GB191303746A - Improvements in Hydro-aeroplane Floats. - Google Patents

Improvements in Hydro-aeroplane Floats.

Info

Publication number
GB191303746A
GB191303746A GB191303746DA GB191303746A GB 191303746 A GB191303746 A GB 191303746A GB 191303746D A GB191303746D A GB 191303746DA GB 191303746 A GB191303746 A GB 191303746A
Authority
GB
United Kingdom
Prior art keywords
floats
struts
line
aeroplane
hydro
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
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.)
J Samuel White and Co Ltd
Original Assignee
J Samuel White and 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 J Samuel White and Co Ltd filed Critical J Samuel White and Co Ltd
Application granted granted Critical
Publication of GB191303746A publication Critical patent/GB191303746A/en
Expired legal-status Critical Current

Links

Classifications

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Earth Drilling (AREA)

Abstract

3746. White & Co., J. S., and Smith, J. Feb. 13. Floats for aerial machines. - Floats for hydro - aeroplanes are approximately boatshaped with considerable overhang forward in elevation a n d of stream - line shape in plan, and are constructed with a turtle-back deck 5. The bottom 6 is curved in cross-section and provided with steps 7 situated directly beneath the struts 22 by which the aeroplane is supported. A longitudinal bulkhead 9 the whole depth of the float is fitted, and in addition transverse shallow floors 10. Diagonal struts 19 are placed transversely between the longitudinal bulkhead and the outer ends of the floors. The transverse bulkheads 8 are fitted in line with the steps 7, and upright struts are secured to the central bulkheads. A keelson and middle-line deck stringer constitute features of the construction.
GB191303746D 1913-02-13 1913-02-13 Improvements in Hydro-aeroplane Floats. Expired GB191303746A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191303746T 1913-02-13

Publications (1)

Publication Number Publication Date
GB191303746A true GB191303746A (en) 1914-02-12

Family

ID=34358857

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191303746D Expired GB191303746A (en) 1913-02-13 1913-02-13 Improvements in Hydro-aeroplane Floats.

Country Status (1)

Country Link
GB (1) GB191303746A (en)

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