US2271971A - Turbine bucket wheel - Google Patents

Turbine bucket wheel Download PDF

Info

Publication number
US2271971A
US2271971A US377172A US37717241A US2271971A US 2271971 A US2271971 A US 2271971A US 377172 A US377172 A US 377172A US 37717241 A US37717241 A US 37717241A US 2271971 A US2271971 A US 2271971A
Authority
US
United States
Prior art keywords
bases
buckets
bucket
pair
bucket wheel
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
US377172A
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 US377172A priority Critical patent/US2271971A/en
Application granted granted Critical
Priority to GB1411/42A priority patent/GB555135A/en
Publication of US2271971A publication Critical patent/US2271971A/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
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type

Definitions

  • each bucket I l has a blade 20 and a base 2
  • the blades I8. and 20 of the buckets l6 and I1 01' each pair are identical.
  • of the buckets in accordance with my invention constitute mirror images to each other,
  • each base has a side 22 which in the assembly is located in a radial plane and a serrated or dovetailed side 23 in intermeshing relationship with one of the serrated sides l4, l5 of a groove.
  • the object of my invention is to provide an improved bucket wheel or like structure of the type above set forth whereby such structure may.
  • a bucket wheel structure in which pairs of separate buckets are held in serrated or dovetailed grooves.
  • the bases of each pair of buckets constitute mirror images relative to each other.
  • the base of one bucket of such pair is the same or substantially the same as the tion; and
  • Fig. 2 is a modification according to my invention.
  • the bucket wheel structure in Fig. 1 comprises a disk or like supporting member Ill with an outer rim II for supporting a plurality of buckets l2.
  • the rim has a plurality of axial grooves or slots I3 substantially V-shaped in cross section and with a circumferential width increasing in radial direction of the disk l0.
  • Each g-roove' has two serrated surfaces ll and IS inclined in opposite direction towards the radial plane through the center of the groove.
  • the buckets are arranged in pairs, each pair comprising a first bucket I6 and a second bucket l'l.
  • Each bucket It has a blade l8 and a base I9 gaging each other are inserted axially into the slots l3.
  • An upper portion of each base near the thin edges of the blades forms a projection 24 in engagement with the outer surface 25 of the rim intermediate adjacent slots l3 and with a similar projection of an adjacent bucket.
  • the arrangement of Fig. 2 comprises a pair of buckets with bases 26 and 21 corresponding to the bases l9 and 2
  • the bases 26, 21 have adjacent surfaces engaging each other.
  • the surface of the base 21 has radially spaced axial grooves or serrations 28 for receiving radially spaced projections 29 formed on the adjacent face of the base 21.
  • the other surfaces of the bases have serrations or grooves 30 and 3
  • the buckets may be prevented from axial movement by suitable known means such as peening-over portions of the rim of the disk.
  • Each bucket has a base with dovetailed, grooved or serrated portions in intermeshing relationship with correspondingly dovetailed, grooved or serrated portions of the disk.
  • the base of each bucket has a width increasing outwardly in radial direction, that is, in the direction towards the blade.
  • the means for securely connecting the buckets to the disk may also include serrated or grooved portions of adjacent bucket bases in intermeshing relationship with each other.
  • Opposite surfaces of the bases are inclined in opposite directions with respect to adjacent surfaces thereof.
  • the cross-sectional area of each base increases towards the end of the blade to which it is attached.
  • a grooved supporting member is secured to opposite surfaces of each pair of bases.
  • a turbine bucket wheel comprising a disk having a rim with a plurality of circumferentially spaced substantially V-shaped axial slots, each slot having a circumferential width increasing of pairs of buckets having blades and separate V-shaped bases with adjacent surfaces of the bases engaging each other and opposite serrated Sing-1088 meshing with the serrated sides of the s o 3.
  • a structure comprising a supporting member having V-shaped slots with serrations in both sides thereof, and pairs of separate buckets each having a blade and a base increasing in width towards the blade with adjacent surfaces of the bases of each pair engaging each other, one of the adjacent surfaces having a groove and the other of the adjacent surfaces having a projection filling the groove, the opposite surfaces of the bases of each pair being inclined in opposite directions towards the adjacent surfaces and having serrations intermesh-- ing with the serrations of the slots.
  • a bucket wheel structure comprising a supporting member having a rim with a plurality of axial grooved slots, each slot having a circumferential width increasing outwardly in radial direction, and a group of buckets each having a base with grooved sides, the grooved bases of each group of buckets filling one of the slots and being arranged in intermeshing relationship with each other and with the grooved slot.
  • a structure comprising a plurality of pairs of blades, pairs of separate bases attached to the ends of the pairs of blades, adjacent surfaces of the bases of each pair engaging,
  • each other and opposite surfaces of each pair of bases being inclined in opposite direction with respect to adjacent surfaces thereof, each pair of bases having a cross-sectional area increasing towards the ends of the blades to which they are attached, a support having a plurality of grooved portions, both bases of each pair of bases being disposed in and substantially filling 'the groove of a grooved portion, and means locking opposite surfaces of each pair of bases to opposite surfaces of such groove.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

