FR3092616B1 - DEVICE FOR FIXING AND MAINTAINING AT LEAST ONE PIPE ON A TURBOMACHINE ELEMENT - Google Patents

DEVICE FOR FIXING AND MAINTAINING AT LEAST ONE PIPE ON A TURBOMACHINE ELEMENT Download PDF

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Publication number
FR3092616B1
FR3092616B1 FR1901423A FR1901423A FR3092616B1 FR 3092616 B1 FR3092616 B1 FR 3092616B1 FR 1901423 A FR1901423 A FR 1901423A FR 1901423 A FR1901423 A FR 1901423A FR 3092616 B1 FR3092616 B1 FR 3092616B1
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FR
France
Prior art keywords
pipe
fixing
fixing support
maintaining
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
FR1901423A
Other languages
French (fr)
Other versions
FR3092616A1 (en
Inventor
Soufien Akachkachy
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 FR1901423A priority Critical patent/FR3092616B1/en
Publication of FR3092616A1 publication Critical patent/FR3092616A1/en
Application granted granted Critical
Publication of FR3092616B1 publication Critical patent/FR3092616B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • 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
    • F05D2240/90—Mounting on supporting structures or systems
    • F05D2240/91—Mounting on supporting structures or systems on a stationary structure
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position

Abstract

L’invention se rapporte à un dispositif de fixation et de maintien (100) d’au moins une conduite (10) sur un élément (2) de turbomachine, comportant : un élément de maintien (101) adapté pour recevoir et maintenir en position ladite conduite (10), un support de fixation (102) solidaire de l’élément de maintien (101) et destiné à être fixé sur l’élément (2) de turbomachine (1), le support de fixation (102) et comportant une première languette (1024) et une deuxième languette (1025) s’étendant de part et d’autre d’un corps central (1023) du support de fixation, lesdites languettes (1024, 1025) étant aptes à former des butées destinées à bloquer les mouvements de rotation dudit support de fixation (102) par rapport à l’élément (2) de la turbomachine. Figure à publier avec l’abrégé : Fig. 4The invention relates to a device for fixing and holding (100) at least one pipe (10) on a turbomachine element (2), comprising: a holding element (101) adapted to receive and hold in position said pipe (10), a fixing support (102) integral with the holding element (101) and intended to be fixed on the element (2) of the turbomachine (1), the fixing support (102) and comprising a first tongue (1024) and a second tongue (1025) extending on either side of a central body (1023) of the fixing support, the said tongues (1024, 1025) being adapted to form abutments intended to blocking the rotational movements of said fixing support (102) with respect to the element (2) of the turbine engine. Figure to be published with abstract: Fig. 4

FR1901423A 2019-02-13 2019-02-13 DEVICE FOR FIXING AND MAINTAINING AT LEAST ONE PIPE ON A TURBOMACHINE ELEMENT Active FR3092616B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1901423A FR3092616B1 (en) 2019-02-13 2019-02-13 DEVICE FOR FIXING AND MAINTAINING AT LEAST ONE PIPE ON A TURBOMACHINE ELEMENT

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1901423A FR3092616B1 (en) 2019-02-13 2019-02-13 DEVICE FOR FIXING AND MAINTAINING AT LEAST ONE PIPE ON A TURBOMACHINE ELEMENT
FR1901423 2019-02-13

Publications (2)

Publication Number Publication Date
FR3092616A1 FR3092616A1 (en) 2020-08-14
FR3092616B1 true FR3092616B1 (en) 2022-06-24

Family

ID=66776606

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1901423A Active FR3092616B1 (en) 2019-02-13 2019-02-13 DEVICE FOR FIXING AND MAINTAINING AT LEAST ONE PIPE ON A TURBOMACHINE ELEMENT

Country Status (1)

Country Link
FR (1) FR3092616B1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012000890A1 (en) * 2012-01-18 2013-07-18 Rolls-Royce Deutschland Ltd & Co Kg Fastening element and deicing device of an aircraft gas turbine engine
US20140075957A1 (en) * 2012-09-20 2014-03-20 United Technologies Corporation Formed gussets for brackets on gas turbine engines
FR3021700B1 (en) * 2014-05-27 2016-07-01 Snecma DEVICE FOR MAINTAINING A COOLING TUBE FOR A TURBOJET CARTRIDGE
US10711920B2 (en) * 2016-09-28 2020-07-14 General Electric Company Clamping device and an associated method thereof

Also Published As

Publication number Publication date
FR3092616A1 (en) 2020-08-14

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