ES2165044T3 - Ala neumatica adaptable para aeroplanos de alas rigidas. - Google Patents

Ala neumatica adaptable para aeroplanos de alas rigidas.

Info

Publication number
ES2165044T3
ES2165044T3 ES97917986T ES97917986T ES2165044T3 ES 2165044 T3 ES2165044 T3 ES 2165044T3 ES 97917986 T ES97917986 T ES 97917986T ES 97917986 T ES97917986 T ES 97917986T ES 2165044 T3 ES2165044 T3 ES 2165044T3
Authority
ES
Spain
Prior art keywords
wing
double
bands
coating
wrapping
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
Application number
ES97917986T
Other languages
English (en)
Inventor
Andreas Reinhard
Frederick E To
Otto Ramseier
Res Kammer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Prospective Concepts AG
Original Assignee
Prospective Concepts AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Prospective Concepts AG filed Critical Prospective Concepts AG
Application granted granted Critical
Publication of ES2165044T3 publication Critical patent/ES2165044T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/30—Wings comprising inflatable structural components

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Feedback Control In General (AREA)
  • Retarders (AREA)
  • Tents Or Canopies (AREA)
  • Laminated Bodies (AREA)
  • Fluid-Damping Devices (AREA)
  • Treatment Of Fiber Materials (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

EL ALA NEUMATICA REIVINDICADA COMPRENDE UNA ENVOLTURA HERMETICA CONTINUA (8) COMPUESTA DE UN MATERIAL BASE TEXTIL Y SUBDIVIDIDA EN CELDAS (15) A TRAVES DE UNA PLURALIDAD DE BANDAS TEXTILES (3). LA ENVOLTURA (8) FORMA UN REVESTIMIENTO SUPERIOR (1) Y UN REVESTIMIENTO INFERIOR (2) TALES QUE EL REVESTIMIENTO SUPERIOR (1) SE PUEDA COMPLETAR EN PARTE (HACIA EL BORDE DE TIRO DESCENDENTE (5)), Y EL REVESTIMIENTO INFERIOR (2) POR COMPLETO O EN PARTE, POR UN REVESTIMIENTO DOBLE SUPERIOR Y UNO INFERIOR (16, 17). LOS REVESTIMIENTOS DOBLES (16, 17) QUEDAN CONECTADOS A LA ENVOLTURA (8) ENTRE LAS LINEAS DE ACOPLAMIENTO DE LAS BANDAS (3) FORMANDO ASI ENTRE LA ENVOLTURA (8) Y LOS REVESTIMIENTOS DOBLES (16,1 7) UNOS CANALES (19) EN LOS QUE PUEDE ENTRAR AIRE COMPRIMIDO. ESTO CAMBIA LA FORMA DEL PERFIL DEL ALA. ADEMAS, LAS BANDAS (3) PUEDEN TENER EN PARTE UN DISEÑO HERMETICO Y DE DOBLE PARED PARECIDO, CREANDO TAMBIEN EN ESTE CASO UNOS CANALES (19) EN LOS QUE PUEDE ENTRAR AIRE COMPRIMIDO. ESTO REDUCE LA ALTURADEL PERFIL DEL ALA. MEDIANTE UNA COMBINACION ADECUADA DE ESTAS OPCIONES, PARTE DEL ALA SE PUEDE DISEÑAR A MODO DE ALERON O DE ALETA DE ATERRIZAJE, O SE PUEDE OPTIMIZAR EL ALA EN SU CONJUNTO RESPECTO A LA VELOCIDAD DE VUELO SELECCIONADA.
ES97917986T 1996-07-18 1997-05-14 Ala neumatica adaptable para aeroplanos de alas rigidas. Expired - Lifetime ES2165044T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH179996 1996-07-18

Publications (1)

Publication Number Publication Date
ES2165044T3 true ES2165044T3 (es) 2002-03-01

Family

ID=4218879

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97917986T Expired - Lifetime ES2165044T3 (es) 1996-07-18 1997-05-14 Ala neumatica adaptable para aeroplanos de alas rigidas.

