GB191310801A - Improvements in Floats for Hydro-aeroplanes. - Google Patents

Improvements in Floats for Hydro-aeroplanes.

Info

Publication number
GB191310801A
GB191310801A GB191310801DA GB191310801A GB 191310801 A GB191310801 A GB 191310801A GB 191310801D A GB191310801D A GB 191310801DA GB 191310801 A GB191310801 A GB 191310801A
Authority
GB
United Kingdom
Prior art keywords
floats
aeroplanes
hydro
horizontal
members
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
Inventor
Oscar Theodor Gnosspelius
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
Application granted granted Critical
Publication of GB191310801A publication Critical patent/GB191310801A/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)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Earth Drilling (AREA)

Abstract

10,801. Gnosspelius, O. T. May 7. Floats for aerial machines.-Floats for hydroaeroplanes are constructed with a bottom surface comprising a number of hydroplane surfaces, the forward one A being inclined to the vertical at a smaller angle than the remainder of the hydroplane members B, C. These members B, G are inclined in a rearward direction, first at a small angle above the horizontal and then, after curving down, at a small angle below the horizontal.
GB191310801D 1913-05-07 1913-05-07 Improvements in Floats for Hydro-aeroplanes. Expired GB191310801A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191310801T 1913-05-07

Publications (1)

Publication Number Publication Date
GB191310801A true GB191310801A (en) 1914-02-12

Family

ID=32370479

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191310801D Expired GB191310801A (en) 1913-05-07 1913-05-07 Improvements in Floats for Hydro-aeroplanes.

Country Status (1)

Country Link
GB (1) GB191310801A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5588389A (en) * 1995-03-30 1996-12-31 Carter, Jr.; Jay Dual lift boat hull
EP2903886A4 (en) * 2012-10-08 2016-10-19 K2 Keller Consulting Llc Watercraft hull with improved lift, planing speed range, and near maximum efficiency
US10647385B2 (en) 2017-08-29 2020-05-12 John H. Keller Advances in watercraft hull lift, efficiency, and reduced hump drag with increased stability

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5588389A (en) * 1995-03-30 1996-12-31 Carter, Jr.; Jay Dual lift boat hull
EP2903886A4 (en) * 2012-10-08 2016-10-19 K2 Keller Consulting Llc Watercraft hull with improved lift, planing speed range, and near maximum efficiency
US10647385B2 (en) 2017-08-29 2020-05-12 John H. Keller Advances in watercraft hull lift, efficiency, and reduced hump drag with increased stability

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