GB629770A - Improvements in or relating to sealing rings for turbines - Google Patents

Improvements in or relating to sealing rings for turbines

Info

Publication number
GB629770A
GB629770A GB3093547A GB3093547A GB629770A GB 629770 A GB629770 A GB 629770A GB 3093547 A GB3093547 A GB 3093547A GB 3093547 A GB3093547 A GB 3093547A GB 629770 A GB629770 A GB 629770A
Authority
GB
United Kingdom
Prior art keywords
rings
turbines
stator
secured
relating
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
GB3093547A
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.)
Napier Turbochargers Ltd
Original Assignee
D Napier and Son Ltd
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 D Napier and Son Ltd filed Critical D Napier and Son Ltd
Priority to GB3093547A priority Critical patent/GB629770A/en
Priority to FR975326D priority patent/FR975326A/en
Publication of GB629770A publication Critical patent/GB629770A/en
Expired legal-status Critical Current

Links

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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor

Landscapes

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

Abstract

629,770. Elastic-fluid turbines. NAPIER & SON, Ltd., D., and BARLOW, B. W. Nov. 21, 1947, No. 30935. [Class 110 (iii)] Flanges B<4> on turbine rotor discs B, B' co-act with the inwardly and outwardly directed lips of stationary rings F<1>, F<2> to form a leakage preventing device. The rings F<1>, F<2> which are bolted together at F<5> are supported by tangentially arranged links G. These are pivoted to the rings and to brackets E<1> formed on bridge pieces E each secured to the inner ends of two or more stator blades C. Alternatively the rings could be secured to the stator blades and selected blades supported from the stator by the arrangement of links.
GB3093547A 1947-11-21 1947-11-21 Improvements in or relating to sealing rings for turbines Expired GB629770A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB3093547A GB629770A (en) 1947-11-21 1947-11-21 Improvements in or relating to sealing rings for turbines
FR975326D FR975326A (en) 1947-11-21 1948-11-20 Improvement in turbine seals

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3093547A GB629770A (en) 1947-11-21 1947-11-21 Improvements in or relating to sealing rings for turbines

Publications (1)

Publication Number Publication Date
GB629770A true GB629770A (en) 1949-09-28

Family

ID=10315403

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3093547A Expired GB629770A (en) 1947-11-21 1947-11-21 Improvements in or relating to sealing rings for turbines

Country Status (2)

Country Link
FR (1) FR975326A (en)
GB (1) GB629770A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2671634A (en) * 1949-07-01 1954-03-09 Rolls Royce Adjustable stator blade and shroud ring arrangement for axial flow turbines and compressors
US4088422A (en) * 1976-10-01 1978-05-09 General Electric Company Flexible interstage turbine spacer
FR2603340A1 (en) * 1986-09-03 1988-03-04 Snecma TURBOMACHINE COMPRISING A DEVICE FOR ADJUSTING THE GAMES OF A LABYRINTH JOINT BETWEEN ROTOR AND STATOR AND OF THE GAS VEIN ALIGNMENT AND METHOD OF APPLICATION
EP0710766A1 (en) * 1994-11-05 1996-05-08 ROLLS-ROYCE plc Integral disc seal
GB2422641A (en) * 2005-01-28 2006-08-02 Rolls Royce Plc Vane having sealing part with a cavity
GB2469364A (en) * 2009-04-06 2010-10-13 Rolls Royce Plc A movable sealing assembly
WO2017014737A1 (en) * 2015-07-20 2017-01-26 Siemens Energy, Inc. Gas turbine seal arrangement

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE556215A (en) * 1956-03-28 1957-04-15

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2671634A (en) * 1949-07-01 1954-03-09 Rolls Royce Adjustable stator blade and shroud ring arrangement for axial flow turbines and compressors
US4088422A (en) * 1976-10-01 1978-05-09 General Electric Company Flexible interstage turbine spacer
FR2603340A1 (en) * 1986-09-03 1988-03-04 Snecma TURBOMACHINE COMPRISING A DEVICE FOR ADJUSTING THE GAMES OF A LABYRINTH JOINT BETWEEN ROTOR AND STATOR AND OF THE GAS VEIN ALIGNMENT AND METHOD OF APPLICATION
EP0259221A1 (en) * 1986-09-03 1988-03-09 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Labyrinth clearance adjustment for a turbo machine
US4773817A (en) * 1986-09-03 1988-09-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Labyrinth seal adjustment device for incorporation in a turbomachine
EP0710766A1 (en) * 1994-11-05 1996-05-08 ROLLS-ROYCE plc Integral disc seal
GB2422641A (en) * 2005-01-28 2006-08-02 Rolls Royce Plc Vane having sealing part with a cavity
GB2422641B (en) * 2005-01-28 2007-11-14 Rolls Royce Plc Vane for a gas turbine engine
US7695244B2 (en) 2005-01-28 2010-04-13 Rolls-Royce Plc Vane for a gas turbine engine
GB2469364A (en) * 2009-04-06 2010-10-13 Rolls Royce Plc A movable sealing assembly
GB2469364B (en) * 2009-04-06 2012-08-01 Rolls Royce Plc A sealing assembly
US8387991B2 (en) 2009-04-06 2013-03-05 Rolls-Royce Plc Sealing assembly
WO2017014737A1 (en) * 2015-07-20 2017-01-26 Siemens Energy, Inc. Gas turbine seal arrangement

Also Published As

Publication number Publication date
FR975326A (en) 1951-03-05

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