US1366667A - Elastic-fluid turbine - Google Patents

Elastic-fluid turbine Download PDF

Info

Publication number
US1366667A
US1366667A US338997A US33899719A US1366667A US 1366667 A US1366667 A US 1366667A US 338997 A US338997 A US 338997A US 33899719 A US33899719 A US 33899719A US 1366667 A US1366667 A US 1366667A
Authority
US
United States
Prior art keywords
buckets
bucket
elastic
bases
rim
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
US338997A
Inventor
Junggren Oscar
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
Priority to US307184A priority Critical patent/US1366605A/en
Priority to US31499719 priority patent/US1366592A/en
Application filed by General Electric Co filed Critical General Electric Co
Priority to US338997A priority patent/US1366667A/en
Priority to FR519206A priority patent/FR519206A/en
Priority to FR23665A priority patent/FR23665E/en
Priority to FR24760A priority patent/FR24760E/en
Application granted granted Critical
Publication of US1366667A publication Critical patent/US1366667A/en
Priority to DEG56548D priority patent/DE393837C/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/3046Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses the rotor having ribs around the circumference
    • 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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49321Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Definitions

  • the present invention relates to elastic tion of a portion of a bucket wheel embody-' ing my invention and Fig. 2 is a radial sectional view thereof.
  • 3 indicates the web of the wheel or rotor and 4 the rim thereof upon which the ring of buckets 5 is mounted.
  • rim'& On opposite sides rim'& is provided with annular shoulders 6 and annular grooves 7 thereby providing an annular head 8 having undercut sides.
  • bases are provided with slots forming two legs or furcations 9 which. straddle head 8.
  • legs 9 On their inner ends legs 9 are provided with inwardly facing projections 10 which fit into grooves 7 and engage under head 8.
  • Shoulders 6 are provided with annular projections 11 behind which projections 12 on the extremities of legs 9 are located to prevent the legs from spreading.
  • the buckets will be assembled on the rim in the usual manner one or more fillin slots not shown) being provided in the rim as is well understood.
  • 14 indicates the bucket cover.
  • each group may comprise a bases are illustrated as bein
  • the bucketsuitable number of buckets for example, from 6 to 8 or more, and the bucket cover Wlll be made in sections of such length that each section just spans one group.
  • the bucket bases of the group are rigidly united.
  • the bucket bases The of a group may however, be united in other ways, such as by copper brazing, for eX- ample, and if found desirable, the bucket groups may be formed the buckets on the wheel.
  • the bucket cover in addition to being prior to mounting fastened by tenons 17, as indicated, is also preferably welded or brazed to the bucket ends so the bucket cover will be firmly supported at all points.
  • a rotor In an elastic fluid turbine, a rotor havets having bases provided with projections which engage in said grooves to fasten the buckets individually to the rim, said bucket bases being fastened to each other by fusion of metal to form groups.
  • a rotor havinga rim provided With a groove, buckets having bases provided With projections which enga e in said grooves'to fasten the buckets individually to the rim, and a sectional bucket cover fastened on the ends of said buckets, said bucket bases being fastoned to each other by fusion of metal to form groups.
  • i turbine rotor comprisin a rim proaving projections which fit into said groove to fasten the bucket to the rim, and a sectional bucket cover, characterized bythe fact that the bucket basesare united by fusion of metal to form bucket groups whereby any bucket is prevented from moving individually.
  • a turbine rotor having the buckets fastened thereon individually by dovetailed connections characterized by the fact that the buckets are formed into groups by uniting the bases of successive series of buckets 6.
  • a rotor having a rim and buckets having bases, said bases being fastened to the run by dovetailed connections, said buckets being arranged in groups, each group comprising a plurality of buckets having their bases 1 welded together and a bucket cover section Welded to their outer ends.

Description

0. JUNGGREN.
ELASTIC FLUID TURBINE.
APPLICATION FILED IIOv. III. 1919.
Inventor:
1,366,667, Patented Jan. 25, 1921.
HisAL ornes.
UNITED .sTA'rEs OSCAR J'UNGGBEN,
PATENT OFFICE.-
OF SOHENECTADY, YORK, ASSIGNOB; 530 GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK.
ELASTIC-FLUID TURBINE.
Specification of Letters Patent.
Patented Jan. 25, 1921;
' Application filed November 18, 1919. Serial Hm 338,997.
To all whom it may concern:
Be it known that I, OSCAR JUNeonnN, a citizen of the United States, residing at Schenectady, in the county of Schenectady,
State of New York, have invented certain new and useful Improvements in Elastic- Fluid Turbines, of which the following is a specification.
The present invention relates to elastic tion of a portion of a bucket wheel embody-' ing my invention and Fig. 2 is a radial sectional view thereof.
Referring to the drawing, 3 indicates the web of the wheel or rotor and 4 the rim thereof upon which the ring of buckets 5 is mounted. On opposite sides rim'& is provided with annular shoulders 6 and annular grooves 7 thereby providing an annular head 8 having undercut sides. bases are provided with slots forming two legs or furcations 9 which. straddle head 8. On their inner ends legs 9 are provided with inwardly facing projections 10 which fit into grooves 7 and engage under head 8. Shoulders 6 are provided with annular projections 11 behind which projections 12 on the extremities of legs 9 are located to prevent the legs from spreading. The buckets will be assembled on the rim in the usual manner one or more fillin slots not shown) being provided in the rim as is well understood. 14 indicates the bucket cover.
The bucket fastening means as just described forms what is termed the inverted dovetailed type of fastening and in itself is well known. It ma be taken as typical of a suitable type of astening means in connection with which my invention may be carried out.
Now, according to my invention, I fasten the turbine buckets to the wheelin groups, the buckets of each group being fastened to each other by fastening their bases together in a suitable manner such as by Welding, and their outer ends together'by means of the bucket cover. Each group may comprise a bases are illustrated as bein The bucketsuitable number of buckets, for example, from 6 to 8 or more, and the bucket cover Wlll be made in sections of such length that each section just spans one group. In Fig."
1 of the drawing, one group and a part of the group on each side thereof is shown. Such group extends from a to b and is shown 'as comprising seven buckets.
fastened together by providing them with grooves 15 on opposite sides which grooves, after the buckets have been assembled on the wheel, are filled with metal 16 as by the arc welding process so all the bucket bases of the group are rigidly united. The bucket bases The of a group may however, be united in other ways, such as by copper brazing, for eX- ample, and if found desirable, the bucket groups may be formed the buckets on the wheel.
The bucket cover, in addition to being prior to mounting fastened by tenons 17, as indicated, is also preferably welded or brazed to the bucket ends so the bucket cover will be firmly supported at all points.
With the above described arrangement wherein the buckets are attached to. .the
wheel in groups the buckets of each group being firmly united, it will be seen this there is no osslbility for any bucket to move indivi ually or yield at its base in such manner as to permit it to incline slightly, which may result in breakin of the bucket cover or of the tenons. Furt ermore, if'any individual bucket base does not fit the rim well nevertheless it cannot loosen or move since it is held by ad'acent buckets.
In accordance wit 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 to secure. by Letters Patent of the United States, is:
1. In an elastic fluid turbine, a rotor havets having bases provided with projections which engage in said grooves to fasten the buckets individually to the rim, said bucket bases being fastened to each other by fusion of metal to form groups.
- vided with a groove, buckets 2. In an elastic 'fluid turbine, a rotor havinga rim provided With a groove, buckets having bases provided With projections which enga e in said grooves'to fasten the buckets individually to the rim, and a sectional bucket cover fastened on the ends of said buckets, said bucket bases being fastoned to each other by fusion of metal to form groups.
3. i turbine rotor 'comprisin a rim proaving projections which fit into said groove to fasten the bucket to the rim, and a sectional bucket cover, characterized bythe fact that the bucket basesare united by fusion of metal to form bucket groups whereby any bucket is prevented from moving individually.
4:. A turbine rotor having the buckets fastened thereon individually by dovetailed connections characterized by the fact that the buckets are formed into groups by uniting the bases of successive series of buckets 6. In an elastic fluid turbine, a rotor having a rim and buckets having bases, said bases being fastened to the run by dovetailed connections, said buckets being arranged in groups, each group comprising a plurality of buckets having their bases 1 welded together and a bucket cover section Welded to their outer ends.
In witness whereof, I have hereunto set my hand this 17th da of November 1919.
OSC AR JUNGGREN'Q
US338997A 1919-06-27 1919-11-18 Elastic-fluid turbine Expired - Lifetime US1366667A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
US307184A US1366605A (en) 1919-06-27 1919-06-27 Blade-securing means and method of making the same
US31499719 US1366592A (en) 1919-06-27 1919-08-02 Elastic-fluid turbine
US338997A US1366667A (en) 1919-06-27 1919-11-18 Elastic-fluid turbine
FR519206A FR519206A (en) 1919-06-27 1920-06-21 Improvements in the manufacture and fixing methods of urban fins
FR23665A FR23665E (en) 1919-06-27 1920-07-29 Improvements in the manufacture and fixing methods of turbine fins
FR24760A FR24760E (en) 1919-06-27 1920-11-17 Improvements in the manufacture and fixing methods of turbine fins
DEG56548D DE393837C (en) 1919-06-27 1922-05-12 Attachment of turbine blades

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US307184A US1366605A (en) 1919-06-27 1919-06-27 Blade-securing means and method of making the same
US338997A US1366667A (en) 1919-06-27 1919-11-18 Elastic-fluid turbine

Publications (1)

Publication Number Publication Date
US1366667A true US1366667A (en) 1921-01-25

Family

ID=40343635

Family Applications (3)

Application Number Title Priority Date Filing Date
US307184A Expired - Lifetime US1366605A (en) 1919-06-27 1919-06-27 Blade-securing means and method of making the same
US31499719 Expired - Lifetime US1366592A (en) 1919-06-27 1919-08-02 Elastic-fluid turbine
US338997A Expired - Lifetime US1366667A (en) 1919-06-27 1919-11-18 Elastic-fluid turbine

Family Applications Before (2)

Application Number Title Priority Date Filing Date
US307184A Expired - Lifetime US1366605A (en) 1919-06-27 1919-06-27 Blade-securing means and method of making the same
US31499719 Expired - Lifetime US1366592A (en) 1919-06-27 1919-08-02 Elastic-fluid turbine

Country Status (3)

Country Link
US (3) US1366605A (en)
DE (1) DE393837C (en)
FR (3) FR519206A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2745171A (en) * 1949-09-08 1956-05-15 Niagara Blower Co Method of producing a bladed structure
US20140255194A1 (en) * 2012-12-21 2014-09-11 General Electric Company Tip shrouds of turbine rotor blades and methods of manufacture related thereto

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2454580A (en) * 1943-03-18 1948-11-23 Gen Electric Method of manufacturing bladed rotors
GB572916A (en) * 1944-04-18 1945-10-29 Armstrong Siddeley Motors Ltd Securing projections to a rotor
US2558976A (en) * 1947-04-10 1951-07-03 Charles M O'leary Rotary hydrokinetic torque converter with cooling system
CH349624A (en) * 1957-03-05 1960-10-31 Oerlikon Maschf Axial flow machine
DE1240093B (en) * 1964-02-15 1967-05-11 Demag Ag Process for the production of an impeller for axial turbines or compressors
US3985465A (en) * 1975-06-25 1976-10-12 United Technologies Corporation Turbomachine with removable stator vane
FR2514409B1 (en) * 1981-10-09 1986-03-21 Snecma DEVICE FOR LAYING BLADES IN SECTORS ON A TURBOMACHINE ROTOR DISC
US6203278B1 (en) 1999-02-17 2001-03-20 Lau Industries, Inc. Blower wheel with center disc having roughened blade engaging surface
EP1674734A1 (en) * 2004-12-21 2006-06-28 ALSTOM Technology Ltd Method for improving the flow stability of a turbo compressor
DE102005003511A1 (en) * 2005-01-26 2006-07-27 Mtu Aero Engines Gmbh Turbine engine rotor, especially gas turbine rotor e.g. air craft engine rotor, has groove with groove wall leg at side, in which blade root of rotor blades or rotor blade segments abut with corresponding support flanks

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2745171A (en) * 1949-09-08 1956-05-15 Niagara Blower Co Method of producing a bladed structure
US20140255194A1 (en) * 2012-12-21 2014-09-11 General Electric Company Tip shrouds of turbine rotor blades and methods of manufacture related thereto

Also Published As

Publication number Publication date
US1366605A (en) 1921-01-25
FR23665E (en) 1921-12-15
DE393837C (en) 1924-04-10
FR519206A (en) 1921-06-07
FR24760E (en) 1922-10-14
US1366592A (en) 1921-01-25

Similar Documents

Publication Publication Date Title
US1366667A (en) Elastic-fluid turbine
US2221685A (en) Elastic fluid turbine bucket unit
US1362074A (en) Turbine
US2454580A (en) Method of manufacturing bladed rotors
US2380276A (en) Welded structure
US1858067A (en) Elastic fluid turbine
US3572968A (en) Turbine bucket cover
US2326145A (en) Turbine blade fastening
US1466324A (en) Elastic-fluid turbine
US1470507A (en) Method of making rotor elements for elastic-fluid turbines
US1415266A (en) Elastic-fluid turbine
US2225769A (en) Turbine blade
US822801A (en) Turbine bucket-wheel.
US1118361A (en) Wheel for elastic-fluid turbines.
US2651495A (en) Turbine inlet structure
US1072457A (en) Blade-mounting.
US980732A (en) Bucket structure for turbines.
US1593393A (en) Elastic-fluid turbine and the like
US980562A (en) Turbine-bucket construction.
US1267229A (en) Elastic-fluid turbine.
US1842957A (en) Bridge band for blade groups of turbine rotors
US1470502A (en) Method of making blade rings for elastic-fluid turbines
US1247400A (en) Blading for elastic-fluid turbines.
US1640451A (en) Elastic-fluid turbine
US1118352A (en) Nozzles in elastic-fluid turbines.