FR2041146A1 - - Google Patents
Info
- Publication number
- FR2041146A1 FR2041146A1 FR7012629A FR7012629A FR2041146A1 FR 2041146 A1 FR2041146 A1 FR 2041146A1 FR 7012629 A FR7012629 A FR 7012629A FR 7012629 A FR7012629 A FR 7012629A FR 2041146 A1 FR2041146 A1 FR 2041146A1
- Authority
- FR
- France
- 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.)
- Withdrawn
Links
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
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1824169 | 1969-04-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR2041146A1 true FR2041146A1 (fr) | 1971-01-29 |
Family
ID=10109086
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7012629A Withdrawn FR2041146A1 (fr) | 1969-04-09 | 1970-04-08 |
Country Status (2)
| Country | Link |
|---|---|
| DE (1) | DE2016805A1 (fr) |
| FR (1) | FR2041146A1 (fr) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2947244A1 (fr) * | 2009-06-25 | 2010-12-31 | Airbus | Aeronef subsonique |
| FR3068002A1 (fr) * | 2017-06-23 | 2018-12-28 | Airbus Operations (S.A.S.) | Fond etanche arriere presentant une membrane integrale a geometrie composee |
| US11878809B2 (en) | 2018-03-23 | 2024-01-23 | Airbus Operations S.A.S. | Aircraft propulsion assembly comprising two adjacent engines, of which the outlet nozzles have a straight portion in the vicinity of a median plane of the propulsion assembly |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2931799B1 (fr) | 2008-05-30 | 2010-12-24 | Airbus France | Avion a reacteurs arrieres. |
| US10017270B2 (en) * | 2015-10-09 | 2018-07-10 | General Electric Company | Aft engine for an aircraft |
-
1970
- 1970-04-08 FR FR7012629A patent/FR2041146A1/fr not_active Withdrawn
- 1970-04-08 DE DE19702016805 patent/DE2016805A1/de active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2947244A1 (fr) * | 2009-06-25 | 2010-12-31 | Airbus | Aeronef subsonique |
| FR3068002A1 (fr) * | 2017-06-23 | 2018-12-28 | Airbus Operations (S.A.S.) | Fond etanche arriere presentant une membrane integrale a geometrie composee |
| US11878809B2 (en) | 2018-03-23 | 2024-01-23 | Airbus Operations S.A.S. | Aircraft propulsion assembly comprising two adjacent engines, of which the outlet nozzles have a straight portion in the vicinity of a median plane of the propulsion assembly |
Also Published As
| Publication number | Publication date |
|---|---|
| DE2016805A1 (de) | 1970-10-15 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |