FR3037560B1 - Aile d'aeronef comprenant un embout d'aile pilotable en incidence - Google Patents

Aile d'aeronef comprenant un embout d'aile pilotable en incidence Download PDF

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Publication number
FR3037560B1
FR3037560B1 FR1555494A FR1555494A FR3037560B1 FR 3037560 B1 FR3037560 B1 FR 3037560B1 FR 1555494 A FR1555494 A FR 1555494A FR 1555494 A FR1555494 A FR 1555494A FR 3037560 B1 FR3037560 B1 FR 3037560B1
Authority
FR
France
Prior art keywords
wing
pilotable
incidence
fit
aircraft
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.)
Active
Application number
FR1555494A
Other languages
English (en)
Other versions
FR3037560A1 (fr
Inventor
Olivier Cazals
Thierry Druot
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1555494A priority Critical patent/FR3037560B1/fr
Priority to US15/182,709 priority patent/US10329010B2/en
Publication of FR3037560A1 publication Critical patent/FR3037560A1/fr
Application granted granted Critical
Publication of FR3037560B1 publication Critical patent/FR3037560B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
    • B64C23/072—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips the wing tip airfoil devices being moveable in their entirety
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/385—Variable incidence wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/42—Adjusting about chordwise axes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1555494A 2015-06-16 2015-06-16 Aile d'aeronef comprenant un embout d'aile pilotable en incidence Active FR3037560B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1555494A FR3037560B1 (fr) 2015-06-16 2015-06-16 Aile d'aeronef comprenant un embout d'aile pilotable en incidence
US15/182,709 US10329010B2 (en) 2015-06-16 2016-06-15 Aircraft wing comprising a controllable-attack wing tip

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1555494A FR3037560B1 (fr) 2015-06-16 2015-06-16 Aile d'aeronef comprenant un embout d'aile pilotable en incidence
FR1555494 2015-06-16

Publications (2)

Publication Number Publication Date
FR3037560A1 FR3037560A1 (fr) 2016-12-23
FR3037560B1 true FR3037560B1 (fr) 2018-06-01

Family

ID=54291423

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1555494A Active FR3037560B1 (fr) 2015-06-16 2015-06-16 Aile d'aeronef comprenant un embout d'aile pilotable en incidence

Country Status (2)

Country Link
US (1) US10329010B2 (fr)
FR (1) FR3037560B1 (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10287000B2 (en) * 2014-07-25 2019-05-14 Hyalta Aeronautics, Inc. Hybrid lighter-than-air vehicle
EP3301016B1 (fr) * 2016-07-06 2020-12-23 Airbus Operations GmbH Aéronef équipé d'un élément de type aile de réduction de charge
US10589801B2 (en) * 2017-04-27 2020-03-17 Paccar Inc Vehicle propulsive aerodynamic elements
US10507901B2 (en) * 2017-06-07 2019-12-17 The Boeing Company Protecting and ensuring readiness of a vehicle
GB2569535A (en) * 2017-12-18 2019-06-26 Airbus Sas Passively actuated fluid foil
RU2674900C1 (ru) * 2017-12-18 2018-12-13 Публичное акционерное общество (ПАО) "Туполев" Консоль крыла летательного аппарата с устройством для управления по курсу
FR3079209A1 (fr) * 2018-03-22 2019-09-27 Francois Geli Avion gros porteur bi-reacteur a voilure non-planaire a geometrie variable
GB2581136A (en) * 2019-01-30 2020-08-12 Airbus Operations Ltd Hinge fairing
GB2580930A (en) * 2019-01-30 2020-08-05 Airbus Operations Ltd Fairing for folding wing tip
GB2583499A (en) * 2019-04-30 2020-11-04 Airbus Operations Ltd Aircraft wing with a moveable wing tip for load alleviation
CN112829922B (zh) * 2021-02-08 2022-01-07 北京北航天宇长鹰无人机科技有限公司 无人机
CN114802710A (zh) * 2022-04-21 2022-07-29 中国航空工业集团公司沈阳飞机设计研究所 一种飞机v尾结构
GB2628523A (en) * 2022-11-16 2024-10-02 Airbus Operations Ltd Aircraft wing
CN117906897B (zh) * 2024-03-18 2024-06-11 西安羚控电子科技有限公司 一种机翼折叠驱动装置的模拟风载控制方法及系统

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2186558A (en) * 1937-05-24 1940-01-09 Rouanet Roger Leger Ma Fernand Aircraft
DE2756107C2 (de) * 1977-12-16 1980-02-28 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Hochwirksames Seitenleitwerk mit variabler Flügelgeometrie
US4542866A (en) * 1983-09-30 1985-09-24 The Boeing Company Aircraft with directional controlling canards
US5156358A (en) * 1991-04-11 1992-10-20 Northrop Corporation Aircraft outboard control
US6547181B1 (en) * 2002-05-29 2003-04-15 The Boeing Company Ground effect wing having a variable sweep winglet
DE10313290B4 (de) * 2003-03-25 2005-12-29 Johannes Schweiger Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche oder Ruderfläche eines Fluggeräts
US6886778B2 (en) * 2003-06-30 2005-05-03 The Boeing Company Efficient wing tip devices and methods for incorporating such devices into existing wing designs
GB0326228D0 (en) * 2003-11-10 2003-12-17 Airbus Uk Ltd Wing tip device
DE102005028688A1 (de) * 2005-05-19 2006-11-30 Airbus Deutschland Gmbh Konzept eines variablen Winglets zur lateralen Lastenreduktion zur kombinierten lateralen und vertikalen Lastenreduktion und zur Performanceverbesserung von Fortbewegungsmitteln

Also Published As

Publication number Publication date
US10329010B2 (en) 2019-06-25
FR3037560A1 (fr) 2016-12-23
US20160368594A1 (en) 2016-12-22

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