Feb. 3, H DORAN TURBINE BUCKET WHEEL Filed Feb. 3, 1941 Inventor:
John H. Devan,
His Attorney.
Patented Feb.: 3, 1942 UNITED STATES PATENT OFFICE TURBINE BUCKET WHEEL John H. Doran, Scotla, N. Y., assignor to General Electric Company, a corporation or New York Application February 3, 1941, Serial no. 317,112-
Claims. ((1253-77) accurately machined to form a tight connection with the machined bases of the buckets. The machining of bucket wheels with narrow slots or grooves is diflicult and expensive when theparts are small and require very accurate machining Similarly each bucket I l has a blade 20 and a base 2|. The blades I8. and 20 of the buckets l6 and I1 01' each pair are identical. The bases I9 and 2| of the buckets in accordance with my invention constitute mirror images to each other,
that is, the bases l9 and 2| have the same shape but each base constitutes the image produced by a mirror of the other. Each base has a side 22 which in the assembly is located in a radial plane and a serrated or dovetailed side 23 in intermeshing relationship with one of the serrated sides l4, l5 of a groove. During assembly the pairs of. buckets with their plane surfaces 22 ento get good engagement on both sides of the dovetails.
The object of my invention is to provide an improved bucket wheel or like structure of the type above set forth whereby such structure may.
be readily produced at reduced manufacturing cost.
This is accomplished in accordance with my invention by the provision of a bucket wheel structure in which pairs of separate buckets are held in serrated or dovetailed grooves. In a preferred embodiment the bases of each pair of buckets constitute mirror images relative to each other. In other words, the base of one bucket of such pair is the same or substantially the same as the tion; and Fig. 2 is a modification according to my invention.
The bucket wheel structure in Fig. 1 comprises a disk or like supporting member Ill with an outer rim II for supporting a plurality of buckets l2. The rim has a plurality of axial grooves or slots I3 substantially V-shaped in cross section and with a circumferential width increasing in radial direction of the disk l0. Each g-roove' has two serrated surfaces ll and IS inclined in opposite direction towards the radial plane through the center of the groove. The buckets are arranged in pairs, each pair comprising a first bucket I6 and a second bucket l'l. Each bucket It has a blade l8 and a base I9 gaging each other are inserted axially into the slots l3. An upper portion of each base near the thin edges of the blades forms a projection 24 in engagement with the outer surface 25 of the rim intermediate adjacent slots l3 and with a similar projection of an adjacent bucket.
The arrangement of Fig. 2 comprises a pair of buckets with bases 26 and 21 corresponding to the bases l9 and 2| of a'pair of buckets in Fig. 1. The bases 26, 21 have adjacent surfaces engaging each other. The surface of the base 21 has radially spaced axial grooves or serrations 28 for receiving radially spaced projections 29 formed on the adjacent face of the base 21. Thus the adjacent surfaces of the bases of this pair of buckets are interlocked. v The other surfaces of the bases have serrations or grooves 30 and 3| respectively in intermeshing relationship with corresponding serrations or grooves formed on a disk 32. The buckets may be prevented from axial movement by suitable known means such as peening-over portions of the rim of the disk.
