FR3074522B1 - Partie de turbomachine carenee - Google Patents

Partie de turbomachine carenee Download PDF

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Publication number
FR3074522B1
FR3074522B1 FR1761607A FR1761607A FR3074522B1 FR 3074522 B1 FR3074522 B1 FR 3074522B1 FR 1761607 A FR1761607 A FR 1761607A FR 1761607 A FR1761607 A FR 1761607A FR 3074522 B1 FR3074522 B1 FR 3074522B1
Authority
FR
France
Prior art keywords
fairings
arm
downstream
upstream
turbomachine
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.)
Active
Application number
FR1761607A
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English (en)
Other versions
FR3074522A1 (fr
Inventor
Thierry KOHN
Damien CESAR
Julien SAYN-URPAR
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.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1761607A priority Critical patent/FR3074522B1/fr
Publication of FR3074522A1 publication Critical patent/FR3074522A1/fr
Application granted granted Critical
Publication of FR3074522B1 publication Critical patent/FR3074522B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention s'applique à une turbomachine comprenant un bras amont (9) et un bras aval (15) s'étendant en aval du bras amont par rapport à un flux d'air dans une veine (8), et un dispositif (19) de liaison aérodynamique comprenant des carénages (21a, 21b) s'étendant entre les bras amont et aval et des moyens (25) de maintien en place des carénages vis-à-vis des bras, lesquels comprennent des premiers organes (25a) de liaison entre le bras amont et les carénages, assurant au moins une fixation entre les carénages et un pincement du bras amont (9) entre lesdits carénages, et des seconds organes (25b) de liaison entre le bras aval et les carénages, assurant des fixations entre les carénages et le bras aval.
FR1761607A 2017-12-04 2017-12-04 Partie de turbomachine carenee Active FR3074522B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1761607A FR3074522B1 (fr) 2017-12-04 2017-12-04 Partie de turbomachine carenee

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1761607 2017-12-04
FR1761607A FR3074522B1 (fr) 2017-12-04 2017-12-04 Partie de turbomachine carenee

Publications (2)

Publication Number Publication Date
FR3074522A1 FR3074522A1 (fr) 2019-06-07
FR3074522B1 true FR3074522B1 (fr) 2019-11-29

Family

ID=61187493

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1761607A Active FR3074522B1 (fr) 2017-12-04 2017-12-04 Partie de turbomachine carenee

Country Status (1)

Country Link
FR (1) FR3074522B1 (fr)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080159856A1 (en) * 2006-12-29 2008-07-03 Thomas Ory Moniz Guide vane and method of fabricating the same
US8550776B2 (en) * 2010-07-28 2013-10-08 General Electric Company Composite vane mounting
US8690531B2 (en) * 2010-12-30 2014-04-08 General Electroc Co. Vane with spar mounted composite airfoil
FR3004749B1 (fr) * 2013-04-22 2015-05-08 Snecma Roue de stator, roue d'aubes de redresseur, turbomachine equipee d'une telle roue et procede de compensation de la distorsion dans une telle roue
FR3028893B1 (fr) * 2014-11-24 2019-11-08 Safran Aircraft Engines Structure de support de carter

Also Published As

Publication number Publication date
FR3074522A1 (fr) 2019-06-07

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