GB201704787D0 - Foldable aerodynamic structure with slewing bearing - Google Patents

Foldable aerodynamic structure with slewing bearing

Info

Publication number
GB201704787D0
GB201704787D0 GBGB1704787.9A GB201704787A GB201704787D0 GB 201704787 D0 GB201704787 D0 GB 201704787D0 GB 201704787 A GB201704787 A GB 201704787A GB 201704787 D0 GB201704787 D0 GB 201704787D0
Authority
GB
United Kingdom
Prior art keywords
slewing bearing
aerodynamic structure
foldable aerodynamic
foldable
slewing
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Withdrawn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
GBGB1704787.9A
Other versions
GB2560900A (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 GB1704787.9A priority Critical patent/GB2560900A/en
Publication of GB201704787D0 publication Critical patent/GB201704787D0/en
Publication of GB2560900A publication Critical patent/GB2560900A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069Influencing 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
    • B64C23/072Influencing 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/40Varying angle of sweep
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/56Folding or collapsing to reduce overall dimensions of aircraft
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Rolling Contact Bearings (AREA)
GB1704787.9A 2017-03-27 2017-03-27 Foldable aerodynamic structure with slewing bearing Withdrawn GB2560900A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1704787.9A GB2560900A (en) 2017-03-27 2017-03-27 Foldable aerodynamic structure with slewing bearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1704787.9A GB2560900A (en) 2017-03-27 2017-03-27 Foldable aerodynamic structure with slewing bearing

Publications (2)

Publication Number Publication Date
GB201704787D0 true GB201704787D0 (en) 2017-05-10
GB2560900A GB2560900A (en) 2018-10-03

Family

ID=58687809

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1704787.9A Withdrawn GB2560900A (en) 2017-03-27 2017-03-27 Foldable aerodynamic structure with slewing bearing

Country Status (1)

Country Link
GB (1) GB2560900A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11254412B2 (en) 2019-03-29 2022-02-22 The Boeing Company Foldable raked wing tips having aerodynamic devices

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3279721A (en) * 1964-10-30 1966-10-18 Boeing Co Bearing arrangement for variable sweep wing aircraft
DE1481541C3 (en) * 1966-12-22 1975-09-04 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Bearing for an aircraft wing that can be pivoted about a vertical axis
FR1531596A (en) * 1967-05-23 1968-07-05 Dassault Avions Connection device between the fuselage and the movable wings of a variable-geometry airplane
FR1569233A (en) * 1967-07-05 1969-05-30
DE1935920A1 (en) * 1969-07-15 1971-05-27 Messerschmitt Boelkow Blohm Storage facility
US8708286B2 (en) * 2012-06-21 2014-04-29 The Boeing Company Swing tip assembly rotation joint
US9296471B2 (en) * 2013-10-06 2016-03-29 The Boeing Company Swing wing tip system, assembly and method with dual load path structure
GB2539497A (en) * 2015-06-19 2016-12-21 Airbus Operations Ltd A Rotational Joint For An Aircraft Folding Wing
US9856910B2 (en) * 2015-11-30 2018-01-02 Roller Bearing Company Of America, Inc. Self-lubricated thrust bearing for a hinged aircraft wing

Also Published As

Publication number Publication date
GB2560900A (en) 2018-10-03

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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)