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US1068622A - Turbine-blading. - Google Patents

Turbine-blading. Download PDF

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Publication number
US1068622A
US1068622A US71494912A US1912714949A US1068622A US 1068622 A US1068622 A US 1068622A US 71494912 A US71494912 A US 71494912A US 1912714949 A US1912714949 A US 1912714949A US 1068622 A US1068622 A US 1068622A
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US
United States
Prior art keywords
slot
blades
turbine
undercut
blading
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
US71494912A
Inventor
Otto Banner
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.)
Ingersoll Rand Co
Original Assignee
Ingersoll Rand 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 Ingersoll Rand Co filed Critical Ingersoll Rand Co
Priority to US71494912A priority Critical patent/US1068622A/en
Application granted granted Critical
Publication of US1068622A publication Critical patent/US1068622A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F01D5/303Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides

Definitions

  • This invention relates to the construction of turbine rotors and more particularly to a means of securing the blades 'of such a rotor thereto.
  • the object of the present invention is to provide a strong and simple means for securing a series of blades in the periphery of such a rotor.
  • the rotor as shown comprises a disk 1 the outer edge of which is enlarged into a blade holding ring or rim 2 in the periphery of which, for its whole circumference .is an inverted T shaped undercut slot 3 1n which fit the correspondingly shaped bases 4 of the blades.
  • a second undercut slot is made transversely across the periphery of the rim 2, this slot extending in depth to the shoulders of the peripheral slot 3 and being of slightly greater length than the depth of one of the blades.
  • blade retaining blocks 7 are inserted into the slot 6 on each side of the blades. These blocks are 'of such a size and shape as to complete the peripheral slot 3, and their inner edges engage the bases of the last blade or blades and hold them in position. Radial movement of these blocks '7 is prevented by the fact that the slot 6 is undercut and is larger at the bottom than at the top while transverse movement is prevented by screws 8 which engage the lower part of the blocks and the rim 2.
  • Vhat I claim is:
  • a turbine rotor disk having an undercut slot in its periphery, and a second undercut slot transversely of said first slot and communicating therewith, blades having bases iitting in said peripheral slot, a fastening block on each side of said blades having projecting parts engaging the undercut portions of said transverse slot, and means to secure said blocks in position.
  • a turbine rotor disk having in its periphery an undercut slot with a retaining shoulder therein, and a second undercut slot transversely of said first slot and extending to the shoulder of said first slot, blades having bases fitting in said,
  • peripheral slot and blade retaining blocks on each side of said blades, having bases of greater width than the upper parts thereof to engage the undercut portions of said transverse slo-t and prevent radial movement of said blocks.

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

Description

TINTTEE STATES PATENT OFFTOE,
OTTO BANNER, OF EASTON, PENNSYLVANIA, ASSIGNOR T0 INGERSOLL-RAND COM- PANY, 0F NEW YORK, N. Y., A CORPORATION OF NEW JERSEY.
TURBINE-BLADING- Specification of Letters Patent.
Patented July 29, 1913.
Application filed. August 14, 1912. Serial No. 714,949.
To all whom t may concern:
Be it known that I, OTTO BANNER, a subject of the German Emperor, residing at Easton, in the county of Northampton and State of Pennsylvania, have invented a certain new and useful Improvement in Securing Devices for Turbine-Blading, of which the following is a specification.
This invention relates to the construction of turbine rotors and more particularly to a means of securing the blades 'of such a rotor thereto. i
The object of the present invention is to provide a strong and simple means for securing a series of blades in the periphery of such a rotor.
Tith this object in view I have devised a construction the practical embodiment of which is shown in the accompanying draw ings in whichu Figure l shows a side elevation partly in section, of a portion of a turbine rotor embodying my invention. Fig. 2 shows a section on the line II-II of Fig. 1 and Fig. 3 shows a transverse section through the rotor on the line III-III of Fig. 1.
The rotor as shown comprises a disk 1 the outer edge of which is enlarged into a blade holding ring or rim 2 in the periphery of which, for its whole circumference .is an inverted T shaped undercut slot 3 1n which fit the correspondingly shaped bases 4 of the blades. To allow the insertion of the bases of the blades in the slot 3 a second undercut slot is made transversely across the periphery of the rim 2, this slot extending in depth to the shoulders of the peripheral slot 3 and being of slightly greater length than the depth of one of the blades. In assembling the blades in the slot, they are dropped in radially at the transverse slot 6 and moved along into the slot 3, the shoul ders of the slot 3 engaging their bases and holding them against radial movement. To secure the last blade in position blade retaining blocks 7 are inserted into the slot 6 on each side of the blades. These blocks are 'of such a size and shape as to complete the peripheral slot 3, and their inner edges engage the bases of the last blade or blades and hold them in position. Radial movement of these blocks '7 is prevented by the fact that the slot 6 is undercut and is larger at the bottom than at the top while transverse movement is prevented by screws 8 which engage the lower part of the blocks and the rim 2. By this construction a fastening for the blades is obtained which does not depend for its resistance to the enormous centrifugal pull on the blades, on any threaded securing means, the undercut slot and retaining block fitting it providing a construction nearly as strong as an entirely continuous rim.
It is to be understood that the present showing and description discloses only one specified modification of my invention and other forms and modiiications are included in the spirit and scope of the invention as expressed in the claims.
Vhat I claim is:
1. In combination, a turbine rotor disk having an undercut slot in its periphery, and a second undercut slot transversely of said first slot and communicating therewith, blades having bases iitting in said peripheral slot, a fastening block on each side of said blades having projecting parts engaging the undercut portions of said transverse slot, and means to secure said blocks in position.
2. In combination, a turbine rotor disk having in its periphery an undercut slot with a retaining shoulder therein, and a second undercut slot transversely of said first slot and extending to the shoulder of said first slot, blades having bases fitting in said,
peripheral slot, and blade retaining blocks on each side of said blades, having bases of greater width than the upper parts thereof to engage the undercut portions of said transverse slo-t and prevent radial movement of said blocks.
In testimony whereof, I have hereunto set my hand.
OTTO BANNER. Witnesses:
ROBERT E. KIEFFER, GEORGE OUMBERLEDGE.
Copies of this patent may be obtained for five cents each, by addressing the Commissioner of Patents,
Washington, D. C.
US71494912A 1912-08-14 1912-08-14 Turbine-blading. Expired - Lifetime US1068622A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US71494912A US1068622A (en) 1912-08-14 1912-08-14 Turbine-blading.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US71494912A US1068622A (en) 1912-08-14 1912-08-14 Turbine-blading.

Publications (1)

Publication Number Publication Date
US1068622A true US1068622A (en) 1913-07-29

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Family Applications (1)

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US71494912A Expired - Lifetime US1068622A (en) 1912-08-14 1912-08-14 Turbine-blading.

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