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GB2577847B - Modifying the chord length of an aircraft wing - Google Patents

Modifying the chord length of an aircraft wing Download PDF

Info

Publication number
GB2577847B
GB2577847B GB2000527.8A GB202000527A GB2577847B GB 2577847 B GB2577847 B GB 2577847B GB 202000527 A GB202000527 A GB 202000527A GB 2577847 B GB2577847 B GB 2577847B
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.)
Active
Application number
GB2000527.8A
Other versions
GB2577847A (en
GB202000527D0 (en
Inventor
John Lyons Neil
Alderman James
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 claimed from GB1719583.5A external-priority patent/GB2568731B/en
Publication of GB202000527D0 publication Critical patent/GB202000527D0/en
Publication of GB2577847A publication Critical patent/GB2577847A/en
Application granted granted Critical
Publication of GB2577847B publication Critical patent/GB2577847B/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
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • 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
    • B64C9/14—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
    • 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)
  • Transmission Devices (AREA)
GB2000527.8A 2017-11-24 2017-11-24 Modifying the chord length of an aircraft wing Active GB2577847B (en)

Priority Applications (1)

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

Applications Claiming Priority (2)

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
GB2000527.8A GB2577847B (en) 2017-11-24 2017-11-24 Modifying the chord length of an aircraft wing

Publications (3)

Publication Number Publication Date
GB202000527D0 GB202000527D0 (en) 2020-02-26
GB2577847A GB2577847A (en) 2020-04-08
GB2577847B true GB2577847B (en) 2020-12-09

Family

ID=69626799

Family Applications (1)

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

Country Status (1)

Country Link
GB (1) GB2577847B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102022002158B3 (en) 2022-06-15 2023-03-16 Karl-Peter Kämpf Ventilated surface flap

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
GB2577847A (en) 2020-04-08
GB202000527D0 (en) 2020-02-26

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