GB9604567D0 - Shroud assembly - Google Patents

Shroud assembly

Info

Publication number
GB9604567D0
GB9604567D0 GBGB9604567.9A GB9604567A GB9604567D0 GB 9604567 D0 GB9604567 D0 GB 9604567D0 GB 9604567 A GB9604567 A GB 9604567A GB 9604567 D0 GB9604567 D0 GB 9604567D0
Authority
GB
United Kingdom
Prior art keywords
shroud assembly
shroud
assembly
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.)
Withdrawn
Application number
GBGB9604567.9A
Other versions
GB2310895A (en
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB9604567A priority Critical patent/GB2310895A/en
Publication of GB9604567D0 publication Critical patent/GB9604567D0/en
Publication of GB2310895A publication Critical patent/GB2310895A/en
Withdrawn legal-status Critical Current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
    • 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
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • 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
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb
GB9604567A 1996-03-04 1996-03-04 Turbine shroud assembly Withdrawn GB2310895A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9604567A GB2310895A (en) 1996-03-04 1996-03-04 Turbine shroud assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9604567A GB2310895A (en) 1996-03-04 1996-03-04 Turbine shroud assembly

Publications (2)

Publication Number Publication Date
GB9604567D0 true GB9604567D0 (en) 1996-05-01
GB2310895A GB2310895A (en) 1997-09-10

Family

ID=10789810

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9604567A Withdrawn GB2310895A (en) 1996-03-04 1996-03-04 Turbine shroud assembly

Country Status (1)

Country Link
GB (1) GB2310895A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10140742B4 (en) 2000-12-16 2015-02-12 Alstom Technology Ltd. Device for sealing gap reduction between a rotating and a stationary component within an axial flow-through turbomachine
FR3095833B1 (en) * 2019-05-07 2021-05-28 Safran Helicopter Engines SEALING RING FOR AN AIRCRAFT TURBOMACHINE

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1008526A (en) * 1964-04-09 1965-10-27 Rolls Royce Axial flow bladed rotor, e.g. for a turbine

Also Published As

Publication number Publication date
GB2310895A (en) 1997-09-10

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)