FR3105296B1 - Réservoir de lubrification pour une turbomachine d’aéronef ou d’engin aérien autopropulsé - Google Patents
Réservoir de lubrification pour une turbomachine d’aéronef ou d’engin aérien autopropulsé Download PDFInfo
- Publication number
- FR3105296B1 FR3105296B1 FR1915260A FR1915260A FR3105296B1 FR 3105296 B1 FR3105296 B1 FR 3105296B1 FR 1915260 A FR1915260 A FR 1915260A FR 1915260 A FR1915260 A FR 1915260A FR 3105296 B1 FR3105296 B1 FR 3105296B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- aircraft
- self
- aerial vehicle
- propelled aerial
- 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
Links
- 238000005461 lubrication Methods 0.000 title abstract 2
- 238000007872 degassing Methods 0.000 abstract 2
- 239000000314 lubricant Substances 0.000 abstract 1
- 238000005192 partition Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M11/00—Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
- F01M11/0004—Oilsumps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D19/00—Degasification of liquids
- B01D19/0042—Degasification of liquids modifying the liquid flow
-
- 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
- F01D25/18—Lubricating arrangements
-
- 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
- F02C7/06—Arrangements of bearings; Lubricating
-
- 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
- F16N39/00—Arrangements for conditioning of lubricants in the lubricating system
- F16N39/002—Arrangements for conditioning of lubricants in the lubricating system by deaeration
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M11/00—Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
- F01M11/0004—Oilsumps
- F01M2011/0033—Oilsumps with special means for guiding the return of oil into the sump
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M11/00—Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
- F01M11/0004—Oilsumps
- F01M2011/0037—Oilsumps with different oil compartments
- F01M2011/0041—Oilsumps with different oil compartments for accommodating movement or position of engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M11/00—Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
- F01M11/0004—Oilsumps
- F01M2011/007—Oil pickup tube to oil pump, e.g. strainer
-
- 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
-
- 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
- F16N2210/00—Applications
- F16N2210/02—Turbines
-
- 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
- F16N2210/00—Applications
- F16N2210/08—Aircraft
- F16N2210/09—Aircraft for inverted flight
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- General Details Of Gearings (AREA)
Abstract
L’invention concerne un réservoir (14) de lubrification pour une turbomachine d’aéronef ou d’engin aérien autopropulsé, comportant dans une partie inférieure (38) de ladite enceinte (26) une crépine d’aspiration (40), dans une partie supérieure (44) au moins un dispositif de dégazage (30) et au moins un évent (42), caractérisé en ce qu’il comporte, pour permettre l’alimentation de la crépine (40) et interdire l’intrusion d’un lubrifiant (28) dans ledit au moins un évent (42), au moins une première cloison (46) séparant la partie inférieure (38) de la partie supérieure (44) percée d’orifices calibrés (48), deux évents agencés de part et d’autre d’un plan médian vertical (P) de l’enceinte (26) et deux canalisations (50) d’évents, qui s’étendent dans la partie supérieure (44) en dessous du dispositif de dégazage (30), chaque canalisation (50) comportant un coude (56) et ayant ledit coude (56) situé de l’autre côté dudit plan médian (P) par rapport à son entrée. Figure pour l'abrégé : Figure 4.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1915260A FR3105296B1 (fr) | 2019-12-20 | 2019-12-20 | Réservoir de lubrification pour une turbomachine d’aéronef ou d’engin aérien autopropulsé |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1915260A FR3105296B1 (fr) | 2019-12-20 | 2019-12-20 | Réservoir de lubrification pour une turbomachine d’aéronef ou d’engin aérien autopropulsé |
FR1915260 | 2019-12-20 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3105296A1 FR3105296A1 (fr) | 2021-06-25 |
FR3105296B1 true FR3105296B1 (fr) | 2021-12-17 |
Family
ID=73497810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1915260A Active FR3105296B1 (fr) | 2019-12-20 | 2019-12-20 | Réservoir de lubrification pour une turbomachine d’aéronef ou d’engin aérien autopropulsé |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3105296B1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2022263728A2 (fr) * | 2021-06-13 | 2022-12-22 | Safran Power Units | Reservoir de lubrification pour une turbomachine d'aeronef ou d'engin aerien autopropulse |
FR3127527B1 (fr) * | 2021-09-30 | 2023-09-01 | Safran Aircraft Engines | Reservoir auxiliaire d’huile pour une turbomachine d’aeronef |
EP4296475A1 (fr) * | 2022-06-24 | 2023-12-27 | Safran Aero Boosters | Reservoir d'huile avec compartiment inférieur ayant un conduit de depart d'huile compatible g négatif |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3016912A (en) * | 1959-12-14 | 1962-01-16 | United Aircraft Prod | Vented liquid storage tank with priority system of supply |
GB1339825A (en) * | 1971-07-07 | 1973-12-05 | Rolls Royce | Liquid supply systems |
FR2687329B1 (fr) | 1992-02-19 | 1994-05-06 | Snecma | Desaerateur d'huile par centrifugation. |
US8312969B2 (en) * | 2010-06-29 | 2012-11-20 | Pratt & Whitney Canada Corp. | Lubrication system for aircraft engine |
US20140174093A1 (en) * | 2012-12-20 | 2014-06-26 | Solar Turbines Incorporated | Gas turbine engine lube oil system |
GB201807265D0 (en) * | 2018-05-03 | 2018-06-20 | Rolls Royce Plc | Oil tank system |
-
2019
- 2019-12-20 FR FR1915260A patent/FR3105296B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3105296A1 (fr) | 2021-06-25 |
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Effective date: 20210625 |
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