Thus, with my invention I have accomplished :an improved construction of turbine bucket wheels and like structures. Briefly, a bucket wheel structure according to my invention comprises a supporting member or disk with a row of separate buckets secured thereto. Each bucket has a base with dovetailed, grooved or serrated portions in intermeshing relationship with correspondingly dovetailed, grooved or serrated portions of the disk. In the arrangement illustrated the base of each bucket has a width increasing outwardly in radial direction, that is, in the direction towards the blade. In addition, the means for securely connecting the buckets to the disk may also include serrated or grooved portions of adjacent bucket bases in intermeshing relationship with each other. With this in view, a bucket wheel according to my invention comprises a disk with a group or row of buckets viewpoint, a structure according to my invention comprises a plurality of pairs of blades with pairs of bases attached to the ends of the blades.
Opposite surfaces of the bases are inclined in opposite directions with respect to adjacent surfaces thereof. The cross-sectional area of each base increases towards the end of the blade to which it is attached. A grooved supporting member is secured to opposite surfaces of each pair of bases. With this arrangement the center-lines of gravity of the buckets pass substantially through the center portions of the supporting surfaces and with the bucket bases increasing in width towards the blades the latter exert only small bending forces on the bases, thus assuring a rigid construction which may be safely operated at comparatively high load.
Having described the method of operation of my invention, together with the-apparatus which I now consider to represent the best embodiment thereof, I desire to have it understood that the apparatus shown is uily 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 a turbine bucket wheel comprising a disk having a rim with a plurality of circumferentially spaced substantially V-shaped axial slots, each slot having a circumferential width increasing of pairs of buckets having blades and separate V-shaped bases with adjacent surfaces of the bases engaging each other and opposite serrated Sing-1088 meshing with the serrated sides of the s o 3. In a turbine, a structure comprising a supporting member having V-shaped slots with serrations in both sides thereof, and pairs of separate buckets each having a blade and a base increasing in width towards the blade with adjacent surfaces of the bases of each pair engaging each other, one of the adjacent surfaces having a groove and the other of the adjacent surfaces having a projection filling the groove, the opposite surfaces of the bases of each pair being inclined in opposite directions towards the adjacent surfaces and having serrations intermesh-- ing with the serrations of the slots.
4. A bucket wheel structure comprising a supporting member having a rim with a plurality of axial grooved slots, each slot having a circumferential width increasing outwardly in radial direction, and a group of buckets each having a base with grooved sides, the grooved bases of each group of buckets filling one of the slots and being arranged in intermeshing relationship with each other and with the grooved slot.
5.. In a turbine, a structure comprising a plurality of pairs of blades, pairs of separate bases attached to the ends of the pairs of blades, adjacent surfaces of the bases of each pair engaging,
each other and opposite surfaces of each pair of bases being inclined in opposite direction with respect to adjacent surfaces thereof, each pair of bases having a cross-sectional area increasing towards the ends of the blades to which they are attached, a support having a plurality of grooved portions, both bases of each pair of bases being disposed in and substantially filling 'the groove of a grooved portion, and means locking opposite surfaces of each pair of bases to opposite surfaces of such groove.
- JOHN H. DORAN.
US377172A 1941-02-03 1941-02-03 Turbine bucket wheel Expired - Lifetime US2271971A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US377172A US2271971A (en) 1941-02-03 1941-02-03 Turbine bucket wheel
GB1411/42A GB555135A (en) 1941-02-03 1942-02-03 Improvements in and relating to turbine bucket wheels