Country Status (17)

Country Link
US (1) US6199796B1 (es)
EP (1) EP0851829B1 (es)
JP (1) JPH11512998A (es)
CN (1) CN1080225C (es)
AT (1) ATE210042T1 (es)
AU (1) AU712971B2 (es)
BR (1) BR9702347A (es)
CA (1) CA2232321C (es)
CZ (1) CZ295332B6 (es)
DE (1) DE59705660D1 (es)
ES (1) ES2165044T3 (es)
HU (1) HU222475B1 (es)
IL (1) IL123329A (es)
MX (1) MX9801856A (es)
NZ (1) NZ329761A (es)
PL (1) PL183614B1 (es)
WO (1) WO1998003398A1 (es)

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CH700461A2 (de) * 2009-02-17 2010-08-31 Empa Gekrümmter pneumatischer Träger.
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US9308979B2 (en) 2012-03-06 2016-04-12 Stanislav Mostoviy Reversible camber soft wing sail
CN102642611B (zh) * 2012-04-24 2014-10-01 哈尔滨工业大学 一种基于气动肌肉的主动变形蒙皮结构
CN102700705B (zh) * 2012-06-29 2014-01-22 哈尔滨工业大学 一种用于控制充气结构构型混编预张力索网的方法
US10132290B2 (en) * 2012-06-29 2018-11-20 General Electric Company Apparatus and method for aerodynamic performance enhancement of a wind turbine
DE102012017823B4 (de) * 2012-09-08 2014-09-18 Faurecia Autositze Gmbh Verstellvorrichtung für Kraftfahrzeugsitze
CN102923298B (zh) * 2012-11-22 2016-01-20 哈尔滨工业大学 一种落丝阵式可充气展开机翼
EP2769911A3 (de) * 2013-02-22 2017-08-16 Herbert Kotschnig Zerlegbarer Flügelholm für insbesondere ebenfalls zerlegbare Tragflächen oder flügelähnliche aerodynamische Gegenstände
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CN104354875B (zh) * 2014-10-31 2016-08-24 中国航天空气动力技术研究院 一种考虑运动轨迹的增升装置优化设计方法
US9714057B2 (en) 2015-05-08 2017-07-25 Paccar Inc Pneumatically actuated air control devices and methods
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ES2633608B1 (es) * 2016-03-21 2018-07-13 Fco. Javier Porras Vila Alas con arcos, y, tubos en la superficie inferior
CN106081099B (zh) * 2016-08-30 2019-05-03 苏跃进 竖直升降的多旋翼飞机和水平升降的固定翼飞机
CN106892087B (zh) * 2017-03-17 2020-07-03 哈尔滨工业大学 一种充气式滑翔翼无人机
CN106945832B (zh) * 2017-03-17 2020-07-03 哈尔滨工业大学 一种充气式滑翔翼无人机
CN106864727B (zh) * 2017-03-17 2020-07-03 哈尔滨工业大学 一种充气式滑翔翼无人机
CN106864728B (zh) * 2017-03-17 2020-07-03 哈尔滨工业大学 一种充气式滑翔翼无人机
EP3466811B1 (en) * 2017-10-09 2023-06-21 Airbus Operations GmbH Vertical tail unit for flow control
ES2927476T3 (es) * 2017-10-09 2022-11-07 Airbus Operations Gmbh Unidad de cola vertical para control de flujo
CN108557077B (zh) * 2018-01-25 2020-12-11 中航联创科技有限公司 一种具有柔性蜷缩式机翼的无人机
CN109552597A (zh) * 2018-11-15 2019-04-02 北京遥感设备研究所 一种充气机翼及制备方法
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Also Published As

Publication number Publication date
PL183614B1 (pl) 2002-06-28
WO1998003398A1 (de) 1998-01-29
AU712971B2 (en) 1999-11-18
ATE210042T1 (de) 2001-12-15
HUP9901554A2 (hu) 1999-08-30
JPH11512998A (ja) 1999-11-09
CA2232321A1 (en) 1998-01-29
MX9801856A (es) 1998-11-29
CN1198137A (zh) 1998-11-04
IL123329A0 (en) 1998-09-24
EP0851829A1 (de) 1998-07-08
HU222475B1 (hu) 2003-07-28
CA2232321C (en) 2004-11-30
NZ329761A (en) 1999-01-28
AU2630997A (en) 1998-02-10
CZ295332B6 (cs) 2005-07-13
BR9702347A (pt) 1999-12-28
IL123329A (en) 2000-10-31
HUP9901554A3 (en) 2000-04-28
EP0851829B1 (de) 2001-12-05
CZ81598A3 (cs) 1998-11-11
US6199796B1 (en) 2001-03-13
CN1080225C (zh) 2002-03-06
DE59705660D1 (de) 2002-01-17
PL326030A1 (en) 1998-08-17

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