[go: up one dir, main page]

US1778066A - Elastic fluid turbine - Google Patents

Elastic fluid turbine Download PDF

Info

Publication number
US1778066A
US1778066A US358122A US35812229A US1778066A US 1778066 A US1778066 A US 1778066A US 358122 A US358122 A US 358122A US 35812229 A US35812229 A US 35812229A US 1778066 A US1778066 A US 1778066A
Authority
US
United States
Prior art keywords
bases
elastic fluid
bucket
fluid turbine
lugs
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
US358122A
Inventor
John H Doran
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
Application filed by General Electric Co filed Critical General Electric Co
Priority to US358122A priority Critical patent/US1778066A/en
Priority to FR694357D priority patent/FR694357A/en
Priority to GB12803/30A priority patent/GB347480A/en
Application granted granted Critical
Publication of US1778066A publication Critical patent/US1778066A/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

Definitions

  • the present invention relates to elasticfluid turbines and particularly relates to a construction of bucket dovetail attaching means which provides for heat expansion.
  • Hot steam entering the turbine may cause the ring of bucket bases to increase in circumference much faster than the wheel due to the more direct contact of the buckets with the steam.
  • the bucket bases as temperature conditions are varied, expand radially, laterally, and endwise. The radial and lateral. ex-
  • pansions are not material since only single short dimensions are involved.
  • the endwise expansion of the bucket bases is accumulative and constitutes the circumferential expansion of the ring or annulus of bases.
  • the endwise dimension involved is the circumference of the ring and as this is large the endwise expansion of several hundred buckets which make up a'ring becomes very material. WVhere the bucket bases form a tight fit there is no room for expansion to take place.
  • the bucket bases are restricted from expanding circumferentially they f produce heavy forces on the dovetail connections in aradial direction, tending to break the bucket bases or the dovetail lug of the wheel. Breakages usually occur at or near stages where hot steam may initially enter the turbine.
  • I provide base members 7 with cut-away portions 8 and 9 as shown in the drawing.
  • the cut-away portions 8 are disposed adjacent the center of one end surface of alternate bucket bases 7 forming marginal lugs 10 thereon.
  • the cut-away portions 9 are disposed adjacent to the outer edges of one end surface of the remaining bucket bases forming central lugs 11 thereon.
  • a, wheel a row of buckets having bases attached to the wheel, one-half of said bucket bases being provided with centrally located circumferentially projecting lugs and the other half of said bucket bases being provided with marginal circumferentially projecting lugs, said lugs serving to define spaces between the The bases having the cut-away bases whereby heat expansion of said bases may occur in a circumferential direction.
  • a wheel a row of buckets having bases attached to said wheel by an inverted dovetail joint, lugs defining spaces between said bases, said lugs comprising central circumferentially projecting base lugs which define one-half of said spaces, and marginal circumferentially pro- 10 jecting base lugs which define the other onehalf of said spaces whereby expansion of said bases may occur in a circumferential direction.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Distillation Of Fermentation Liquor, Processing Of Alcohols, Vinegar And Beer (AREA)

Description

Oct. 14, 1930. .1. H. DORAN ELASTIC FLUID TURBINE Filed April 25, 1929 Inventor. John H-DOY-21Y\, b His Attorneg Patented Oct. 14, 1930 UNITED STATES PAT NT? OFFICE JOHN H. nonan, or SCI-IENECTADY, new YORK, As'sren'on To GENERAL ELECTRIC COMPANY, A conronarroivor NEW YORK.
ELASTIC FLUID TURBINE Application filed April 25, 1929: fseriai No. 358,122.
The present invention relates to elasticfluid turbines and particularly relates to a construction of bucket dovetail attaching means which provides for heat expansion.
In turbine practice it is essential to obtain a rigidconstruction of the bucket bases and wheelswhich will withstand not only the stresses set up due to centrifugal action, but
also those Which'occur due to substantial ternperature changes which are continuously going on in the turbine by, virtue of changing conditions of such factors as load and vacuum. Hot steam entering the turbine may cause the ring of bucket bases to increase in circumference much faster than the wheel due to the more direct contact of the buckets with the steam. The bucket bases, as temperature conditions are varied, expand radially, laterally, and endwise. The radial and lateral. ex-
20. pansionsare not material since only single short dimensions are involved. However, the endwise expansion of the bucket bases is accumulative and constitutes the circumferential expansion of the ring or annulus of bases. The endwise dimension involved is the circumference of the ring and as this is large the endwise expansion of several hundred buckets which make up a'ring becomes very material. WVhere the bucket bases form a tight fit there is no room for expansion to take place. As the bucket bases are restricted from expanding circumferentially they f produce heavy forces on the dovetail connections in aradial direction, tending to break the bucket bases or the dovetail lug of the wheel. Breakages usually occur at or near stages where hot steam may initially enter the turbine.
. According to my invention I provide an improved structure and arrangement in a fas- Referring to the drawing, 5 indicates a turbine wheel carrying buckets 6. The base membersof the buckets are indicated at 7. They ar'e' formed with slits which provide legs which straddle the rim of the wheel and engage 1n grooves in: the sides of the rim. This is a known bucketfastening, means termed usually aninverted dovetail. connection.
According to my invention I provide base members 7 with cut-away portions 8 and 9 as shown in the drawing. The cut-away portions 8 are disposed adjacent the center of one end surface of alternate bucket bases 7 forming marginal lugs 10 thereon. The cut-away portions 9 are disposed adjacent to the outer edges of one end surface of the remaining bucket bases forming central lugs 11 thereon.
With the foregoing arrangement, when temperature changes take place during starting or changes of vacuum or load conditions the bucket bases expand into the cut-away portions and also may bow slightly to allow further expansion to take place without breakage. portion disposed adjacent the center of its end surface would bow in the direction of that surface. The remaining bases '7 would bendin the opposite direction.
It is obvious that other means may be employed in carrying out the present invention such as any provision. of bucket bases susceptible of yielding or elastic material in or between said bases.
I therefore do not desire that my invention shall be construed as limited to the specific structural details that are illustrated since they may be modified without departing from the spirit and scope of the invention as set forth in the appended claims.
What I claim as new and desire to secure by Letters Patent of the United States, is:
1. In an elastic fluid turbine, a, wheel, a row of buckets having bases attached to the wheel, one-half of said bucket bases being provided with centrally located circumferentially projecting lugs and the other half of said bucket bases being provided with marginal circumferentially projecting lugs, said lugs serving to define spaces between the The bases having the cut-away bases whereby heat expansion of said bases may occur in a circumferential direction.
2. In an elastic fluid turbine, a wheel, a row of buckets having bases attached to said wheel by an inverted dovetail joint, lugs defining spaces between said bases, said lugs comprising central circumferentially projecting base lugs which define one-half of said spaces, and marginal circumferentially pro- 10 jecting base lugs which define the other onehalf of said spaces whereby expansion of said bases may occur in a circumferential direction.
15 arrow of buckets fastened thereon, and lugs disposed intermediate the bases of said buckets, said lugs defining centrally disposed spaces between alternate adjacent base sides and marginally disposed spaces between the 20 remaining adjacent base sides whereby expansion of said bases may take place in a circumferential direction,
In witness whereof, I have hereunto set In hand this 24th day of April, 1929.
25 j JOHN H. DORAN.
3. In an elastic fluid turbine, a wheel with
US358122A 1929-04-25 1929-04-25 Elastic fluid turbine Expired - Lifetime US1778066A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US358122A US1778066A (en) 1929-04-25 1929-04-25 Elastic fluid turbine
FR694357D FR694357A (en) 1929-04-25 1930-04-24 Improvements to blade attachment systems in elastic fluid turbines
GB12803/30A GB347480A (en) 1929-04-25 1930-04-25 Improvements in and relating to elastic fluid turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US358122A US1778066A (en) 1929-04-25 1929-04-25 Elastic fluid turbine

Publications (1)

Publication Number Publication Date
US1778066A true US1778066A (en) 1930-10-14

Family

ID=23408387

Family Applications (1)

Application Number Title Priority Date Filing Date
US358122A Expired - Lifetime US1778066A (en) 1929-04-25 1929-04-25 Elastic fluid turbine

Country Status (3)

Country Link
US (1) US1778066A (en)
FR (1) FR694357A (en)
GB (1) GB347480A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9657581B2 (en) 2012-01-23 2017-05-23 Mtu Aero Engines Gmbh Rotor for a turbomachine

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025037A (en) * 1957-10-24 1962-03-13 Bert F Beckstrom Gas turbine
US4688992A (en) * 1985-01-25 1987-08-25 General Electric Company Blade platform

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9657581B2 (en) 2012-01-23 2017-05-23 Mtu Aero Engines Gmbh Rotor for a turbomachine

Also Published As

Publication number Publication date
GB347480A (en) 1931-04-30
FR694357A (en) 1930-12-03

Similar Documents

Publication Publication Date Title
US1554614A (en) Turbine blading
US2326145A (en) Turbine blade fastening
US1352278A (en) Elastic-fluid turbine
US1466324A (en) Elastic-fluid turbine
US1778066A (en) Elastic fluid turbine
US2294127A (en) Turbine nozzle chamber construction
US1831224A (en) Labyrinth packing
US1625541A (en) Elastic-fluid turbine
US1415266A (en) Elastic-fluid turbine
US890635A (en) Elastic-fluid turbine.
US1270232A (en) Elastic-fluid turbine.
US2036083A (en) Bucket wheel
US1680737A (en) Elastic-fluid turbine
US2281318A (en) Bladed structure
US1362437A (en) Elastic-fluid turbine
US1314806A (en) Turbine construction
US1267229A (en) Elastic-fluid turbine.
US2255486A (en) Elastic fluid turbine bucket wheel
US1949678A (en) Elastic fluid turbine
US1593393A (en) Elastic-fluid turbine and the like
US2256221A (en) Elastic fluid turbine casing
US2001492A (en) Method of assembling packing rings in turbine rotors
US1698327A (en) Elastic-fluid turbine
US1640451A (en) Elastic-fluid turbine
US3084343A (en) Compensating device for turbomachine bucket wheel