GB2165007B - Rotor and stator assembly for a gas turbine engine - Google Patents

Rotor and stator assembly for a gas turbine engine

Info

Publication number
GB2165007B
GB2165007B GB08036344A GB8036344A GB2165007B GB 2165007 B GB2165007 B GB 2165007B GB 08036344 A GB08036344 A GB 08036344A GB 8036344 A GB8036344 A GB 8036344A GB 2165007 B GB2165007 B GB 2165007B
Authority
GB
United Kingdom
Prior art keywords
rotor
gas turbine
turbine engine
stator assembly
stator
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
GB08036344A
Other versions
GB2165007A (en
Inventor
Robert Rudolph Moritz
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 GB08036344A priority Critical patent/GB2165007B/en
Publication of GB2165007A publication Critical patent/GB2165007A/en
Application granted granted Critical
Publication of GB2165007B publication Critical patent/GB2165007B/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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB08036344A 1980-11-11 1980-11-11 Rotor and stator assembly for a gas turbine engine Expired GB2165007B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08036344A GB2165007B (en) 1980-11-11 1980-11-11 Rotor and stator assembly for a gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08036344A GB2165007B (en) 1980-11-11 1980-11-11 Rotor and stator assembly for a gas turbine engine

Publications (2)

Publication Number Publication Date
GB2165007A GB2165007A (en) 1986-04-03
GB2165007B true GB2165007B (en) 1986-08-20

Family

ID=10517263

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08036344A Expired GB2165007B (en) 1980-11-11 1980-11-11 Rotor and stator assembly for a gas turbine engine

Country Status (1)

Country Link
GB (1) GB2165007B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5759012A (en) * 1996-12-13 1998-06-02 Caterpillar Inc. Turbine disc ingress prevention method and apparatus
DE10295864D2 (en) * 2001-12-14 2004-11-04 Alstom Technology Ltd Baden Gas turbine arrangement
US6832893B2 (en) 2002-10-24 2004-12-21 Pratt & Whitney Canada Corp. Blade passive cooling feature
DE102008011746A1 (en) * 2008-02-28 2009-09-03 Mtu Aero Engines Gmbh Device and method for diverting a leakage current
GB0905548D0 (en) * 2009-04-01 2009-05-13 Rolls Royce Plc A rotor arrangement

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2032531B (en) * 1978-10-26 1982-09-22 Rolls Royce Air cooled gas turbine rotor

Also Published As

Publication number Publication date
GB2165007A (en) 1986-04-03

Similar Documents

Publication Publication Date Title
GB2127906B (en) Rotor assembly e g for a gas turbine engine
IL67806A (en) Rotor assembly for gas turbine engine
DE3064862D1 (en) Stator vane assembly for a gas turbine engine
GB2151710B (en) Stator structure for a gas turbine engine
GB2169038B (en) Coolable stator assembly for a gas turbine engine
GB2220711B (en) Stator assembly for a gas turbine engine
GB2125111B (en) Shroud assembly for a gas turbine engine
GB2193125B (en) Gas turbine engine rotor assembly
GB2129882B (en) Gas turbine stator vane
GB2169356B (en) Coolable stator assembly for a gas turbine engine
GB2103294B (en) Shroud assembly for a gas turbine engine
GB2093126B (en) Rotor blade for a gas turbine engine
GB2093125B (en) Gas turbine engine casing
GB2171151B (en) Rotors for gas turbine engines
GB2078865B (en) A variable stator vane operating mechanism for a gas turbine engine
GB2043796B (en) Bladed rotor for gas turbine engine
DE3564847D1 (en) Hybrid gas turbine rotor
GB2033021B (en) Gas turbine stator casing
GB2119028B (en) Aerofoil for a gas turbine engine
GB2114661B (en) Casing structure for a gas turbine engine
GB2233394B (en) A gas turbine engine rotor assembly
GB2129501B (en) Gas turbine engine casing
IL56847A0 (en) Bearing clamping assembly for a gas turbine engine
GB8302880D0 (en) Combustion turbine single airfoil stator vane structure
GB2151711B (en) Stator structure for supporting an outer air seal in a gas turbine engine

Legal Events

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