GB8823094D0 - Clearance control between rotating & static components - Google Patents

Clearance control between rotating & static components

Info

Publication number
GB8823094D0
GB8823094D0 GB888823094A GB8823094A GB8823094D0 GB 8823094 D0 GB8823094 D0 GB 8823094D0 GB 888823094 A GB888823094 A GB 888823094A GB 8823094 A GB8823094 A GB 8823094A GB 8823094 D0 GB8823094 D0 GB 8823094D0
Authority
GB
United Kingdom
Prior art keywords
rotating
clearance control
static components
static
components
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.)
Pending
Application number
GB888823094A
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 GB888823094A priority Critical patent/GB8823094D0/en
Publication of GB8823094D0 publication Critical patent/GB8823094D0/en
Priority to GB8921959A priority patent/GB2225388B/en
Pending legal-status Critical Current

Links

GB888823094A 1988-10-01 1988-10-01 Clearance control between rotating & static components Pending GB8823094D0 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB888823094A GB8823094D0 (en) 1988-10-01 1988-10-01 Clearance control between rotating & static components
GB8921959A GB2225388B (en) 1988-10-01 1989-09-28 Improvements in tip clearance setting in gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB888823094A GB8823094D0 (en) 1988-10-01 1988-10-01 Clearance control between rotating & static components

Publications (1)

Publication Number Publication Date
GB8823094D0 true GB8823094D0 (en) 1988-11-09

Family

ID=10644589

Family Applications (2)

Application Number Title Priority Date Filing Date
GB888823094A Pending GB8823094D0 (en) 1988-10-01 1988-10-01 Clearance control between rotating & static components
GB8921959A Expired - Fee Related GB2225388B (en) 1988-10-01 1989-09-28 Improvements in tip clearance setting in gas turbine engines

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB8921959A Expired - Fee Related GB2225388B (en) 1988-10-01 1989-09-28 Improvements in tip clearance setting in gas turbine engines

Country Status (1)

Country Link
GB (2) GB8823094D0 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6755619B1 (en) * 2000-11-08 2004-06-29 General Electric Company Turbine blade with ceramic foam blade tip seal, and its preparation
US6533285B2 (en) 2001-02-05 2003-03-18 Caterpillar Inc Abradable coating and method of production
CH696854A5 (en) * 2003-04-14 2007-12-31 Alstom Technology Ltd Thermal turbomachinery.
US7811053B2 (en) 2005-07-22 2010-10-12 United Technologies Corporation Fan rotor design for coincidence avoidance
EP1820938A1 (en) * 2006-02-20 2007-08-22 ABB Turbo Systems AG Cleaning elements on blade tips of an exhaust turbine
US20130078084A1 (en) * 2011-09-23 2013-03-28 United Technologies Corporation Airfoil air seal assembly
DE102013212741A1 (en) * 2013-06-28 2014-12-31 Siemens Aktiengesellschaft Gas turbine and heat shield for a gas turbine
EP3088672A1 (en) * 2015-04-27 2016-11-02 Siemens Aktiengesellschaft Method for designing a fluid flow engine and fluid flow engine
US10400786B2 (en) 2016-11-07 2019-09-03 United Technologies Corporation Coated turbomachinery component
GB201801296D0 (en) * 2018-01-26 2018-03-14 Rolls Royce Plc Circumferental seal
US11299993B2 (en) * 2019-10-28 2022-04-12 Honeywell International Inc. Rotor assembly for in-machine grinding of shroud member and methods of using the same

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4169020A (en) * 1977-12-21 1979-09-25 General Electric Company Method for making an improved gas seal
US4390320A (en) * 1980-05-01 1983-06-28 General Electric Company Tip cap for a rotor blade and method of replacement
US4386112A (en) * 1981-11-02 1983-05-31 United Technologies Corporation Co-spray abrasive coating
DE3401742C2 (en) * 1984-01-19 1986-08-14 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Rotor for an axial compressor
FR2576301B1 (en) * 1985-01-24 1992-03-13 Europ Propulsion PROCESS FOR THE PREPARATION OF POROUS REFRACTORY MATERIALS, NOVEL PRODUCTS THUS OBTAINED AND THEIR APPLICATIONS IN THE PREPARATION OF ABRADABLE TURBINE RINGS

Also Published As

Publication number Publication date
GB2225388A (en) 1990-05-30
GB8921959D0 (en) 1989-11-15
GB2225388B (en) 1992-08-19

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