[go: up one dir, main page]

GB723405A - Improvements in or relating to blade-carrying turbine rotors and the like - Google Patents

Improvements in or relating to blade-carrying turbine rotors and the like

Info

Publication number
GB723405A
GB723405A GB32692/52A GB3269252A GB723405A GB 723405 A GB723405 A GB 723405A GB 32692/52 A GB32692/52 A GB 32692/52A GB 3269252 A GB3269252 A GB 3269252A GB 723405 A GB723405 A GB 723405A
Authority
GB
United Kingdom
Prior art keywords
pin
blade
root portion
rim
slot
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
Application number
GB32692/52A
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.)
Motors Liquidation Co
Original Assignee
General Motors Corp
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 Motors Corp filed Critical General Motors Corp
Publication of GB723405A publication Critical patent/GB723405A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32—Locking, e.g. by final locking blades or keys
    • F01D5/326—Locking of axial insertion type blades by other means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

723,405. Elastic-fluid turbines and compressors. GENERAL MOTORS CORPORATION. Dec. 24, 1952 [Dec. 26, 1951], No. 32692/52. Class 110 (3). In a turbine or compressor rotor wherein each blade has an enlarged root portion mounted in a slot in a support member by a pin which is carried by the rotor and enters an aperture in said root portion, the position and construction of the pin is such that the blade can be released from the slot by sliding it longitudinally thereof thereby causing the pin to shear part of the said root portion. In the compressor shown each rotor disc 14 comprises a thickened rim 30 and a spacing flange 32 the end of which engages a shoulder 36 on another disc 14. The discs 14 are interconnected by dowels 38 and by a tie bolt extending between the hubs of the end discs. The root portion 44 of each blade 16 is located in a dovetailed slot in the rim 30 and is locked therein. by a pin 50 which is frictionally retained within the rim 30. The rim 30 and the pin 50 are made of a material such as alloy steel which is stronger than the material of the root portion 44. The pin 50 bears against a lip 54 on the root which shears during axial displacement of the blade. The stator vanes 12 have tenons mounted in shrouds 18, 20; the shroud 20 comprising concentric channel members 24, 26 having superimposed webs spot welded together.
GB32692/52A 1951-12-26 1952-12-24 Improvements in or relating to blade-carrying turbine rotors and the like Expired GB723405A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US263436A US2935296A (en) 1951-12-26 1951-12-26 Blade retaining means

Publications (1)

Publication Number Publication Date
GB723405A true GB723405A (en) 1955-02-09

Family

ID=23001760

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32692/52A Expired GB723405A (en) 1951-12-26 1952-12-24 Improvements in or relating to blade-carrying turbine rotors and the like

Country Status (2)

Country Link
US (1) US2935296A (en)
GB (1) GB723405A (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3086697A (en) * 1958-05-12 1963-04-23 Ite Circuit Breaker Ltd Rotor design for aero-dynamic wave machine
US3039740A (en) * 1959-11-27 1962-06-19 Gen Motors Corp Blade retainer
CH406739A (en) * 1963-08-14 1966-01-31 Bbc Brown Boveri & Cie Pressure wave machine
US3295826A (en) * 1966-04-08 1967-01-03 Gen Motors Corp Blade lock
US3817655A (en) * 1972-11-22 1974-06-18 Carrier Corp Stator blade mounting structure for turbomachines
US4265595A (en) * 1979-01-02 1981-05-05 General Electric Company Turbomachinery blade retaining assembly
US4489468A (en) * 1982-06-24 1984-12-25 Elliott Turbomachinery Co., Inc. Method of providing a multivalve turbine nozzle ring interface seal
RU2143561C1 (en) * 1998-03-13 1999-12-27 Открытое акционерное общество "А.Люлька-Сатурн" Device for fixing compressor working blade in rotor slot
DE102005059084A1 (en) * 2005-12-10 2007-06-14 Mtu Aero Engines Gmbh Turbomachine, in particular gas turbine
GB0910752D0 (en) * 2009-06-23 2009-08-05 Rolls Royce Plc An annulus filler for a gas turbine engine
GB0914060D0 (en) * 2009-08-12 2009-09-16 Rolls Royce Plc A rotor assembly for a gas turbine
GB2478918B8 (en) * 2010-03-23 2013-06-19 Rolls Royce Plc Interstage seal
JP6118104B2 (en) * 2012-12-26 2017-04-19 川崎重工業株式会社 Propeller blade fixing mechanism
US20140199172A1 (en) * 2013-01-11 2014-07-17 General Electric Company Turbomachine and method of handling turbomachine components
AT518289B1 (en) * 2016-02-18 2018-06-15 Andritz Hydro Gmbh Pelton
EP4551824A1 (en) * 2022-07-07 2025-05-14 Siemens Energy Global GmbH & Co. KG Coupling joints to interconnect and transmit rotational torque between adjacent impeller bodies in a turbomachine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US741776A (en) * 1902-12-13 1903-10-20 Gen Electric Means for improving the efficiency of turbines.
US1095587A (en) * 1910-03-31 1914-05-05 George Mcintosh Turbine.
US1535417A (en) * 1924-07-05 1925-04-28 Ingersoll Rand Co Open impeller
US1959220A (en) * 1933-05-26 1934-05-15 Gen Electric Rotary disk turbine bucket wheel, or the like
US2483610A (en) * 1943-03-23 1949-10-04 Mini Of Supply Bladed impeller for turboblowers

Also Published As

Publication number Publication date
US2935296A (en) 1960-05-03

Similar Documents

Publication Publication Date Title
GB723405A (en) Improvements in or relating to blade-carrying turbine rotors and the like
GB715145A (en) Improvements in or relating to stator constructions for compressors
GB996729A (en) Improvements relating to turbines and compressors
GB1460714A (en) Bladed rotor for a gas turbine engine
GB1272200A (en) Axial-flow turbomachine rotors
GB1386590A (en) Turbine rotor
GB1500044A (en) Turbomachinery discs
GB837575A (en) Improvements in gas turbine rotor
GB1512882A (en) Bladed rotor assembly for a gas turbine engine
GB1187227A (en) Improvements in Bladed Rotors for Axial Flow Compressors, Turbines and the like
GB1266505A (en)
GB1217275A (en) Gas turbine engine axial flow multi-stage compressor
GB1326122A (en) Blade securing arrangement for compressors and or turbines
GB701263A (en) Improvements in or relating to turbo-machines
GB1141280A (en) Bladed rotor for a fluid flow machine
GB933047A (en) Improvements in rotor assembly for gas turbine engines
GB748903A (en) Blades for compressors, turbines and like bladed rotary machines
GB1450133A (en) Cooling of gas turbine engines
GB902064A (en) Blade damping means for compressors and turbines
GB1148339A (en) Compressors or turbines for gas turbine engines
GB1527074A (en) Bladed rotors
GB609322A (en) Improvements relating to axial-flow compressors and like machines, and blading thereof
GB706730A (en) Improvements relating to turbine rotors
GB677021A (en) Improved locking arrangement for axial-flow turbine and compressor blading
GB848465A (en) Rotors of multi-stage axial flow compressors or turbines