FR2952614B1 - Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef - Google Patents
Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronefInfo
- Publication number
- FR2952614B1 FR2952614B1 FR0958124A FR0958124A FR2952614B1 FR 2952614 B1 FR2952614 B1 FR 2952614B1 FR 0958124 A FR0958124 A FR 0958124A FR 0958124 A FR0958124 A FR 0958124A FR 2952614 B1 FR2952614 B1 FR 2952614B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- turbomoteur
- suspension
- suspension beam
- 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
- 239000000725 suspension Substances 0.000 title 1
Classifications
-
- B64D27/40—
-
- B64D27/404—
-
- B64D27/406—
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0958124A FR2952614B1 (fr) | 2009-11-17 | 2009-11-17 | Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef |
EP10737561.0A EP2459446B1 (fr) | 2009-07-28 | 2010-07-27 | Poutre de suspension de turbomoteur a la structure d'un aeronef |
US13/387,534 US9321537B2 (en) | 2009-07-28 | 2010-07-27 | Beam for suspending a turboshaft engine from an aircraft structure |
CN2010800340198A CN102470928A (zh) | 2009-07-28 | 2010-07-27 | 用于从飞机结构悬置涡轮轴引擎的梁 |
RU2012107090/11A RU2571680C2 (ru) | 2009-07-28 | 2010-07-27 | Балка подвески турбинного двигателя к конструкции летательного аппарата |
PCT/EP2010/060856 WO2011012603A2 (fr) | 2009-07-28 | 2010-07-27 | Poutre de suspension de turbomoteur a la structure d'un aeronef |
BR112012001965A BR112012001965B8 (pt) | 2009-07-28 | 2010-07-27 | viga para a suspensão de um turbomotor na estrutura de uma aeronave, utilização de uma viga, e, aeronave |
CA2768085A CA2768085C (fr) | 2009-07-28 | 2010-07-27 | Poutre de suspension de turbomoteur a la structure d'un aeronef |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0958124A FR2952614B1 (fr) | 2009-11-17 | 2009-11-17 | Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2952614A1 FR2952614A1 (fr) | 2011-05-20 |
FR2952614B1 true FR2952614B1 (fr) | 2012-02-03 |
Family
ID=42199997
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0958124A Active FR2952614B1 (fr) | 2009-07-28 | 2009-11-17 | Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2952614B1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3026137B1 (fr) * | 2014-09-22 | 2019-03-15 | Safran Aircraft Engines | Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion |
FR3039204B1 (fr) * | 2015-07-24 | 2017-07-21 | Snecma | Ensemble de montage d'une turbomachine |
FR3049582B1 (fr) * | 2016-03-31 | 2023-01-13 | Snecma | Turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2919284B1 (fr) * | 2007-07-26 | 2010-09-24 | Snecma | Piece mecanique comportant un insert en materiau composite. |
FR2925016B1 (fr) * | 2007-12-12 | 2010-06-18 | Snecma | Suspension d'un turboreacteur a un aeronef |
-
2009
- 2009-11-17 FR FR0958124A patent/FR2952614B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2952614A1 (fr) | 2011-05-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2963315B1 (fr) | Helice d'aeronef | |
BRPI0818168A2 (pt) | aerogerador com duas hélices sucessivas. | |
FR2917711B1 (fr) | Suspension d'un turbomoteur a la structure d'un aeronef | |
JP2011507597A5 (ja) | 弁葉の展開を遅延させた弁および同弁を備えたシステム | |
EP2551187A4 (fr) | Bouchon, structure fixée utilisant celui-ci et avion doté de ladite structure fixée | |
BR112013009498A2 (pt) | pistão e disposição de cartucho com o mesmo | |
EP2554961A4 (fr) | Indicateur de gestion de température, et structure sur laquelle est fixé cet indicateur | |
JP2011175111A5 (fr) | ||
FR2924094B1 (fr) | Turboreacteur suspendu a un pylone d'aeronef | |
FR2961480B1 (fr) | Atterrisseur principal d'aeronef a deux balanciers articules sur la structure de l'aeronef. | |
BR112012001965A2 (pt) | viga para a suspensão de um turbomotor na estrutura de uma aeronave, utilização de uma viga, e, aeronave | |
BRPI0906171A2 (pt) | Nacela de aeronave | |
JP2012120780A5 (fr) | ||
FI20065092A (fi) | Ilma-aluksen siipi, kiinnitysjärjestely sekä välituki | |
BRPI0924184A2 (pt) | massas resistentes a ácidos, de consolidação hidráulica e o uso das mesmas | |
HK1187729A1 (zh) | 運動平台和包括運動平台的飛行器模擬器 | |
FR2961172B1 (fr) | Suspension d'un turbomoteur ou analogue a un pylone d'aeronef, a securite integree. | |
BR112013007230A2 (pt) | ''processo de cristalização pulverizável,particulas sólidas e uso''. | |
FR2933375B1 (fr) | Agencement de fuselage d'avion | |
FR2961481B1 (fr) | Atterrisseur principal d'aeronef a deux balanciers et structure a parallelogramme deformable. | |
FR2939766B1 (fr) | Pylone central d'aeronef. | |
FR2965588B1 (fr) | Ensemble propulsif d'aeronef | |
BRPI0908341A2 (pt) | Estrutura aerodinâmica com ondulações de choque assimétricas | |
FR2939405B1 (fr) | Troncon de fuselage d'aeronef | |
FR2952614B1 (fr) | Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 Owner name: MESSIER DOWTY SA, FR Effective date: 20170717 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
TQ | Partial transmission of property |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20200916 Owner name: SAFRAN LANDING SYSTEMS, FR Effective date: 20200916 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |