GB518670A - Improvements relating to aircraft wing systems - Google Patents

Improvements relating to aircraft wing systems

Info

Publication number
GB518670A
GB518670A GB22825/38A GB2282538A GB518670A GB 518670 A GB518670 A GB 518670A GB 22825/38 A GB22825/38 A GB 22825/38A GB 2282538 A GB2282538 A GB 2282538A GB 518670 A GB518670 A GB 518670A
Authority
GB
United Kingdom
Prior art keywords
wing
leading
pivoted
trailing
disposed
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.)
Expired
Application number
GB22825/38A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB22825/38A priority Critical patent/GB518670A/en
Publication of GB518670A publication Critical patent/GB518670A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B64C9/146—Adjustable control surfaces or members, e.g. rudders forming slots at an other wing location than the rear or the front
    • 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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • 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
    • B64C9/28—Adjustable control surfaces or members, e.g. rudders forming slots by flaps at both the front and rear of the wing operating in unison
    • 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)
  • Toys (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

518,670. Controlling aircraft. STONE, T. H. Aug. 2, 1938, No. 22825. [Class 4] An auxiliary surface or surfaces adapted to be nested on either or both upper and lower surfaces of an aircraft wing is carried by arms pivoted to the wing about an axis disposed nearer to the leading or trailing edge of the wing according to whether the trailing or leading edge of the surface is disposed adjacent the trailing or leading edge of the wing. In one form, the arms 21 are pivoted to brackets carried by the front spar 11 of the wing and a hydraulic jack is pivotally mounted on the rear spar 12 and comprises relatively telescopic cylinders 24A, 24B, 24C and a piston rod 24D pivoted to the surface 17. Either or both ailerons or wing flaps may be disposed rearwardly of the surface. In a modification, an additional auxiliary surface is nested normally against the upper leading surface of the wing. In this case the flaps are separately actuated by jacks disposed horizontally in the wing. In.a further modification, an auxiliary surface on the upper leading surface of the wing is connected through link and lever mechanism with the lower auxiliary surface which is actuated in a manner similar to that shown in Fig. 2.
GB22825/38A 1938-08-02 1938-08-02 Improvements relating to aircraft wing systems Expired GB518670A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB22825/38A GB518670A (en) 1938-08-02 1938-08-02 Improvements relating to aircraft wing systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB22825/38A GB518670A (en) 1938-08-02 1938-08-02 Improvements relating to aircraft wing systems

Publications (1)

Publication Number Publication Date
GB518670A true GB518670A (en) 1940-03-05

Family

ID=10185647

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22825/38A Expired GB518670A (en) 1938-08-02 1938-08-02 Improvements relating to aircraft wing systems

Country Status (1)

Country Link
GB (1) GB518670A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2538224A (en) * 1945-11-13 1951-01-16 Daniel R Zuck Wing with interconnected flap and nose slat
US2557829A (en) * 1947-11-07 1951-06-19 Thomas B Lavelle Aircraft control means
CN113226921A (en) * 2018-12-28 2021-08-06 列奥纳多股份公司 Aircraft wing

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2538224A (en) * 1945-11-13 1951-01-16 Daniel R Zuck Wing with interconnected flap and nose slat
US2557829A (en) * 1947-11-07 1951-06-19 Thomas B Lavelle Aircraft control means
CN113226921A (en) * 2018-12-28 2021-08-06 列奥纳多股份公司 Aircraft wing
CN113226921B (en) * 2018-12-28 2024-01-23 列奥纳多股份公司 Aircraft wing

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