CH538046A - Device for setting the tip clearance on turbomachines - Google Patents

Device for setting the tip clearance on turbomachines

Info

Publication number
CH538046A
CH538046A CH1625571A CH1625571A CH538046A CH 538046 A CH538046 A CH 538046A CH 1625571 A CH1625571 A CH 1625571A CH 1625571 A CH1625571 A CH 1625571A CH 538046 A CH538046 A CH 538046A
Authority
CH
Switzerland
Prior art keywords
turbomachines
setting
tip clearance
clearance
tip
Prior art date
Application number
CH1625571A
Other languages
German (de)
Inventor
Sidler Erwin
Original Assignee
Bbc Brown Boveri & Cie
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 Bbc Brown Boveri & Cie filed Critical Bbc Brown Boveri & Cie
Priority to CH1625571A priority Critical patent/CH538046A/en
Priority to DE2159080A priority patent/DE2159080C3/en
Priority to JP10150372A priority patent/JPS559522B2/ja
Priority to US00298235A priority patent/US3790299A/en
Priority to GB5161672A priority patent/GB1406098A/en
Priority to FR7239560A priority patent/FR2159378B3/fr
Priority to IT31403/72A priority patent/IT970271B/en
Publication of CH538046A publication Critical patent/CH538046A/en

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH1625571A 1971-11-10 1971-11-10 Device for setting the tip clearance on turbomachines CH538046A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
CH1625571A CH538046A (en) 1971-11-10 1971-11-10 Device for setting the tip clearance on turbomachines
DE2159080A DE2159080C3 (en) 1971-11-10 1971-11-29 Gap seal for a turbomachine with axial flow
JP10150372A JPS559522B2 (en) 1971-11-10 1972-10-09
US00298235A US3790299A (en) 1971-11-10 1972-10-17 Apparatus for adjusting tip clearance in fluid flow machines
GB5161672A GB1406098A (en) 1971-11-10 1972-11-08 Fluid flow machines
FR7239560A FR2159378B3 (en) 1971-11-10 1972-11-08
IT31403/72A IT970271B (en) 1971-11-10 1972-11-08 PROVISION FOR ADJUSTING THE PLAY OF PROFILES IN CONTINUOUS FLOW MACHINES

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1625571A CH538046A (en) 1971-11-10 1971-11-10 Device for setting the tip clearance on turbomachines

Publications (1)

Publication Number Publication Date
CH538046A true CH538046A (en) 1973-06-15

Family

ID=4415730

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1625571A CH538046A (en) 1971-11-10 1971-11-10 Device for setting the tip clearance on turbomachines

Country Status (7)

Country Link
US (1) US3790299A (en)
JP (1) JPS559522B2 (en)
CH (1) CH538046A (en)
DE (1) DE2159080C3 (en)
FR (1) FR2159378B3 (en)
GB (1) GB1406098A (en)
IT (1) IT970271B (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2119452A (en) * 1982-04-27 1983-11-16 Rolls Royce Shroud assemblies for axial flow turbomachine rotors
US4645417A (en) * 1984-02-06 1987-02-24 General Electric Company Compressor casing recess
US5333995A (en) * 1993-08-09 1994-08-02 General Electric Company Wear shim for a turbine engine
US6059525A (en) * 1998-05-19 2000-05-09 General Electric Co. Low strain shroud for a turbine technical field
US6315519B1 (en) 1998-09-28 2001-11-13 General Electric Company Turbine inner shroud and turbine assembly containing such inner shroud
DE50112597D1 (en) * 2001-04-12 2007-07-19 Siemens Ag Gas turbine with axially movable housing parts
FR2949810B1 (en) * 2009-09-04 2013-06-28 Turbomeca DEVICE FOR SUPPORTING A TURBINE RING, TURBINE WITH SUCH A DEVICE AND TURBOMOTOR WITH SUCH A TURBINE
FR2949809B1 (en) * 2009-09-04 2011-11-18 Turbomeca RING OF TURBINE, TURBINE WITH SUCH A RING AND TURBOMOTOR WITH SUCH A TURBINE
GB201309580D0 (en) * 2013-05-29 2013-07-10 Siemens Ag Rotor tip clearance
US10655491B2 (en) * 2017-02-22 2020-05-19 Rolls-Royce Corporation Turbine shroud ring for a gas turbine engine with radial retention features

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA468847A (en) * 1950-10-17 William Walton Morley Frederick Axial compressors
US2722373A (en) * 1951-02-06 1955-11-01 United Aircraft Corp Compressor casing and stator assembly
US2749026A (en) * 1951-02-27 1956-06-05 United Aircraft Corp Stator construction for compressors
DE1162384B (en) * 1959-07-10 1964-02-06 Licentia Gmbh Unslotted austenitic sealing ring for ferritic steam turbine housing

Also Published As

Publication number Publication date
FR2159378B3 (en) 1975-11-28
IT970271B (en) 1974-04-10
JPS4854307A (en) 1973-07-31
US3790299A (en) 1974-02-05
JPS559522B2 (en) 1980-03-11
DE2159080B2 (en) 1979-10-18
GB1406098A (en) 1975-09-17
DE2159080A1 (en) 1973-05-17
DE2159080C3 (en) 1980-07-03
FR2159378A1 (en) 1973-06-22

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Legal Events

Date Code Title Description
PL Patent ceased