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FR3004758B1 - Dispositif de maintien d'elements de forme allongee d'une turbomachine d'aeronef - Google Patents

Dispositif de maintien d'elements de forme allongee d'une turbomachine d'aeronef Download PDF

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Publication number
FR3004758B1
FR3004758B1 FR1353480A FR1353480A FR3004758B1 FR 3004758 B1 FR3004758 B1 FR 3004758B1 FR 1353480 A FR1353480 A FR 1353480A FR 1353480 A FR1353480 A FR 1353480A FR 3004758 B1 FR3004758 B1 FR 3004758B1
Authority
FR
France
Prior art keywords
shape elements
extended shape
aircraft turbomachine
maintaining extended
maintaining
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
FR1353480A
Other languages
English (en)
Other versions
FR3004758A1 (fr
Inventor
Tewfik Boudebiza
Arnaud Bergamaschi
Guillaume Marcillaud
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
SNECMA 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, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1353480A priority Critical patent/FR3004758B1/fr
Publication of FR3004758A1 publication Critical patent/FR3004758A1/fr
Application granted granted Critical
Publication of FR3004758B1 publication Critical patent/FR3004758B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F02C7/22—Fuel supply systems
    • F02C7/222—Fuel flow conduits, e.g. manifolds
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1353480A 2013-04-17 2013-04-17 Dispositif de maintien d'elements de forme allongee d'une turbomachine d'aeronef Active FR3004758B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1353480A FR3004758B1 (fr) 2013-04-17 2013-04-17 Dispositif de maintien d'elements de forme allongee d'une turbomachine d'aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1353480A FR3004758B1 (fr) 2013-04-17 2013-04-17 Dispositif de maintien d'elements de forme allongee d'une turbomachine d'aeronef
FR1353480 2013-04-17

Publications (2)

Publication Number Publication Date
FR3004758A1 FR3004758A1 (fr) 2014-10-24
FR3004758B1 true FR3004758B1 (fr) 2018-01-05

Family

ID=48570398

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1353480A Active FR3004758B1 (fr) 2013-04-17 2013-04-17 Dispositif de maintien d'elements de forme allongee d'une turbomachine d'aeronef

Country Status (1)

Country Link
FR (1) FR3004758B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3120391B1 (fr) * 2021-03-03 2023-11-03 Safran Aircraft Engines Systeme de maintien et de fixation d’un harnais electrique pour une turbomachine d’aeronef

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3023989A (en) * 1958-10-21 1962-03-06 James C White Clamp and clamp assembly
FR1230634A (fr) * 1959-04-03 1960-09-19 Raymond A Dispositif de fixation démontable de câbles électriques ou autres éléments sur des supports
AU517796B2 (en) * 1977-09-01 1981-08-27 Amp Incorporated Cable suspension clamp
US6038852A (en) * 1997-12-05 2000-03-21 United Technologies Corporation Wear resistant augmentor fuel manifold clamp
FR2909153B1 (fr) * 2006-11-24 2010-10-22 Snecma Dispositif pour la fixation d'un element

Also Published As

Publication number Publication date
FR3004758A1 (fr) 2014-10-24

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