SE8300022D0 - Tetning for skiljeveggar i en kompressor - Google Patents

Tetning for skiljeveggar i en kompressor

Info

Publication number
SE8300022D0
SE8300022D0 SE8300022A SE8300022A SE8300022D0 SE 8300022 D0 SE8300022 D0 SE 8300022D0 SE 8300022 A SE8300022 A SE 8300022A SE 8300022 A SE8300022 A SE 8300022A SE 8300022 D0 SE8300022 D0 SE 8300022D0
Authority
SE
Sweden
Prior art keywords
seal
inner shroud
shroud
support structure
base
Prior art date
Application number
SE8300022A
Other languages
English (en)
Other versions
SE8300022L (sv
SE455219B (sv
Inventor
S F Arlington
L D Mclaurin
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of SE8300022D0 publication Critical patent/SE8300022D0/sv
Publication of SE8300022L publication Critical patent/SE8300022L/sv
Publication of SE455219B publication Critical patent/SE455219B/sv

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001Preventing 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
SE8300022A 1982-01-20 1983-01-03 Ledskenekrans for kompressor i en forbrenningsturbin SE455219B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US34103782A 1982-01-20 1982-01-20

Publications (3)

Publication Number Publication Date
SE8300022D0 true SE8300022D0 (sv) 1983-01-03
SE8300022L SE8300022L (sv) 1983-07-21
SE455219B SE455219B (sv) 1988-06-27

Family

ID=23336004

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8300022A SE455219B (sv) 1982-01-20 1983-01-03 Ledskenekrans for kompressor i en forbrenningsturbin

Country Status (9)

Country Link
JP (2) JPS58124025A (sv)
AR (1) AR229634A1 (sv)
BE (1) BE895651A (sv)
BR (1) BR8300073A (sv)
CA (1) CA1229306A (sv)
GB (1) GB2113772B (sv)
IT (1) IT1173652B (sv)
MX (1) MX154757A (sv)
SE (1) SE455219B (sv)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3631271B2 (ja) * 1993-11-19 2005-03-23 ユナイテッド テクノロジーズ コーポレイション インナーシュラウド一体型ステータベーン構造
US5584654A (en) * 1995-12-22 1996-12-17 General Electric Company Gas turbine engine fan stator
JP5091615B2 (ja) 2007-10-15 2012-12-05 三菱重工業株式会社 静翼環セグメントの組立方法、静翼環セグメント、結合部材、溶接方法

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5268613A (en) * 1975-12-04 1977-06-07 Agency Of Ind Science & Technol Cooling device for inner diameterside sealing material of nozzle-wing in turbo-fan engine

Also Published As

Publication number Publication date
BE895651A (fr) 1983-07-19
JPH0128245Y2 (sv) 1989-08-29
JPS62101042U (sv) 1987-06-27
JPS58124025A (ja) 1983-07-23
MX154757A (es) 1987-12-09
SE8300022L (sv) 1983-07-21
GB2113772B (en) 1985-10-09
GB2113772A (en) 1983-08-10
CA1229306A (en) 1987-11-17
IT8319068A0 (it) 1983-01-12
IT1173652B (it) 1987-06-24
SE455219B (sv) 1988-06-27
AR229634A1 (es) 1983-09-30
BR8300073A (pt) 1983-09-20
GB8300980D0 (en) 1983-02-16

Similar Documents

Publication Publication Date Title
IL58878A0 (en) Outer air seal support structure for gas turbine engine
IT7920610A0 (it) Supporto con parete di raffreddamento per urto della fascia di rotore di turbina a gas.
AR210412A1 (es) Conjunto de rotor para un motor de turbina de gas
ZA777122B (en) Inlet air cleaner assembly for turbine engines
AR213401A1 (es) Compresor centrifugo para un motor de turbina de gas
GB2019947B (en) Gas turbine engine combustor assembly
AT364961B (de) Brennkammer, insbesondere fuer gasturbinentriebwerke
GB2043796B (en) Bladed rotor for gas turbine engine
IT975686B (it) Rotore di turbina per turbine a gas particolarmente per autoveicoli
JPS5618032A (en) Cooling shroud for gas turbine engine
BE829703A (fr) Perfectionnements aux stators de turbomachines axiales
GB2016092B (en) Blade-retainer for the rotor of a turbo machine particularly an axial flow turbine
IL56847A0 (en) Bearing clamping assembly for a gas turbine engine
CA986321A (en) Rotor bearing for a gas turbine engine
IT8022694A0 (it) Diffusore particolarmente adattoper turbomotori a gas.
IT1169856B (it) Sistema di supporto per motori a turbina a gas turboalbero accoppiati
DE3069465D1 (en) Retaining structure for the compressor housing of a turbo engine
SE8300022D0 (sv) Tetning for skiljeveggar i en kompressor
GB2043791B (en) Gas turbine engine rotor thrust compensating
GB2018362B (en) Gas turbine engine cooling
CA1002034A (en) Pressurized strongback regenerator for gas turbine engines
AR207884A1 (es) Un rotor para un motor de turbina de gas
IT991920B (it) Dispositivo per la regolazione di turbine a gas
BR7705267A (pt) Vedacao do eixo para uma turbina a vapor
GB2011553A (en) Turbomachine casings

Legal Events

Date Code Title Description
NUG Patent has lapsed

Ref document number: 8300022-4

Effective date: 19910109

Format of ref document f/p: F