ES2031102T3 - Dispositivo para las trampillas de efecto aerodinamico en las alas sustentadoras de los aviones, sobre todo para los alerones-traseros. - Google Patents
Dispositivo para las trampillas de efecto aerodinamico en las alas sustentadoras de los aviones, sobre todo para los alerones-traseros.Info
- Publication number
- ES2031102T3 ES2031102T3 ES87114933T ES87114933T ES2031102T3 ES 2031102 T3 ES2031102 T3 ES 2031102T3 ES 87114933 T ES87114933 T ES 87114933T ES 87114933 T ES87114933 T ES 87114933T ES 2031102 T3 ES2031102 T3 ES 2031102T3
- Authority
- ES
- Spain
- Prior art keywords
- wings
- valve
- hatches
- valves
- aerodynamic effect
- 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 - Lifetime
Links
- SQEHCNOBYLQFTG-UHFFFAOYSA-M lithium;thiophene-2-carboxylate Chemical compound [Li+].[O-]C(=O)C1=CC=CS1 SQEHCNOBYLQFTG-UHFFFAOYSA-M 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Check Valves (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19863643808 DE3643808A1 (de) | 1986-12-20 | 1986-12-20 | Einrichtung fuer aerodynamisch arbeitende klappen an flugzeugtragfluegeln, insbesondere spaltklappen |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2031102T3 true ES2031102T3 (es) | 1992-12-01 |
Family
ID=6316808
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES87114933T Expired - Lifetime ES2031102T3 (es) | 1986-12-20 | 1987-10-13 | Dispositivo para las trampillas de efecto aerodinamico en las alas sustentadoras de los aviones, sobre todo para los alerones-traseros. |
Country Status (4)
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006036464B4 (de) * | 2006-08-04 | 2009-08-20 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
GB0708334D0 (en) | 2007-04-30 | 2007-06-06 | Airbus Uk Ltd | Method and apparatus for deploying an auxiliary airfoil |
CN112478133B (zh) * | 2020-12-02 | 2023-07-21 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种耦合连杆驱动机构及其机翼折叠整流盖板开合结构 |
CN115783242B (zh) * | 2022-12-16 | 2024-12-20 | 江西洪都航空工业集团有限责任公司 | 一种带导流片式双缝襟翼的增升装置 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE672401C (de) * | 1936-06-20 | 1939-03-02 | Joseph Ksoll | Fluegelklappe fuer Flugzeugtragfluegel |
GB517895A (en) * | 1938-08-17 | 1940-02-12 | Fairey Aviat Co Ltd | Improvements in or relating to lifting surfaces of aircraft |
DE2914974C2 (de) * | 1979-04-12 | 1985-09-12 | Dornier Gmbh, 7990 Friedrichshafen | Kombinierte Auftriebs- bzw. Steuerklappe, insbesondere an der Hinterkante von Flugzeugtragflügeln |
US4605187A (en) * | 1984-03-09 | 1986-08-12 | The Boeing Company | Wing flap mechanism |
-
1986
- 1986-12-20 DE DE19863643808 patent/DE3643808A1/de active Granted
-
1987
- 1987-10-13 EP EP19870114933 patent/EP0272396B1/de not_active Expired - Lifetime
- 1987-10-13 ES ES87114933T patent/ES2031102T3/es not_active Expired - Lifetime
- 1987-12-18 BR BR8706925A patent/BR8706925A/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EP0272396A2 (de) | 1988-06-29 |
DE3643808C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1989-03-16 |
EP0272396B1 (de) | 1992-03-04 |
BR8706925A (pt) | 1988-07-26 |
DE3643808A1 (de) | 1988-06-30 |
EP0272396A3 (en) | 1989-12-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
MX173575B (es) | Sistema para accionar un par de rotores de helice | |
NO951788L (no) | Kombinert flymaskin | |
ES2063605R (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | ||
ES2010649A4 (es) | Pala de helice de perfil aerodinamico. | |
DE3766636D1 (de) | Flugzeugfluegel mit spoilern und hinterkantenklappen, die auf dem querruder montiert sind. | |
ES2054133T3 (es) | Aeronave con un par de rotores que giran en sentido contrario. | |
DE60301461D1 (de) | Senkrechtstarter | |
ES2063322T3 (es) | Metodo y sistema para sostener un vehiculo aerotransportado al espacio. | |
ES2117210T3 (es) | Ala de banda flexible montada de forma giratoria. | |
ES2105255T3 (es) | Sistema de deshielo. | |
ES2138171T3 (es) | Freno aerodinamico con abertura ajustable para el plano de sustentacion de una aeronave. | |
SU541426A3 (ru) | Крыло дл летательного аппарата | |
ES2006429A4 (es) | Inductor de trepidacion. | |
ES2037972T3 (es) | Artefacto aereo provisto, como minimo, de un propulsor eyectable. | |
ES2031102T3 (es) | Dispositivo para las trampillas de efecto aerodinamico en las alas sustentadoras de los aviones, sobre todo para los alerones-traseros. | |
IL38692A (en) | Multi-engined propeller driven aircraft including one engine mounted on the tail fin | |
ES8607500A1 (es) | Perfeccionamientos en los diferenciales para vehiculo auto- movil | |
GB1118340A (en) | Mounting means for an aircraft engine | |
ATE86931T1 (de) | Senkrechtstarter. | |
GB536865A (en) | Improvements in or relating to aircraft | |
ES8401203A1 (es) | Perfeccionamientos en las juntas homocineticas destinadas a unir dos arboles. | |
ES8708197A1 (es) | Un aparato para situar aeronaves en posicion, particularmente sobre cubiertas de barcos o plataformas de aterrizaje de instalaciones petroliferas. | |
ES2144586T3 (es) | Aleron de aletas fijas al borde de salida para naves. | |
ES2047579T3 (es) | Lancha rapida con dos alas portadoras. | |
CIJAN | The aerodynamic merging of wings, fuselage and cockpit(Open jet wind tunnel testing of Meteor sailplane, examining aerodynamic merging of wings, fuselage and cockpit) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
Ref document number: 272396 Country of ref document: ES |