GB322687A - Aeroplane with supporting surface subdivided by gaps - Google Patents

Aeroplane with supporting surface subdivided by gaps

Info

Publication number
GB322687A
GB322687A GB2463/29A GB246329A GB322687A GB 322687 A GB322687 A GB 322687A GB 2463/29 A GB2463/29 A GB 2463/29A GB 246329 A GB246329 A GB 246329A GB 322687 A GB322687 A GB 322687A
Authority
GB
United Kingdom
Prior art keywords
gaps
supporting surface
aeroplane
subdivided
surface subdivided
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
GB2463/29A
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 GB2463/29A priority Critical patent/GB322687A/en
Publication of GB322687A publication Critical patent/GB322687A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/20—Boundary layer controls by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct
    • 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

Abstract

322,687. Ksoll, J. Jan. 24, 1929. Planes, construction of. - An aeroplane supporting surface is subdivided by gaps d, e meeting at a common point h above the leading edge of a pivoted flap c, the passage then tapering to the outlet i. There may be more than two gaps but all meet at the same point.
GB2463/29A 1929-01-24 1929-01-24 Aeroplane with supporting surface subdivided by gaps Expired GB322687A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2463/29A GB322687A (en) 1929-01-24 1929-01-24 Aeroplane with supporting surface subdivided by gaps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2463/29A GB322687A (en) 1929-01-24 1929-01-24 Aeroplane with supporting surface subdivided by gaps

Publications (1)

Publication Number Publication Date
GB322687A true GB322687A (en) 1929-12-12

Family

ID=9740005

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2463/29A Expired GB322687A (en) 1929-01-24 1929-01-24 Aeroplane with supporting surface subdivided by gaps

Country Status (1)

Country Link
GB (1) GB322687A (en)

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