GB130041A - Improvements in or relating to the Tail Surfaces of Hydro-aeroplane Flying Machines. - Google Patents

Improvements in or relating to the Tail Surfaces of Hydro-aeroplane Flying Machines.

Info

Publication number
GB130041A
GB130041A GB12318A GB12318A GB130041A GB 130041 A GB130041 A GB 130041A GB 12318 A GB12318 A GB 12318A GB 12318 A GB12318 A GB 12318A GB 130041 A GB130041 A GB 130041A
Authority
GB
United Kingdom
Prior art keywords
hydro
slip
stream
tail
relating
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
GB12318A
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.)
HARRIS BOOTH
Blackburn Aeroplane and Motor Co Ltd
Original Assignee
HARRIS BOOTH
Blackburn Aeroplane and Motor Co 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 HARRIS BOOTH, Blackburn Aeroplane and Motor Co Ltd filed Critical HARRIS BOOTH
Priority to GB12318A priority Critical patent/GB130041A/en
Publication of GB130041A publication Critical patent/GB130041A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes
    • B64C35/007—Specific control surfaces therefor

Abstract

130,041. Blackburn Aeroplane & Motor Co., and Booth, H. Jan. 2, 1918. Planes, arrangement of; steering and balancing. -Hydro-aeroplanes, and especially single-engined flying-boats, are provided with two tail-fins 4, 5 arranged at opposite angles to the vertical and so as to form chords to the slip-stream circle 3, in order to reduce yawing due to the spin of the slip-stream, and to obtain a powerful air-rudder control when on water, the rudders 8 being hinged to the rear edges of the tail-fins. The upper tailplane 6 and elevator 9 are shown within the slipstream, and the lower plane 7 and elevator 10 below the slip-stream.
GB12318A 1918-01-02 1918-01-02 Improvements in or relating to the Tail Surfaces of Hydro-aeroplane Flying Machines. Expired GB130041A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB12318A GB130041A (en) 1918-01-02 1918-01-02 Improvements in or relating to the Tail Surfaces of Hydro-aeroplane Flying Machines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB12318A GB130041A (en) 1918-01-02 1918-01-02 Improvements in or relating to the Tail Surfaces of Hydro-aeroplane Flying Machines.

Publications (1)

Publication Number Publication Date
GB130041A true GB130041A (en) 1919-07-31

Family

ID=32340095

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12318A Expired GB130041A (en) 1918-01-02 1918-01-02 Improvements in or relating to the Tail Surfaces of Hydro-aeroplane Flying Machines.

Country Status (1)

Country Link
GB (1) GB130041A (en)

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