IT8820275A0 - Dispositivo per mantenere la bocca anulare di uscita del convogliatore dei gas sempre centrata rispetto al gruppo ugelli di una turbina agas. - Google Patents

Dispositivo per mantenere la bocca anulare di uscita del convogliatore dei gas sempre centrata rispetto al gruppo ugelli di una turbina agas.

Info

Publication number
IT8820275A0
IT8820275A0 IT8820275A IT2027588A IT8820275A0 IT 8820275 A0 IT8820275 A0 IT 8820275A0 IT 8820275 A IT8820275 A IT 8820275A IT 2027588 A IT2027588 A IT 2027588A IT 8820275 A0 IT8820275 A0 IT 8820275A0
Authority
IT
Italy
Prior art keywords
keep
respect
outlet port
nozzle group
annular outlet
Prior art date
Application number
IT8820275A
Other languages
English (en)
Other versions
IT1216611B (it
Inventor
Vasco Mezzedimi
Franco Frosini
Original Assignee
Nuovo Pignone Spa
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 Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Priority to IT8820275A priority Critical patent/IT1216611B/it
Publication of IT8820275A0 publication Critical patent/IT8820275A0/it
Priority to CH1386/89A priority patent/CH675453A5/it
Priority to CA000596600A priority patent/CA1331100C/en
Priority to JP1097679A priority patent/JP2707134B2/ja
Priority to GB8908879A priority patent/GB2218157B/en
Priority to DE3913223A priority patent/DE3913223A1/de
Priority to FR898905309A priority patent/FR2630499B1/fr
Application granted granted Critical
Publication of IT1216611B publication Critical patent/IT1216611B/it
Priority to US07/622,181 priority patent/US5081833A/en

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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
IT8820275A 1988-04-21 1988-04-21 Dispositivo per mantenere la bocca anulare di uscita del convogliatore dei gas sempre centrata rispetto al gruppo ugelli di una turbina agas. IT1216611B (it)

Priority Applications (8)

Application Number Priority Date Filing Date Title
IT8820275A IT1216611B (it) 1988-04-21 1988-04-21 Dispositivo per mantenere la bocca anulare di uscita del convogliatore dei gas sempre centrata rispetto al gruppo ugelli di una turbina agas.
CH1386/89A CH675453A5 (it) 1988-04-21 1989-04-12
CA000596600A CA1331100C (en) 1988-04-21 1989-04-13 Device for keeping the annular outlet mouth of the gas volute always centered about the nozzle assembly in a gas turbine
JP1097679A JP2707134B2 (ja) 1988-04-21 1989-04-19 心決め装置
GB8908879A GB2218157B (en) 1988-04-21 1989-04-19 Improvements in gas turbines.
DE3913223A DE3913223A1 (de) 1988-04-21 1989-04-21 Vorrichtung zum staendigen halten der ringfoermigen auslassmuendung des gasausstroemraums zentriert um die duesenanordnung in einer gasturbine
FR898905309A FR2630499B1 (fr) 1988-04-21 1989-04-21 Dispositif pour maintenir centree la volute d'une turbine a gaz autour de l'ensemble de tuyeres de cette derniere
US07/622,181 US5081833A (en) 1988-04-21 1990-12-03 Device for keeping the annular outlet mouth of the gas volute always centered about the nozzle assembly in a gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT8820275A IT1216611B (it) 1988-04-21 1988-04-21 Dispositivo per mantenere la bocca anulare di uscita del convogliatore dei gas sempre centrata rispetto al gruppo ugelli di una turbina agas.

Publications (2)

Publication Number Publication Date
IT8820275A0 true IT8820275A0 (it) 1988-04-21
IT1216611B IT1216611B (it) 1990-03-08

Family

ID=11165353

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8820275A IT1216611B (it) 1988-04-21 1988-04-21 Dispositivo per mantenere la bocca anulare di uscita del convogliatore dei gas sempre centrata rispetto al gruppo ugelli di una turbina agas.

Country Status (7)

Country Link
JP (1) JP2707134B2 (it)
CA (1) CA1331100C (it)
CH (1) CH675453A5 (it)
DE (1) DE3913223A1 (it)
FR (1) FR2630499B1 (it)
GB (1) GB2218157B (it)
IT (1) IT1216611B (it)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1744014A1 (de) * 2005-07-13 2007-01-17 Siemens Aktiengesellschaft Befestigungseinrichtung der Turbinenleitschaufeln einer Gasturbinenanlage
JP4584080B2 (ja) * 2005-08-31 2010-11-17 株式会社日立製作所 再生式単缶ガスタービン
CN101548135B (zh) * 2006-03-15 2011-06-08 西门子公司 用于在燃气轮机内安装混合壳体的方法和为此的调整装置
RU2544020C1 (ru) * 2014-01-15 2015-03-10 Открытое акционерное общество "Газэнергосервис" Способ монтажа внутренних вставок корпуса турбины газоперекачивающего агрегата

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH354986A (de) * 1956-10-02 1961-06-15 Svenska Turbin Aktiebolaget Lj Gehäuse für eine durch ein elastisches Fluidum getriebene Turbine
US3609968A (en) * 1970-04-29 1971-10-05 Westinghouse Electric Corp Self-adjusting seal structure
GB2102897B (en) * 1981-07-27 1985-06-19 Gen Electric Annular seals
EP0118051B1 (de) * 1983-03-04 1988-02-03 BBC Brown Boveri AG Verbindung zwischen warmen und kalten Teilen bei ungekühlten Abgasturboladern

Also Published As

Publication number Publication date
CH675453A5 (it) 1990-09-28
GB8908879D0 (en) 1989-06-07
DE3913223A1 (de) 1989-11-02
GB2218157A (en) 1989-11-08
DE3913223C2 (it) 1991-07-11
FR2630499B1 (fr) 1991-11-22
FR2630499A1 (fr) 1989-10-27
JP2707134B2 (ja) 1998-01-28
IT1216611B (it) 1990-03-08
CA1331100C (en) 1994-08-02
GB2218157B (en) 1992-06-10
JPH01305133A (ja) 1989-12-08

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19970428