GB473714A - Improvements in or relating to turbines - Google Patents

Improvements in or relating to turbines

Info

Publication number
GB473714A
GB473714A GB1920736A GB1920736A GB473714A GB 473714 A GB473714 A GB 473714A GB 1920736 A GB1920736 A GB 1920736A GB 1920736 A GB1920736 A GB 1920736A GB 473714 A GB473714 A GB 473714A
Authority
GB
United Kingdom
Prior art keywords
blades
plates
turbine
wheel
discs
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
GB1920736A
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.)
GEORGE JAMES VINCETT
Original Assignee
GEORGE JAMES VINCETT
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 GEORGE JAMES VINCETT filed Critical GEORGE JAMES VINCETT
Priority to GB1920736A priority Critical patent/GB473714A/en
Publication of GB473714A publication Critical patent/GB473714A/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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
    • 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/12—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines with repeated action on same blade ring
    • 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
    • F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae

Abstract

473,714. Elastic - fluid turbines. BURKE, P. W., and VINCETT, G. J. Jan. 18, 1937. No. 19207 /36. [Class 110 (iii)] Turbine discs and wheels are made up of a number of plates having blades formed by slotting, these slots being so formed that on assembly a crescent shaped blade of smooth contour is formed. A turbine wheel 10 is made up of plates 12, 13, 14 which are slotted at 24, 26, to form blades 22, 23. A modification, Fig. 4, shows a wheel 40 made up of blades 50 stamped from plates which are seated on ribs 46 between two end plates 42, 43. When used as fixed discs, the outside periphery 45 of the plates is extended in an axial direction so as to locate them in the turbine casing. The wheels and discs may be used in a turbine with the inner row of blades 23 for ahead running and the outer row 22 for astern. The wheel 10 may also be used in a turbine where the steam is first directed on to blades 23 and then on to blades 22. The plates may be secured together by bolts, rivets, or by welding, or a metal ring with inwardly directed flanges may be shrunk on their periphery. Specifications 16157/02 and 1657/03, [both in Class 110], are referred to.
GB1920736A 1937-01-18 1937-01-18 Improvements in or relating to turbines Expired GB473714A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1920736A GB473714A (en) 1937-01-18 1937-01-18 Improvements in or relating to turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1920736A GB473714A (en) 1937-01-18 1937-01-18 Improvements in or relating to turbines

Publications (1)

Publication Number Publication Date
GB473714A true GB473714A (en) 1937-10-19

Family

ID=10125502

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1920736A Expired GB473714A (en) 1937-01-18 1937-01-18 Improvements in or relating to turbines

Country Status (1)

Country Link
GB (1) GB473714A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2418829A (en) * 1943-09-30 1947-04-15 Gibbs Charles William Rotary motor
EP1204818A1 (en) * 1999-07-19 2002-05-15 Michael A. Wilson Efficiency enhanced turbine engine
JP2014521880A (en) * 2011-08-12 2014-08-28 ドレッサー ランド カンパニー Parallel cascade gas expander
CN105756716A (en) * 2016-04-22 2016-07-13 中国船舶重工集团公司第七�三研究所 Double-layer integral fixed blade ring for turbine capable of reversing
CN106567746A (en) * 2015-10-10 2017-04-19 熵零控股股份有限公司 Combined-flow impeller mechanism

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2418829A (en) * 1943-09-30 1947-04-15 Gibbs Charles William Rotary motor
EP1204818A1 (en) * 1999-07-19 2002-05-15 Michael A. Wilson Efficiency enhanced turbine engine
EP1204818A4 (en) * 1999-07-19 2005-04-27 Michael A Wilson Efficiency enhanced turbine engine
JP2014521880A (en) * 2011-08-12 2014-08-28 ドレッサー ランド カンパニー Parallel cascade gas expander
CN106567746A (en) * 2015-10-10 2017-04-19 熵零控股股份有限公司 Combined-flow impeller mechanism
CN105756716A (en) * 2016-04-22 2016-07-13 中国船舶重工集团公司第七�三研究所 Double-layer integral fixed blade ring for turbine capable of reversing

Similar Documents

Publication Publication Date Title
US3356339A (en) Turbine rotor
GB1040825A (en) Improvements in rotor blades and/or stator blades for gas turbine engines
US1998951A (en) Nozzle diaphragm
GB1008526A (en) Axial flow bladed rotor, e.g. for a turbine
GB1523668A (en) Turbomachinery stator assembly
GB1395957A (en) Fluid flow machines and rotors therefor
GB272837A (en) Improvements in and relating to reaction blading for turbines
US2394124A (en) Bladed body
US2945673A (en) Segmented stator ring assembly
GB1326122A (en) Blade securing arrangement for compressors and or turbines
GB473714A (en) Improvements in or relating to turbines
GB1437498A (en) Balde wheel for torque converter or fluid coupling
GB867759A (en) Stator vane assemblies for axial-flow compressors or turbines
GB1058759A (en) Improvements in or relating to the bladed diaphragms of turbines
GB1236366A (en) Elastic fluid machine
GB710119A (en) Improvements in or relating to turbines and compressors and the like machines
GB1121194A (en) Bladed rotor for a fluid flow machine
GB523038A (en) Hollow blade for exhaust gas turbine rotors
GB647143A (en) Improvements in or relating to turbine blades
US2073514A (en) Method of assembling packing rings in solid turbine rotors
GB925273A (en) Improvements relating to rotors for turbines or compressors
GB807231A (en) Securing means for blading of compressors or turbines
GB802667A (en) Improvements in or relating to a turbine wheel assembly for use with a gas turbine engine and method of manufacturing same
GB466259A (en) Improvements in and relating to turbo-blowers
GB476222A (en) Guiding means for turbo-machines