FR2928135B1 - Systeme de propulsion arriere d'avion a entrees d'air laterales escamotables et avion comportant un tel systeme. - Google Patents
Systeme de propulsion arriere d'avion a entrees d'air laterales escamotables et avion comportant un tel systeme.Info
- Publication number
- FR2928135B1 FR2928135B1 FR0851344A FR0851344A FR2928135B1 FR 2928135 B1 FR2928135 B1 FR 2928135B1 FR 0851344 A FR0851344 A FR 0851344A FR 0851344 A FR0851344 A FR 0851344A FR 2928135 B1 FR2928135 B1 FR 2928135B1
- Authority
- FR
- France
- Prior art keywords
- plane
- severable
- air intake
- side air
- propulsion system
- 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.)
- Expired - Fee Related
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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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
- B64D41/00—Power installations for auxiliary purposes
-
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0213—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for auxiliary power units (APU's)
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Jet Pumps And Other Pumps (AREA)
- Exhaust Gas After Treatment (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
Un système de propulsion d'un avion comportant un réacteur auxiliaire (5) est intégré dans un cône arrière (22) d'un fuselage (2).Des entrées d'air latérales (51a, 51b) comportent chacune une écope (71a, 71b) mobile entre une position fermée et une position ouverte associées à des canaux aérodynamiques (72a, 72b) pour alimenter en air le réacteur auxiliaire.Les canaux aérodynamiques se rejoignent au niveau d'un canal commun (73) comportant un volet mobile pour équilibrer les flux d'air provenant des entrées d'air lorsque le fonctionnement n'est pas symétrique.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0851344A FR2928135B1 (fr) | 2008-02-29 | 2008-02-29 | Systeme de propulsion arriere d'avion a entrees d'air laterales escamotables et avion comportant un tel systeme. |
US12/393,645 US8196861B2 (en) | 2008-02-29 | 2009-02-26 | Rear propulsion system with lateral air inlets for an aircraft with such system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0851344A FR2928135B1 (fr) | 2008-02-29 | 2008-02-29 | Systeme de propulsion arriere d'avion a entrees d'air laterales escamotables et avion comportant un tel systeme. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2928135A1 FR2928135A1 (fr) | 2009-09-04 |
FR2928135B1 true FR2928135B1 (fr) | 2010-09-03 |
Family
ID=39865382
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0851344A Expired - Fee Related FR2928135B1 (fr) | 2008-02-29 | 2008-02-29 | Systeme de propulsion arriere d'avion a entrees d'air laterales escamotables et avion comportant un tel systeme. |
Country Status (2)
Country | Link |
---|---|
US (1) | US8196861B2 (fr) |
FR (1) | FR2928135B1 (fr) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9534537B2 (en) | 2011-03-29 | 2017-01-03 | Rolls-Royce North American Technologies Inc. | Phase change material cooling system for a vehicle |
ES2398316B1 (es) * | 2011-07-18 | 2014-04-29 | Airbus Operations, S.L. | Sistema versátil de potencia en aeronaves |
FR2997681B1 (fr) * | 2012-11-08 | 2015-05-15 | Snecma | Avion propulse par un turboreacteur a soufflantes contrarotatives |
US9284063B2 (en) * | 2014-01-02 | 2016-03-15 | Hamilton Sundstrand Corporation | Tail cone driven emergency power generating system |
CN104590567A (zh) * | 2015-01-22 | 2015-05-06 | 谭现东 | 航空飞行器 |
FR3043727B1 (fr) * | 2015-11-16 | 2017-11-10 | Snecma | Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire |
FR3043725B1 (fr) * | 2015-11-16 | 2017-11-17 | Snecma | Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire |
FR3043728B1 (fr) * | 2015-11-16 | 2020-05-01 | Safran Aircraft Engines | Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire |
FR3043726B1 (fr) * | 2015-11-16 | 2020-05-01 | Safran Aircraft Engines | Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire |
FR3043729B1 (fr) * | 2015-11-16 | 2020-06-05 | Safran Aircraft Engines | Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire |
WO2017085406A1 (fr) * | 2015-11-16 | 2017-05-26 | Safran Aircraft Engines | Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire |
FR3043984B1 (fr) | 2015-11-25 | 2017-12-22 | Snecma | Avion propulse par une turbomachine muni d'un ecran acoustique |
US10661907B2 (en) * | 2016-11-17 | 2020-05-26 | Honeywell International Inc. | Hybrid pneumatic and electric secondary power integrated cabin energy system for a pressurized vehicle |
CN106741975A (zh) * | 2016-12-19 | 2017-05-31 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种全电驱动进气道斜板调节控制系统 |
US11519289B2 (en) * | 2019-12-06 | 2022-12-06 | Raytheon Technologies Corporation | Systems and methods for hybrid electric turbine engines |
US11073107B1 (en) | 2020-01-24 | 2021-07-27 | Raytheon Technologies Corporation | Systems and methods for hybrid electric turbine engines |
DE102021004807A1 (de) | 2020-10-07 | 2022-04-07 | Mathias Herrmann | Antriebskonzept zur Kombination von konventionellen Raketentriebwerken und luftatmenden Triebwerken (Heber-Konzept) |
DE102021004784A1 (de) | 2021-09-22 | 2023-03-23 | Mathias Herrmann | Adaptives Triebwerkskonzept (z.B. Raketen, Überschallraketenbrennkammern, luftatmende Triebwerke wie z.B. Düsentriebwerke, Unterschall- Staustahltriebwerken, Ramjets Scramjets, Dualmode, Pulsejets, Detonationsstriebwerke, Raketen-Staustrahl-Antriebe, Laval-/Düsen) und Strukturkonzept (z.B. für Flugzeuge und Raketen) für flexible und gezielt veränderliche Geometrien |
US20230123752A1 (en) * | 2021-10-20 | 2023-04-20 | Innoveering, LLC | Deployable inlet assembly for aerial vehicle |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1339453A (fr) * | 1962-11-26 | 1963-10-04 | Rolls Royce | Perfectionnements aux dispositifs propulsifs de sécurité destinés aux avions |
US3449891A (en) * | 1966-11-15 | 1969-06-17 | United Aircraft Corp | Engine inlet air particle separator |
GB1212875A (en) * | 1967-12-21 | 1970-11-18 | Rolls Royce | Aircraft |
DE1906157A1 (de) * | 1969-02-07 | 1970-08-13 | Messerschmitt Boelkow Blohm | Zusatzlufteinlassanordnung fuer die Triebwerke von Luft- und Raumfahrzeugen |
US5529263A (en) * | 1992-10-21 | 1996-06-25 | The Boeing Company | Supersonic airplane with subsonic boost engine means and method of operating the same |
US7014144B2 (en) * | 2003-07-22 | 2006-03-21 | Honeywell International, Inc. | Dual action inlet door and method for use thereof |
US20060163425A1 (en) * | 2005-01-27 | 2006-07-27 | Honeywell International, Inc. | Aircraft inlet assembly for reducing auxiliary power unit noise |
US7600713B2 (en) * | 2005-03-04 | 2009-10-13 | Honeywell International Inc. | Pre-hung inlet door system |
-
2008
- 2008-02-29 FR FR0851344A patent/FR2928135B1/fr not_active Expired - Fee Related
-
2009
- 2009-02-26 US US12/393,645 patent/US8196861B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2928135A1 (fr) | 2009-09-04 |
US8196861B2 (en) | 2012-06-12 |
US20100044504A1 (en) | 2010-02-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address |
Effective date: 20110916 |
|
CD | Change of name or company name |
Owner name: AIRBUS HOLDING, FR Effective date: 20110916 |
|
CJ | Change in legal form |
Effective date: 20110916 |
|
TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20110913 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
ST | Notification of lapse |
Effective date: 20211005 |