GB201906062D0 - Aircraft wing with a moveable wing tip for load alleviation - Google Patents

Aircraft wing with a moveable wing tip for load alleviation

Info

Publication number
GB201906062D0
GB201906062D0 GBGB1906062.3A GB201906062A GB201906062D0 GB 201906062 D0 GB201906062 D0 GB 201906062D0 GB 201906062 A GB201906062 A GB 201906062A GB 201906062 D0 GB201906062 D0 GB 201906062D0
Authority
GB
United Kingdom
Prior art keywords
wing
moveable
load alleviation
aircraft
tip
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.)
Withdrawn
Application number
GBGB1906062.3A
Other versions
GB2583499A (en
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 Ltd
Original Assignee
Airbus Operations Ltd
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 Ltd filed Critical Airbus Operations Ltd
Priority to GB1906062.3A priority Critical patent/GB2583499A/en
Publication of GB201906062D0 publication Critical patent/GB201906062D0/en
Publication of GB2583499A publication Critical patent/GB2583499A/en
Withdrawn legal-status Critical Current

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
    • B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • 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
    • 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)
  • Automation & Control Theory (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
GB1906062.3A 2019-04-30 2019-04-30 Aircraft wing with a moveable wing tip for load alleviation Withdrawn GB2583499A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1906062.3A GB2583499A (en) 2019-04-30 2019-04-30 Aircraft wing with a moveable wing tip for load alleviation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1906062.3A GB2583499A (en) 2019-04-30 2019-04-30 Aircraft wing with a moveable wing tip for load alleviation

Publications (2)

Publication Number Publication Date
GB201906062D0 true GB201906062D0 (en) 2019-06-12
GB2583499A GB2583499A (en) 2020-11-04

Family

ID=66809072

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1906062.3A Withdrawn GB2583499A (en) 2019-04-30 2019-04-30 Aircraft wing with a moveable wing tip for load alleviation

Country Status (1)

Country Link
GB (1) GB2583499A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111422375A (en) * 2020-04-15 2020-07-17 中国飞机强度研究所 Active control method and system for load of vertical constraint point of airplane

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2621982A (en) * 2022-08-24 2024-03-06 Airbus Operations Ltd Aircraft attitude controller and wing system

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB299212A (en) * 1927-12-01 1928-10-25 Hans Hocke Improvements in aeroplanes with stabilisation surfaces
US6227487B1 (en) * 1999-05-05 2001-05-08 Northrop Grumman Corporation Augmented wing tip drag flap
US6547181B1 (en) * 2002-05-29 2003-04-15 The Boeing Company Ground effect wing having a variable sweep winglet
FR3037560B1 (en) * 2015-06-16 2018-06-01 Airbus Operations AIRCRAFT WING INCLUDING A PILOTABLE WING FIT IN INCIDENCE
GB2569535A (en) * 2017-12-18 2019-06-26 Airbus Sas Passively actuated fluid foil

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111422375A (en) * 2020-04-15 2020-07-17 中国飞机强度研究所 Active control method and system for load of vertical constraint point of airplane

Also Published As

Publication number Publication date
GB2583499A (en) 2020-11-04

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)