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US377172A US2271971A (en) 1941-02-03 1941-02-03 Turbine bucket wheel

Publications (1)

Publication Number Publication Date
US2271971A true US2271971A (en) 1942-02-03

Family

ID=23488056

Family Applications (1)

Application Number Title Priority Date Filing Date
US377172A Expired - Lifetime US2271971A (en) 1941-02-03 1941-02-03 Turbine bucket wheel

Country Status (2)

Country Link
US (1) US2271971A (en)
GB (1) GB555135A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2605996A (en) * 1949-10-20 1952-08-05 Gen Electric Bucket attachment for turbine wheels
US2613058A (en) * 1945-11-30 1952-10-07 Atkinson Joseph Cooled bladed rotor
US2649278A (en) * 1948-07-15 1953-08-18 Edward A Stalker Rotor construction for fluid machines
US2805838A (en) * 1950-06-22 1957-09-10 Power Jets Res & Dev Ltd Rotors for turbines and similarly bladed fluid flow machines
US3112915A (en) * 1961-12-22 1963-12-03 Gen Electric Rotor assembly air baffle
US4084922A (en) * 1976-12-27 1978-04-18 Electric Power Research Institute, Inc. Turbine rotor with pin mounted ceramic turbine blades
EP2617945A1 (en) * 2012-01-23 2013-07-24 MTU Aero Engines GmbH Rotor for a turbo machine
US20170175761A1 (en) * 2015-12-18 2017-06-22 United Technologies Corporation Gas turbine engine with short inlet and mistuned fan blades

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB696815A (en) * 1950-03-07 1953-09-09 Power Jets Res & Dev Ltd Improvements relating to bladed rotors for rotary power conversion machines
US2957675A (en) * 1956-05-07 1960-10-25 Gen Electric Damping means
GB2237846B (en) * 1989-11-09 1993-12-15 Rolls Royce Plc Rim parasitic weight reduction

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2613058A (en) * 1945-11-30 1952-10-07 Atkinson Joseph Cooled bladed rotor
US2649278A (en) * 1948-07-15 1953-08-18 Edward A Stalker Rotor construction for fluid machines
US2605996A (en) * 1949-10-20 1952-08-05 Gen Electric Bucket attachment for turbine wheels
US2805838A (en) * 1950-06-22 1957-09-10 Power Jets Res & Dev Ltd Rotors for turbines and similarly bladed fluid flow machines
US3112915A (en) * 1961-12-22 1963-12-03 Gen Electric Rotor assembly air baffle
US4084922A (en) * 1976-12-27 1978-04-18 Electric Power Research Institute, Inc. Turbine rotor with pin mounted ceramic turbine blades
EP2617945A1 (en) * 2012-01-23 2013-07-24 MTU Aero Engines GmbH Rotor for a turbo machine
US9657581B2 (en) 2012-01-23 2017-05-23 Mtu Aero Engines Gmbh Rotor for a turbomachine
US20170175761A1 (en) * 2015-12-18 2017-06-22 United Technologies Corporation Gas turbine engine with short inlet and mistuned fan blades
US10823192B2 (en) * 2015-12-18 2020-11-03 Raytheon Technologies Corporation Gas turbine engine with short inlet and mistuned fan blades

Also Published As

Publication number Publication date
GB555135A (en) 1943-08-05

Similar Documents

Publication Publication Date Title
US1719415A (en) Turbine-blade attachment
US2271971A (en) Turbine bucket wheel
US1362074A (en) Turbine
US2220918A (en) Elastic fluid turbine bucket wheel
US1793468A (en) Turbine blade
US2873088A (en) Lightweight rotor construction
US2277484A (en) Turbine blade construction
US2199243A (en) Elastic fluid turbine rotor
US2125697A (en) Centrifugal blower wheel
US2790620A (en) Multiple finger dovetail attachment for turbine bucket
US2405146A (en) Turbomachine
US4813850A (en) Integral side entry control stage blade group
US2461402A (en) Rotor for multistage axial flow compressors and turbines
US3656864A (en) Turbomachine rotor
US2906495A (en) Turbine blade with corrugated strut
US2781998A (en) Bladed rotors
US3508844A (en) Blade lock
US2225769A (en) Turbine blade
US2646920A (en) Rotary bladed or like assembly
US1366667A (en) Elastic-fluid turbine
US890635A (en) Elastic-fluid turbine.
US2918255A (en) Elastic fluid utilizing apparatus
US1551402A (en) Botob fob elastic-pi
US2036083A (en) Bucket wheel
US2240742A (en) Turbine blade attachment and method and apparatus therefor