FR3114129B1 - Ensemble comportant une turbomachine d’aeronef et son pylone d’accrochage - Google Patents
Ensemble comportant une turbomachine d’aeronef et son pylone d’accrochage Download PDFInfo
- Publication number
- FR3114129B1 FR3114129B1 FR2009275A FR2009275A FR3114129B1 FR 3114129 B1 FR3114129 B1 FR 3114129B1 FR 2009275 A FR2009275 A FR 2009275A FR 2009275 A FR2009275 A FR 2009275A FR 3114129 B1 FR3114129 B1 FR 3114129B1
- Authority
- FR
- France
- Prior art keywords
- gas generator
- assembly
- turbine engine
- aircraft
- pylone
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 238000011144 upstream manufacturing Methods 0.000 abstract 1
- 210000003462 vein Anatomy 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Ensemble comportant une turbomachine (10) d’aéronef et un pylône (32) d’accrochage de la turbomachine à un élément de l’aéronef, la turbomachine ayant un axe longitudinal (A) et comportant un générateur de gaz (12) comprenant d’amont en aval, dans le sens d’écoulement des gaz, au moins un compresseur (14, 16), une chambre annulaire de combustion (18) et au moins une turbine (20, 22), le générateur de gaz définissant une veine annulaire principale d’écoulement d’un premier flux d’air, et le générateur de gaz étant destiné à être entouré par une veine annulaire secondaire d’écoulement d’un second flux d’air, le générateur de gaz comportant un élément de stator (26, 46) situé entre les veines principale et secondaire et au niveau dudit au moins un compresseur, le pylône ayant une forme générale allongée le long dudit axe et comportant des organes (42, 44) actifs de fixation de la turbomachine en porte-à-faux. Figure pour l'abrégé : Figure 6
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2009275A FR3114129B1 (fr) | 2020-09-14 | 2020-09-14 | Ensemble comportant une turbomachine d’aeronef et son pylone d’accrochage |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2009275A FR3114129B1 (fr) | 2020-09-14 | 2020-09-14 | Ensemble comportant une turbomachine d’aeronef et son pylone d’accrochage |
FR2009275 | 2020-09-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3114129A1 FR3114129A1 (fr) | 2022-03-18 |
FR3114129B1 true FR3114129B1 (fr) | 2022-08-05 |
Family
ID=73139029
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2009275A Active FR3114129B1 (fr) | 2020-09-14 | 2020-09-14 | Ensemble comportant une turbomachine d’aeronef et son pylone d’accrochage |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3114129B1 (fr) |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2969700B1 (fr) | 2010-12-23 | 2015-05-15 | Snecma | Systeme propulsif pour aeronef |
FR2987401B1 (fr) | 2012-02-28 | 2017-05-12 | Snecma | Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants. |
US9217337B2 (en) * | 2012-05-10 | 2015-12-22 | United Technologies Corporation | Adjustable engine mount |
FR3027875A1 (fr) * | 2014-10-30 | 2016-05-06 | Airbus Operations Sas | Dispositif de fixation d'un moteur d'aeronef, et aeronef correspondant |
FR3040076B1 (fr) * | 2015-08-13 | 2017-08-11 | Airbus Operations Sas | Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau |
FR3086924B1 (fr) * | 2018-10-08 | 2021-02-12 | Safran Aircraft Engines | Turbomachine comportant des moyens de suspension |
-
2020
- 2020-09-14 FR FR2009275A patent/FR3114129B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3114129A1 (fr) | 2022-03-18 |
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Legal Events
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Effective date: 20220318 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |