GB2002460B - Bladed rotor for a gas turbine engine - Google Patents

Bladed rotor for a gas turbine engine

Info

Publication number
GB2002460B
GB2002460B GB7830728A GB7830728A GB2002460B GB 2002460 B GB2002460 B GB 2002460B GB 7830728 A GB7830728 A GB 7830728A GB 7830728 A GB7830728 A GB 7830728A GB 2002460 B GB2002460 B GB 2002460B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
bladed rotor
bladed
rotor
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
GB7830728A
Other versions
GB2002460A (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 GB7830728A priority Critical patent/GB2002460B/en
Publication of GB2002460A publication Critical patent/GB2002460A/en
Application granted granted Critical
Publication of GB2002460B publication Critical patent/GB2002460B/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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001—Preventing 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)
GB7830728A 1977-08-09 1978-07-21 Bladed rotor for a gas turbine engine Expired GB2002460B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7830728A GB2002460B (en) 1977-08-09 1978-07-21 Bladed rotor for a gas turbine engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB3325377 1977-08-09
GB7830728A GB2002460B (en) 1977-08-09 1978-07-21 Bladed rotor for a gas turbine engine

Publications (2)

Publication Number Publication Date
GB2002460A GB2002460A (en) 1979-02-21
GB2002460B true GB2002460B (en) 1982-01-13

Family

ID=26261788

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7830728A Expired GB2002460B (en) 1977-08-09 1978-07-21 Bladed rotor for a gas turbine engine

Country Status (1)

Country Link
GB (1) GB2002460B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104420895A (en) * 2013-09-03 2015-03-18 航空技术空间股份有限公司 Turbomachine Axial Compressor Seal with a Brush Seal

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2251040B (en) * 1990-12-22 1994-06-22 Rolls Royce Plc Seal arrangement
DE19619725A1 (en) * 1996-05-15 1997-11-20 Siemens Ag Turbine blade, in particular for a steam turbine
JP2001152804A (en) * 1999-11-19 2001-06-05 Mitsubishi Heavy Ind Ltd Gas turbine facility and turbine blade
EP1508672A1 (en) * 2003-08-21 2005-02-23 Siemens Aktiengesellschaft Segmented fastening ring for a turbine
US20060275106A1 (en) * 2005-06-07 2006-12-07 Ioannis Alvanos Blade neck fluid seal
US20060275107A1 (en) * 2005-06-07 2006-12-07 Ioannis Alvanos Combined blade attachment and disk lug fluid seal
GB2452297B (en) * 2007-08-30 2010-01-06 Rolls Royce Plc A compressor
US20180223683A1 (en) * 2015-07-20 2018-08-09 Siemens Energy, Inc. Gas turbine seal arrangement

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104420895A (en) * 2013-09-03 2015-03-18 航空技术空间股份有限公司 Turbomachine Axial Compressor Seal with a Brush Seal

Also Published As

Publication number Publication date
GB2002460A (en) 1979-02-21

Similar Documents

Publication Publication Date Title
GB2028928B (en) Aerofoil blade for a gas turbine engine
GB2043796B (en) Bladed rotor for gas turbine engine
GB2017228B (en) Shroud for a turbine rotor
DE3064862D1 (en) Stator vane assembly for a gas turbine engine
GB1549152A (en) Rotor stage for a gas trubine engine
GB2030657B (en) Blade for gas turbine engine
GB1555587A (en) Aerofoil blade for a gas turbine engine
JPS54160911A (en) Blade for gas turbine engine
ZA771906B (en) An improvement in or relating to ceramic rotor blade assembly for a gas turbine engine
GB2100808B (en) Blade root modification for a gas turbine engine
JPS5327714A (en) Gas turbine rotor blade
GB2027866B (en) Gas turbine engine comounting
GB2019947A (en) Gas turbine engine combustor assembly
GB2093126B (en) Rotor blade for a gas turbine engine
JPS53131313A (en) Turbine for gas turbine engine
GB1551678A (en) Cooled rotor blade for a gas turbine engine
GB2006883B (en) Fan or compressor stage for a gas turbine engine
GB1551881A (en) Gas turbine engine powerplants
GB2007302B (en) Gas turbine engine
JPS52118117A (en) Rotor blade for gas turbine engine
JPS54101014A (en) Winggshaped blade for gas turbine engine
GB1552536A (en) Rotor blade for a gas turbine engine
JPS5582231A (en) Gas turbine engine combustor
GB2049069B (en) Rotor assembly for a gas turbine engine
GB2002460B (en) Bladed rotor for a gas turbine engine

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee