FR3023260B1 - Ensemble propulsif d'aeronef - Google Patents
Ensemble propulsif d'aeronefInfo
- Publication number
- FR3023260B1 FR3023260B1 FR1456408A FR1456408A FR3023260B1 FR 3023260 B1 FR3023260 B1 FR 3023260B1 FR 1456408 A FR1456408 A FR 1456408A FR 1456408 A FR1456408 A FR 1456408A FR 3023260 B1 FR3023260 B1 FR 3023260B1
- Authority
- FR
- France
- Prior art keywords
- aircraft assembly
- propellant
- propellant aircraft
- assembly
- aircraft
- 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
- 239000003380 propellant Substances 0.000 title 1
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
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/16—Aircraft characterised by the type or position of power plant of jet type
- B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
-
- 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
-
- 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
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/16—Aircraft characterised by the type or position of power plant of jet type
-
- B64D27/40—
-
- 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1456408A FR3023260B1 (fr) | 2014-07-03 | 2014-07-03 | Ensemble propulsif d'aeronef |
PCT/FR2015/051806 WO2016001581A1 (fr) | 2014-07-03 | 2015-07-01 | Ensemble propulsif d'aéronef |
US15/386,954 US9963999B2 (en) | 2014-07-03 | 2016-12-21 | Aircraft propulsion assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1456408A FR3023260B1 (fr) | 2014-07-03 | 2014-07-03 | Ensemble propulsif d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3023260A1 FR3023260A1 (fr) | 2016-01-08 |
FR3023260B1 true FR3023260B1 (fr) | 2016-07-15 |
Family
ID=51352677
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1456408A Active FR3023260B1 (fr) | 2014-07-03 | 2014-07-03 | Ensemble propulsif d'aeronef |
Country Status (3)
Country | Link |
---|---|
US (1) | US9963999B2 (fr) |
FR (1) | FR3023260B1 (fr) |
WO (1) | WO2016001581A1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3060532B1 (fr) * | 2016-12-20 | 2019-05-31 | Airbus Operations | Ensemble moteur pour aeronef, comprenant des dispositifs elastiques souples de transmission d'efforts entre des capots de nacelle et une structure annulaire reliee au carter moteur par des bielles |
US11697506B2 (en) * | 2020-05-15 | 2023-07-11 | General Electric Company | Methods and apparatus for gas turbine bending isolation |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3542826A1 (de) * | 1985-12-04 | 1987-06-11 | Mtu Muenchen Gmbh | Wellendichtungseinrichtung fuer turbomaschinen, insbesondere gasturbinentriebwerke |
GB9602130D0 (en) * | 1996-02-02 | 1996-04-03 | Rolls Royce Plc | Improved method of combining ducted fan gas turbine engine modules and aircraft structure |
US6821085B2 (en) * | 2002-09-30 | 2004-11-23 | General Electric Company | Turbine engine axially sealing assembly including an axially floating shroud, and assembly method |
FR2866070B1 (fr) * | 2004-02-05 | 2008-12-05 | Snecma Moteurs | Turboreacteur a fort taux de dilution |
FR2905991B1 (fr) * | 2006-09-20 | 2012-01-13 | Snecma | Systeme propulsif integre comportant un moteur a turboreacteur a double flux. |
FR2933070B1 (fr) * | 2008-06-25 | 2010-08-20 | Snecma | Systeme propulsif d'aeronef |
GB2525179B (en) * | 2014-04-14 | 2016-09-07 | Rolls Royce Plc | A panel connection system and a method of using the same |
-
2014
- 2014-07-03 FR FR1456408A patent/FR3023260B1/fr active Active
-
2015
- 2015-07-01 WO PCT/FR2015/051806 patent/WO2016001581A1/fr active Application Filing
-
2016
- 2016-12-21 US US15/386,954 patent/US9963999B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20170101895A1 (en) | 2017-04-13 |
WO2016001581A1 (fr) | 2016-01-07 |
FR3023260A1 (fr) | 2016-01-08 |
US9963999B2 (en) | 2018-05-08 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20160108 |
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PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
CD | Change of name or company name |
Owner name: SAFRAN NACELLES, FR Effective date: 20180125 |
|
PLFP | Fee payment |
Year of fee payment: 5 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |