FR2355183B1 - - Google Patents

Info

Publication number
FR2355183B1
FR2355183B1 FR7718178A FR7718178A FR2355183B1 FR 2355183 B1 FR2355183 B1 FR 2355183B1 FR 7718178 A FR7718178 A FR 7718178A FR 7718178 A FR7718178 A FR 7718178A FR 2355183 B1 FR2355183 B1 FR 2355183B1
Authority
FR
France
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
FR7718178A
Other versions
FR2355183A1 (fr
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.)
Nuovo Pignone SpA
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
Publication of FR2355183A1 publication Critical patent/FR2355183A1/fr
Application granted granted Critical
Publication of FR2355183B1 publication Critical patent/FR2355183B1/fr
Granted 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
FR7718178A 1976-06-15 1977-06-14 Systeme perfectionne pour verrouiller en position des aubes dans l'enveloppe de stator d'un compresseur axial fonctionnant en milieu poussiereux Granted FR2355183A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT24337/76A IT1062412B (it) 1976-06-15 1976-06-15 Sistema perfezionato di bloccaggio in posizione delle pale sulla casca statorica di un compressore assiale operante in ambiente pulverulento

Publications (2)

Publication Number Publication Date
FR2355183A1 FR2355183A1 (fr) 1978-01-13
FR2355183B1 true FR2355183B1 (fr) 1981-01-16

Family

ID=11213149

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7718178A Granted FR2355183A1 (fr) 1976-06-15 1977-06-14 Systeme perfectionne pour verrouiller en position des aubes dans l'enveloppe de stator d'un compresseur axial fonctionnant en milieu poussiereux

Country Status (14)

Country Link
US (1) US4142827A (fr)
JP (1) JPS52154112A (fr)
AR (1) AR210686A1 (fr)
BE (1) BE855715A (fr)
BR (1) BR7703782A (fr)
CA (1) CA1073362A (fr)
DE (1) DE2724003C3 (fr)
FR (1) FR2355183A1 (fr)
GB (1) GB1550018A (fr)
IT (1) IT1062412B (fr)
NL (1) NL167502C (fr)
SE (1) SE7705650L (fr)
SU (1) SU694098A3 (fr)
ZA (1) ZA773058B (fr)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4285633A (en) * 1979-10-26 1981-08-25 The United States Of America As Represented By The Secretary Of The Air Force Broad spectrum vibration damper assembly fixed stator vanes of axial flow compressor
US4832568A (en) * 1982-02-26 1989-05-23 General Electric Company Turbomachine airfoil mounting assembly
IT1167241B (it) * 1983-10-03 1987-05-13 Nuovo Pignone Spa Sistema perfezionato per il fissaggio degli ugelli statorici alla cassa di una turbina di potenza
US4907944A (en) * 1984-10-01 1990-03-13 General Electric Company Turbomachinery blade mounting arrangement
US4712979A (en) * 1985-11-13 1987-12-15 The United States Of America As Represented By The Secretary Of The Air Force Self-retained platform cooling plate for turbine vane
FR2671140B1 (fr) * 1990-12-27 1995-01-13 Snecma Aubage redresseur pour compresseur de turbomachine.
US5123813A (en) * 1991-03-01 1992-06-23 General Electric Company Apparatus for preloading an airfoil blade in a gas turbine engine
US5232340A (en) * 1992-09-28 1993-08-03 General Electric Company Gas turbine engine stator assembly
US5371973A (en) * 1992-09-30 1994-12-13 Western Atlas Inc. Grinding machine utilizing multiple, parallel, abrasive belts simultaneously grinding surfaces on a workpiece
US6413038B1 (en) 2000-11-03 2002-07-02 Donald Lord Windmill
US6733237B2 (en) * 2002-04-02 2004-05-11 Watson Cogeneration Company Method and apparatus for mounting stator blades in axial flow compressors
US6843638B2 (en) 2002-12-10 2005-01-18 Honeywell International Inc. Vane radial mounting apparatus
EP1548232A1 (fr) * 2003-12-23 2005-06-29 Siemens Aktiengesellschaft Turbomachine avec un stator et procédé de fixation d'aubes statoriques dans le stator
US7661924B2 (en) * 2007-03-28 2010-02-16 General Electric Company Method and apparatus for assembling turbine engines
FR2925107B1 (fr) * 2007-12-14 2010-01-22 Snecma Distributeur sectorise pour une turbomachine
EP2204547B1 (fr) * 2008-12-29 2013-12-11 Techspace Aero Virole extérieure et procédé de montage par soudage entre cette virole et une aube fixe
ATE556195T1 (de) * 2009-02-05 2012-05-15 Siemens Ag Ringförmige schaufelanordnung für einen gasturbinenmotor
US8550776B2 (en) 2010-07-28 2013-10-08 General Electric Company Composite vane mounting
US8734101B2 (en) 2010-08-31 2014-05-27 General Electric Co. Composite vane mounting
US8920112B2 (en) * 2012-01-05 2014-12-30 United Technologies Corporation Stator vane spring damper
US8899914B2 (en) * 2012-01-05 2014-12-02 United Technologies Corporation Stator vane integrated attachment liner and spring damper
US10378371B2 (en) 2014-12-18 2019-08-13 United Technologies Corporation Anti-rotation vane

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US930908A (en) * 1907-08-09 1909-08-10 George Westinghouse Elastic-fluid turbine.
CH124821A (de) * 1926-11-06 1928-03-01 Alfred Buechi Schaufelung für Gas- und Dampfturbinen.
GB620877A (en) * 1947-01-28 1949-03-31 Bristol Aeroplane Co Ltd Improvements in or relating to attachment means for the blades of fans, compressors,turbines or the like apparatus
US2786648A (en) * 1950-04-04 1957-03-26 United Aircraft Corp Blade locking device
US3045329A (en) * 1959-07-30 1962-07-24 Gen Electric Method for assembling tongue-and-groove members with locking keys
DE1476928A1 (de) * 1965-05-29 1969-07-31 Bergmann Borsig Veb Leitschaufelfuss fuer Turbinen mit hoher Eintrittstemperatur
US3849023A (en) * 1973-06-28 1974-11-19 Gen Electric Stator assembly
FR2275651A1 (fr) * 1974-06-21 1976-01-16 Snecma Perfectionnements aux stators de turbomachines axiales
US4019832A (en) * 1976-02-27 1977-04-26 General Electric Company Platform for a turbomachinery blade

Also Published As

Publication number Publication date
BE855715A (fr) 1977-12-15
IT1062412B (it) 1984-10-10
GB1550018A (en) 1979-08-08
JPS52154112A (en) 1977-12-21
AR210686A1 (es) 1977-08-31
ZA773058B (en) 1978-04-26
SU694098A3 (ru) 1979-10-25
CA1073362A (fr) 1980-03-11
US4142827A (en) 1979-03-06
NL167502C (nl) 1981-12-16
NL7706273A (nl) 1977-12-19
DE2724003A1 (de) 1977-12-22
DE2724003B2 (de) 1979-08-23
DE2724003C3 (de) 1980-05-14
BR7703782A (pt) 1978-03-21
NL167502B (nl) 1981-07-16
FR2355183A1 (fr) 1978-01-13
SE7705650L (sv) 1977-12-16

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Legal Events

Date Code Title Description
ST Notification of lapse