form of bucket fastening means. In Fig. 5, the rotor or bucket carrying member is indicated at 19. Preferably, pins 14 are so located that when the bucket bases are finished, the pins are removed with the waste material. The holes 15 and pins 14 do not therefore serve in any way to weaken the structure. The 'plate' 16 serves to grip and hold the lower end of inner wall 6. The base member 9 preferabl extends up along the back of wall 7 as indicated at 20 to brace the back of the bucket.
lhe bucket may be provided with a suitable tenon 21 for fastening in place a bucket cover 22, the tenon being fixed to the'bucket by welding or. in any other desired manner.
By the above described arrangement 'I provide a structure wherein the bucket proper comprisin walls 6 and 7 is firmly anchored to the ase and also a structure wherein the base and the portion of the bucket next to the base are amply strong to withstand the centrifugal stresses met with. At the same time by following m method of construction the bucket may". e manufactured at a reasonable cost. The reinforcing projection 12 may be made as long as found desirable in any particular case and may be given a crosssection such as to provide the desired strength. By its use I provide in substance the equivalent of a tapered bucket. I 1
What I claim as new and desire to secure by Letters Patent of the United States, is
1. A turbine bucket comprising curved front and back walls united along their longitudinal edges, the back wall projecting below the front wall at one end, and a plurality of base pieces between which the projecting end of the back wall is held.
2. A turbine bucket comprising curved front and back walls united along their longitudinal edges, the back wall projecting below the front wall at one end, a front and back base piece between which the projecting end is clamped, and a reinforcing projection on'the front base piece which extends up between said front andback walls.
3. A turbine bucket comprising curved front and back walls united along their longitudinal edges, the back wall projecting below the front wall at one end, a front and back base piece between which the projecting end is clamped, and a tapered reinforcing member which projects from the base piece up between said front and back walls.
4. A turbine bucket comprising curved front and back walls united along their longitudinal edges, and base pieces between which the lower ends of said walls are held, said wallsv and base pieces being united by fused metal.
5. A turbine bucket comprising curved 7 front and back walls united along their longitudinal edges, and a plurality of base pieces between which the lower end of the back wall is held, said wall and back piece being united by fused metal.
6. A turbine bucket comprising curved JOHN JOHANSON.
US654523A 1923-07-30 1923-07-30 Hollow turbine bucket and method of manufacturing same Expired - Lifetime US1516607A (en)

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US654523A US1516607A (en) 1923-07-30 1923-07-30 Hollow turbine bucket and method of manufacturing same
FR584517D FR584517A (en) 1923-07-30 1924-07-22 Hollow turbine blade and its manufacturing process

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2601969A (en) * 1946-01-25 1952-07-01 United Specialties Co Turbine wheel
US2656146A (en) * 1948-04-08 1953-10-20 Curtiss Wright Corp Turbine blade construction
US2767460A (en) * 1950-02-08 1956-10-23 Robbins Engineering Company Turbine blade and method of making same
US2786646A (en) * 1949-08-10 1957-03-26 Power Jets Res & Dev Ltd Bladed rotors for axial flow turbines and similarly bladed fluid flow machines
US2819870A (en) * 1955-04-18 1958-01-14 Oleh A Wayne Sheet metal blade base
US2853272A (en) * 1952-09-12 1958-09-23 Napier & Son Ltd Hollow blades for turbo machines
US2856152A (en) * 1953-04-23 1958-10-14 American Motors Corp Turbine wheel assembly
US2976014A (en) * 1952-01-19 1961-03-21 Bbc Brown Boveri & Cie Blading for use in axial flow machines
US3012308A (en) * 1957-08-12 1961-12-12 Joy Mfg Co Method of making blade structures
US3063674A (en) * 1961-02-08 1962-11-13 Jr Clarence E Middlebrooks Rotor construction and method
DE976242C (en) * 1943-05-28 1963-05-22 Versuchsanstalt Fuer Luftfahrt Method for producing hollow blades from sheet metal, in particular for gas turbines
US20100006352A1 (en) * 2008-07-11 2010-01-14 Fabio Agostini Cannon-shaped wind turbines for electric vehicles
US20110142639A1 (en) * 2009-12-15 2011-06-16 Campbell Christian X Modular turbine airfoil and platform assembly with independent root teeth
US20160230568A1 (en) * 2015-02-05 2016-08-11 Rolls-Royce Corporation Ceramic matrix composite gas turbine engine blade
US10738628B2 (en) * 2018-05-25 2020-08-11 General Electric Company Joint for band features on turbine nozzle and fabrication

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE976242C (en) * 1943-05-28 1963-05-22 Versuchsanstalt Fuer Luftfahrt Method for producing hollow blades from sheet metal, in particular for gas turbines
US2601969A (en) * 1946-01-25 1952-07-01 United Specialties Co Turbine wheel
US2656146A (en) * 1948-04-08 1953-10-20 Curtiss Wright Corp Turbine blade construction
US2786646A (en) * 1949-08-10 1957-03-26 Power Jets Res & Dev Ltd Bladed rotors for axial flow turbines and similarly bladed fluid flow machines
US2767460A (en) * 1950-02-08 1956-10-23 Robbins Engineering Company Turbine blade and method of making same
US2976014A (en) * 1952-01-19 1961-03-21 Bbc Brown Boveri & Cie Blading for use in axial flow machines
US2853272A (en) * 1952-09-12 1958-09-23 Napier & Son Ltd Hollow blades for turbo machines
US2856152A (en) * 1953-04-23 1958-10-14 American Motors Corp Turbine wheel assembly
US2819870A (en) * 1955-04-18 1958-01-14 Oleh A Wayne Sheet metal blade base
US3012308A (en) * 1957-08-12 1961-12-12 Joy Mfg Co Method of making blade structures
US3063674A (en) * 1961-02-08 1962-11-13 Jr Clarence E Middlebrooks Rotor construction and method
US20100006352A1 (en) * 2008-07-11 2010-01-14 Fabio Agostini Cannon-shaped wind turbines for electric vehicles
US20110142639A1 (en) * 2009-12-15 2011-06-16 Campbell Christian X Modular turbine airfoil and platform assembly with independent root teeth
US8496443B2 (en) * 2009-12-15 2013-07-30 Siemens Energy, Inc. Modular turbine airfoil and platform assembly with independent root teeth
US20160230568A1 (en) * 2015-02-05 2016-08-11 Rolls-Royce Corporation Ceramic matrix composite gas turbine engine blade
US10253639B2 (en) * 2015-02-05 2019-04-09 Rolls-Royce North American Technologies, Inc. Ceramic matrix composite gas turbine engine blade
US10738628B2 (en) * 2018-05-25 2020-08-11 General Electric Company Joint for band features on turbine nozzle and fabrication

Also Published As

Publication number Publication date
FR584517A (en) 1925-02-09

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