FR2954277B1 - Suspension d'un turboreacteur a un aeronef - Google Patents
Suspension d'un turboreacteur a un aeronefInfo
- Publication number
- FR2954277B1 FR2954277B1 FR0959150A FR0959150A FR2954277B1 FR 2954277 B1 FR2954277 B1 FR 2954277B1 FR 0959150 A FR0959150 A FR 0959150A FR 0959150 A FR0959150 A FR 0959150A FR 2954277 B1 FR2954277 B1 FR 2954277B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- suspension
- turbojet engine
- turbojet
- engine
- 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
-
- 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
- B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0959150A FR2954277B1 (fr) | 2009-12-17 | 2009-12-17 | Suspension d'un turboreacteur a un aeronef |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0959150A FR2954277B1 (fr) | 2009-12-17 | 2009-12-17 | Suspension d'un turboreacteur a un aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2954277A1 FR2954277A1 (fr) | 2011-06-24 |
FR2954277B1 true FR2954277B1 (fr) | 2012-03-23 |
Family
ID=42315251
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0959150A Active FR2954277B1 (fr) | 2009-12-17 | 2009-12-17 | Suspension d'un turboreacteur a un aeronef |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2954277B1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140084129A1 (en) | 2012-09-27 | 2014-03-27 | United Technologies Corporation | Assembly for mounting a turbine engine case to a pylon |
CA2918320C (fr) | 2013-07-26 | 2018-05-15 | Mra Systems, Inc. | Mat d'accrochage de moteur pour aeronef |
FR3059298B1 (fr) * | 2016-11-29 | 2019-05-17 | Airbus Operations | Ensemble pour aeronef comprenant un moteur de type " open rotor puller " et des moyens d'accrochage de celui-ci a la structure rigide d'un mat d'accrochage |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2903382B1 (fr) * | 2006-07-10 | 2008-10-10 | Airbus France Sas | Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a emboitement transversal |
FR2915177B1 (fr) * | 2007-04-20 | 2009-07-10 | Airbus France Sa | Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif |
FR2931800B1 (fr) * | 2008-05-29 | 2010-07-30 | Airbus France | Dispositif de reprise des efforts de poussee pour mat d'accrochage de moteur d'aeronef, comprenant des bielles laterales a butees de palonnier integrees |
-
2009
- 2009-12-17 FR FR0959150A patent/FR2954277B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2954277A1 (fr) | 2011-06-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2924684B1 (fr) | Suspension d'un turboreacteur a un aeronef | |
FR2925016B1 (fr) | Suspension d'un turboreacteur a un aeronef | |
FR2941673B1 (fr) | Ensemble de suspension pour turboreacteur d'aeronef | |
FR2995282B1 (fr) | Pylone de montage d'un moteur a la structure d'un aeronef | |
FI20105169A (fi) | Polttomoottorin esikammiojärjestely | |
PL2635782T3 (pl) | Sposób optymalizacji jednostkowego zużycia paliwa przez śmigłowiec dwusilnikowy i dwusilnikowa konfiguracja z układem sterowania do jego wdrożenia | |
GB201005053D0 (en) | A gas turbine engine nose cone | |
ZA201403473B (en) | Improvement of a combustion engine | |
EP2710228A4 (fr) | Carénage d'une structure de turbine à gaz | |
FR2952922B1 (fr) | Ensemble de manutention d'un module de moteur d'aeronef | |
FR2972709B1 (fr) | Mat d'accrochage de moteur pour aeronef | |
FR2926788B1 (fr) | Fixation d'un turboreacteur multiflux a un aeronef | |
FR2926536B1 (fr) | Accrochage d'un systeme propulsif a un element de structure d'un aeronef | |
EP2900556A4 (fr) | Ensemble de montage d'un carter de moteur à turbine sur un pylône | |
FR2978989B1 (fr) | Cone d'ejection pour turboreacteur d'aeronef | |
FR2974593B1 (fr) | Moteur a turbine comportant une protection metallique d'une piece composite | |
FR2965796B1 (fr) | Suspension d'un moteur a un mat d'aeronef comportant un arceau de suspension | |
FR2917711B1 (fr) | Suspension d'un turbomoteur a la structure d'un aeronef | |
GB201102809D0 (en) | Pylon for attaching a gas turbine engine | |
FR2953563B1 (fr) | Installation d'alimentation en carburant d'un turboreacteur d'avion | |
FR2977237B1 (fr) | Carenage aerodynamique arriere d'un mat de liaison d'un moteur d'aeronef | |
FR2976974B1 (fr) | Dispositif d'assemblage de panneaux acoustiques d'une nacelle de turbomachine | |
EP2893172A4 (fr) | Ensemble de montage d'un moteur à turbine sur un pylône | |
FR2973339B1 (fr) | Dispositif de suspension d'une turbomachine a un avion | |
FR2978988B1 (fr) | Cone d'ejection pour turboreacteur d'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 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |