GB201719583D0 - Modifying the chord length of an aircraft wing - Google Patents

Modifying the chord length of an aircraft wing

Info

Publication number
GB201719583D0
GB201719583D0 GBGB1719583.5A GB201719583A GB201719583D0 GB 201719583 D0 GB201719583 D0 GB 201719583D0 GB 201719583 A GB201719583 A GB 201719583A GB 201719583 D0 GB201719583 D0 GB 201719583D0
Authority
GB
United Kingdom
Prior art keywords
modifying
chord length
aircraft wing
wing
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.)
Granted
Application number
GBGB1719583.5A
Other versions
GB2568731A (en
GB2568731B (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 GB2000527.8A priority Critical patent/GB2577847B/en
Priority to GB1719583.5A priority patent/GB2568731B/en
Publication of GB201719583D0 publication Critical patent/GB201719583D0/en
Publication of GB2568731A publication Critical patent/GB2568731A/en
Application granted granted Critical
Publication of GB2568731B publication Critical patent/GB2568731B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/54—Varying in area
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/06—Adjustable control surfaces or members, e.g. rudders with two or more independent movements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/08—Adjustable control surfaces or members, e.g. rudders bodily displaceable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • 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
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Tires In General (AREA)
GB1719583.5A 2017-11-24 2017-11-24 Modifying the chord length of an aircraft wing Active GB2568731B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB2000527.8A GB2577847B (en) 2017-11-24 2017-11-24 Modifying the chord length of an aircraft wing
GB1719583.5A GB2568731B (en) 2017-11-24 2017-11-24 Modifying the chord length of an aircraft wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1719583.5A GB2568731B (en) 2017-11-24 2017-11-24 Modifying the chord length of an aircraft wing

Publications (3)

Publication Number Publication Date
GB201719583D0 true GB201719583D0 (en) 2018-01-10
GB2568731A GB2568731A (en) 2019-05-29
GB2568731B GB2568731B (en) 2020-04-08

Family

ID=60950585

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1719583.5A Active GB2568731B (en) 2017-11-24 2017-11-24 Modifying the chord length of an aircraft wing

Country Status (1)

Country Link
GB (1) GB2568731B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021083822A1 (en) * 2019-11-01 2021-05-06 Airbus Operations Limited Aircraft wing with trailing edge flight control surface
GB2588680A (en) * 2019-11-01 2021-05-05 Airbus Operations Ltd Control unit and system for a variable geometry aircraft
GB2588766A (en) * 2019-11-01 2021-05-12 Airbus Operations Ltd An aircraft wing with trailing edge flight control surface

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB489853A (en) * 1937-02-03 1938-08-03 Frederick George Miles Improvements relating to aerofoils
KR20090095928A (en) * 2008-03-06 2009-09-10 윙쉽테크놀러지 주식회사 Lift enhancer for a WIG craft
EP2746151B1 (en) * 2012-12-19 2017-04-12 Airbus Operations GmbH Flap system for an aircraft, method for adjusting the lift of an aircraft and aircraft comprising a main wing and at least one flap system
FR3011226B1 (en) * 2013-09-30 2017-05-19 Airbus Operations Sas HYPERSUSTENTER LEAK DEPENDENT SHUTTER SYSTEM FOR AN AIRCRAFT SAIL.

Also Published As

Publication number Publication date
GB2568731A (en) 2019-05-29
GB2568731B (en) 2020-04-08

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