ES2193064T3 - Alas de aviongs - Google Patents

Alas de aviongs

Info

Publication number
ES2193064T3
ES2193064T3 ES00922317T ES00922317T ES2193064T3 ES 2193064 T3 ES2193064 T3 ES 2193064T3 ES 00922317 T ES00922317 T ES 00922317T ES 00922317 T ES00922317 T ES 00922317T ES 2193064 T3 ES2193064 T3 ES 2193064T3
Authority
ES
Spain
Prior art keywords
wings
wing
effective position
parts
angle
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
ES00922317T
Other languages
English (en)
Inventor
Anton Gerald Ofner
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of ES2193064T3 publication Critical patent/ES2193064T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/20—Rigid airships; Semi-rigid airships provided with wings or stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/48—Varying camber by relatively-movable parts of wing structures
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Radio Relay Systems (AREA)
  • Feedback Control In General (AREA)
  • Tires In General (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

Alas de avión (1), en particular alas (1) con una sección transversal y un ángulo de ataque adecuado para el vuelo rápido, en donde a las alas (1) están asignadas partes del ala (20, 21) que influyen en su fuerza ascensional, las cuales se pueden desplazar desde una posición recogida aerodinámicamente inefectiva a una posición aerodinámicamente efectiva, y desde la posición efectiva de vuelta a la posición recogida, caracterizadas porque partes del ala (20, 21) están dispuestas en su posición efectiva en la cara superior (3) y/o en la cara inferior (4) de las alas (1), porque por lo menos una de las partes del ala (20, 21) en la cara superior y/o en la cara inferior de las alas (1) se extiende en su posición efectiva por lo menos a lo largo de la mayor parte de la anchura del ala (1) entre su canto anterior (24) y su canto posterior (23), y porque partes del ala (20) dispuestas en su posición efectiva aumentan la fuerza ascensional de las alas (1) y modifican el ángulo de ataque (2) de lasalas (1), en particular aumentándolo.
ES00922317T 1999-05-04 2000-05-02 Alas de aviongs Expired - Lifetime ES2193064T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT0079399A AT408216B (de) 1999-05-04 1999-05-04 Flugzeugtragflügel

Publications (1)

Publication Number Publication Date
ES2193064T3 true ES2193064T3 (es) 2003-11-01

Family

ID=3499904

Family Applications (1)

Application Number Title Priority Date Filing Date
ES00922317T Expired - Lifetime ES2193064T3 (es) 1999-05-04 2000-05-02 Alas de aviongs

Country Status (7)

Country Link
US (1) US6910662B1 (es)
EP (1) EP1175334B1 (es)
AT (2) AT408216B (es)
DE (1) DE50001799D1 (es)
ES (1) ES2193064T3 (es)
RU (1) RU2222472C2 (es)
WO (1) WO2000066427A1 (es)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NZ511661A (en) * 2001-05-11 2003-09-26 Graham Bond Grove An improved aerofoil
US8439314B1 (en) * 2006-11-06 2013-05-14 Sanjay Dhall Aircraft having offset telescopic wings
WO2009066322A1 (en) * 2007-11-22 2009-05-28 Lappasi Sundararajan Vidhyasag Airfoil structure for wing vortex reduction
WO2010032241A1 (en) * 2008-09-17 2010-03-25 Israel Aerospace Industries Ltd. Aerofoil accessories and method for modyfying the geometry of a wing element

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1559090A (en) * 1923-11-03 1925-10-27 Theodore P Hall Airplane
US1775886A (en) * 1925-01-24 1930-09-16 Carpenter Rupert Evan Howard Electron-discharge device
US1924871A (en) * 1931-06-26 1933-08-29 Ludington Charles Townsend Boat keel
FR781467A (fr) * 1933-08-01 1935-05-16 Aile d'avion à profil variable
US2969207A (en) * 1958-10-16 1961-01-24 Doyle F Fain Variable camber airfoil
US3136501A (en) * 1961-10-23 1964-06-09 Ernest H Barber Aircraft wing construction
US3184187A (en) * 1963-05-10 1965-05-18 Isaac Peter Retractable airfoils and hydrofoils
US3447768A (en) * 1967-02-08 1969-06-03 Whittaker Corp Lifting body external fuel stores
GB1296994A (es) 1969-06-02 1972-11-22
FR2049028A1 (es) 1969-06-09 1971-03-26 Ansaldi Alexandre
US4341176A (en) * 1980-09-29 1982-07-27 Orrison William W Air foil with reversible camber
US4485991A (en) * 1983-07-01 1984-12-04 Fuller Brian L Rollable airfoil
US4890803A (en) * 1987-07-29 1990-01-02 Smith Larry L Airfoil with fixed and variable upper camber portions
NO921248L (no) 1992-03-31 1993-10-01 Tore Lyngholm Anordning ved foil
US6138957A (en) * 1998-12-23 2000-10-31 Northrop Grumman Corporation Swept-back wings with airflow channeling

Also Published As

Publication number Publication date
EP1175334A1 (de) 2002-01-30
ATE237496T1 (de) 2003-05-15
DE50001799D1 (de) 2003-05-22
ATA79399A (de) 2001-02-15
RU2222472C2 (ru) 2004-01-27
WO2000066427A1 (de) 2000-11-09
AT408216B (de) 2001-09-25
EP1175334B1 (de) 2003-04-16
US6910662B1 (en) 2005-06-28

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