ES2585245B1 - Aeronave de baja carga alar - Google Patents
Aeronave de baja carga alar Download PDFInfo
- Publication number
- ES2585245B1 ES2585245B1 ES201630351A ES201630351A ES2585245B1 ES 2585245 B1 ES2585245 B1 ES 2585245B1 ES 201630351 A ES201630351 A ES 201630351A ES 201630351 A ES201630351 A ES 201630351A ES 2585245 B1 ES2585245 B1 ES 2585245B1
- Authority
- ES
- Spain
- Prior art keywords
- aircraft
- support surface
- low load
- low
- wing
- 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
- 238000005265 energy consumption Methods 0.000 abstract 1
- 239000003381 stabilizer Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/10—All-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/08—Stabilising surfaces mounted on, or supported by, wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/10—All-wing aircraft
- B64C2039/105—All-wing aircraft of blended wing body type
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Toys (AREA)
Abstract
Aeronave de baja carga alar, que comprende una superficie sustentadora (1) con una configuración en forma de ala, unos estabilizadores de la superficie sustentadora (1), y unos medios de propulsión (5) de la aeronave, en donde la superficie sustentadora (1) comprende una cubierta superior (11), una cubierta inferior (12), y dos largueros longitudinales (6) dispuestos entre las cubiertas superior (11) e inferior (12), y porque la superficie sustentadora (1) tiene una longitud mayor que su anchura, obteniéndose una aeronave con una baja relación entre el peso de la aeronave y la superficie sustentadora, menor resistencia aerodinámica y menor consumo energético, posibilitando menores distancias de despegue y aterrizaje, con una adecuada estabilidad.
Description
Claims (1)
-
imagen1 imagen2 imagen3
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES201630351A ES2585245B1 (es) | 2016-03-23 | 2016-03-23 | Aeronave de baja carga alar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES201630351A ES2585245B1 (es) | 2016-03-23 | 2016-03-23 | Aeronave de baja carga alar |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES2585245A1 ES2585245A1 (es) | 2016-10-04 |
| ES2585245B1 true ES2585245B1 (es) | 2017-03-17 |
Family
ID=57002683
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES201630351A Expired - Fee Related ES2585245B1 (es) | 2016-03-23 | 2016-03-23 | Aeronave de baja carga alar |
Country Status (1)
| Country | Link |
|---|---|
| ES (1) | ES2585245B1 (es) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20220411058A1 (en) * | 2021-06-25 | 2022-12-29 | Yongjie Zhang | Penetrating High Wing Structure of Civil Aircraft with Blended-Wing-Body |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB427186A (en) * | 1933-10-17 | 1935-04-17 | Petters Ltd | Improvements in or relating to tailless aeroplanes |
| US1980246A (en) * | 1933-12-08 | 1934-11-13 | Austin Gene | Airplane sky sled |
| US2108093A (en) * | 1935-04-30 | 1938-02-15 | Charles H Zimmerman | Aircraft |
| US2561291A (en) * | 1947-06-26 | 1951-07-17 | Scott C Rethorst | Roadable aircraft |
| US4440361A (en) * | 1980-11-18 | 1984-04-03 | Mcgann Rodney | Aircraft structure |
| US8292220B1 (en) * | 2009-03-19 | 2012-10-23 | Northrop Grumman Corporation | Flying wing aircraft with modular missionized elements |
| US8353478B1 (en) * | 2009-03-25 | 2013-01-15 | The Boeing Company | Blended wing aircraft |
| DE102010023938A1 (de) * | 2010-06-16 | 2011-12-22 | Eads Deutschland Gmbh | Angetriebenes Fluggerät, insbesondere als Nurflügler und/oder mit geringer Radarsignatur ausgebildetes Fluggerät |
| US20160009391A1 (en) * | 2013-11-04 | 2016-01-14 | Eric Walter Friesel | Stable Low Aspect Ratio Flying Wing |
| CN104029820A (zh) * | 2014-06-11 | 2014-09-10 | 青岛宇泰新能源科技有限公司 | 一种可长时间飞行的太阳能飞碟 |
-
2016
- 2016-03-23 ES ES201630351A patent/ES2585245B1/es not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20220411058A1 (en) * | 2021-06-25 | 2022-12-29 | Yongjie Zhang | Penetrating High Wing Structure of Civil Aircraft with Blended-Wing-Body |
Also Published As
| Publication number | Publication date |
|---|---|
| ES2585245A1 (es) | 2016-10-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| USD803724S1 (en) | Amphibious unmanned vertical takeoff and landing aircraft | |
| ES2404946B1 (es) | Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado | |
| IL260197A (en) | Hybrid propulsion vertical take-off and landing aircraft | |
| MX2010008030A (es) | Estructura de aspa retractil con borde de salida partido. | |
| ES2694229T8 (es) | Sistema pararrayos para palas de aerogenerador con un área efectiva de inyección en laminados de fibra de carbono y una distribución equilibrada de la intensidad y el voltaje de las corrientes de rayo entre distintos caminos conductores | |
| CN103847954A (zh) | 伸缩式机翼 | |
| JP6402463B2 (ja) | 伸縮マストにおける落雷時導通構造 | |
| IL291438A (en) | Damage mitigating for an aerial vehicle having a deployable parachute | |
| FR3041933B1 (fr) | Aeronef avec un ensemble propulsif comprenant un doublet d'helices a l'arriere du fuselage | |
| ES2512915A1 (es) | Ala deformable con extradós móvil | |
| PL3589543T3 (pl) | Statek powietrzny wyposażony w pomocniczy zespół lotu | |
| ES2585245B1 (es) | Aeronave de baja carga alar | |
| CY1119338T1 (el) | Εδραση γερανογεφυρας και γερανος για χρηση με την εδραση γερανογεφυρας | |
| FR3040686B1 (fr) | Partie arriere d'aeronef comprenant un stabilisateur vertical dont la structure formant caisson comporte une partie inferieure logee dans le fuselage | |
| ES2640739T3 (es) | Faldón de protección de un conductor de motocicleta | |
| BR112016012545A2 (pt) | Base de recipiente com pés | |
| FR3005033B1 (fr) | Structure de suspension d'un turbopropulseur a double helices non carenees sur un element structurel d'un aeronef | |
| ES2457717B1 (es) | Avión con motores y aletas en los extremos de las alas | |
| CL2018002917A1 (es) | Estructura politúnel. | |
| ES2547361A2 (es) | Helicóptero con estructura de aletas en radio de palanca y aletas en las hélices | |
| ES2435480B1 (es) | Conjunto de plataforma y vehículo aéreo no tripulado | |
| ES1245441Y (es) | Disposición sustentadora, estabilizadora y propulsora para aeronaves de despegue y aterrizaje vertical | |
| ES2554202B1 (es) | Ascensor con suplemento de techo de cabina | |
| ES1196335Y (es) | Sistema de sustentación, estabilización y propulsión para aeronaves eléctricas de despegue y aterrizaje vertical | |
| ES2644362A1 (es) | Vela de perfil aerodinámico con el borde de ataque y el borde de fuga permutables |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG2A | Definitive protection |
Ref document number: 2585245 Country of ref document: ES Kind code of ref document: B1 Effective date: 20170317 |
|
| FD2A | Announcement of lapse in spain |
Effective date: 20210930 |