FR3013330B1 - Aeronef comportant un reservoir d'huile deporte - Google Patents

Aeronef comportant un reservoir d'huile deporte

Info

Publication number
FR3013330B1
FR3013330B1 FR1361420A FR1361420A FR3013330B1 FR 3013330 B1 FR3013330 B1 FR 3013330B1 FR 1361420 A FR1361420 A FR 1361420A FR 1361420 A FR1361420 A FR 1361420A FR 3013330 B1 FR3013330 B1 FR 3013330B1
Authority
FR
France
Prior art keywords
deporte
aircraft
oil tank
tank
oil
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
FR1361420A
Other languages
English (en)
Other versions
FR3013330A1 (fr
Inventor
Jeremy Fert
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
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1361420A priority Critical patent/FR3013330B1/fr
Publication of FR3013330A1 publication Critical patent/FR3013330A1/fr
Application granted granted Critical
Publication of FR3013330B1 publication Critical patent/FR3013330B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16N—LUBRICATING
    • F16N19/00—Lubricant containers for use in lubricators or lubrication systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16N—LUBRICATING
    • F16N7/00—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated
    • F16N7/38—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated with a separate pump; Central lubrication systems
    • F16N7/40—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated with a separate pump; Central lubrication systems in a closed circulation system
    • 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
    • F05D2260/98—Lubrication
    • 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
FR1361420A 2013-11-20 2013-11-20 Aeronef comportant un reservoir d'huile deporte Active FR3013330B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1361420A FR3013330B1 (fr) 2013-11-20 2013-11-20 Aeronef comportant un reservoir d'huile deporte

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1361420A FR3013330B1 (fr) 2013-11-20 2013-11-20 Aeronef comportant un reservoir d'huile deporte

Publications (2)

Publication Number Publication Date
FR3013330A1 FR3013330A1 (fr) 2015-05-22
FR3013330B1 true FR3013330B1 (fr) 2017-03-17

Family

ID=49949917

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1361420A Active FR3013330B1 (fr) 2013-11-20 2013-11-20 Aeronef comportant un reservoir d'huile deporte

Country Status (1)

Country Link
FR (1) FR3013330B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3075272B1 (fr) 2017-12-20 2020-01-10 Safran Aircraft Engines Dispositif d'alimentation d'un reservoir d'huile a partir d'un second reservoir

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB546794A (en) * 1941-06-28 1942-07-30 Constant Speed Airscrews Ltd Improvements in fuel and oil tanks for aircraft
US4012012A (en) * 1975-10-30 1977-03-15 Lockheed Aircraft Corporation Supplemental oil system for engines
GB2302371A (en) * 1995-06-21 1997-01-15 Rolls Royce Plc Gas turbine engine cooling air system
GB0608983D0 (en) * 2006-05-06 2006-06-14 Rolls Royce Plc Aeroengine mount
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine

Also Published As

Publication number Publication date
FR3013330A1 (fr) 2015-05-22

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