GB265987A - Improvements in seaplanes - Google Patents
Improvements in seaplanesInfo
- Publication number
- GB265987A GB265987A GB3896/27A GB389627A GB265987A GB 265987 A GB265987 A GB 265987A GB 3896/27 A GB3896/27 A GB 3896/27A GB 389627 A GB389627 A GB 389627A GB 265987 A GB265987 A GB 265987A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- float
- rohrbach
- supporting plane
- floats
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/001—Flying-boats; Seaplanes with means for increasing stability on the water
- B64C35/003—Flying-boats; Seaplanes with means for increasing stability on the water using auxiliary floats at the wing tips
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cleaning Or Clearing Of The Surface Of Open Water (AREA)
Abstract
265,987. Rohrbach, A., (Assignee of Rohrbach Metall-Flugzeugbau, Ges.). Feb. 15, 1926, [Convention date]. Addition to 215,913. Planes, construction of. - A seaplane having floats b as described in the parent Specification is provided with auxiliary floats d arranged inside the supporting plane and consisting of watertight compartments at the free ends or extending throughout the length of the wing. When the thickness of the float is greater than that of the wing it Is provided with a supporting plane section o which prevents balancing of the air pressures above and below the wing by leakage across the tip. The wing may be made in three parts, the hinged nose and edge being designed as floating bodies if desired. The central part is provided with spar insets to serve as covers to facilitate riveting operations during construction. The float mav consist of an inflated rubber pocket. A drain plug may be provided in each float chamber.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE265987X | 1926-02-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB265987A true GB265987A (en) | 1927-06-30 |
Family
ID=5997218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3896/27A Expired GB265987A (en) | 1926-02-15 | 1927-02-11 | Improvements in seaplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB265987A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010144280A1 (en) | 2009-06-10 | 2010-12-16 | Icon Aircraft, Inc. | Wingtip and sponson interaction on an amphibious aircraft |
-
1927
- 1927-02-11 GB GB3896/27A patent/GB265987A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010144280A1 (en) | 2009-06-10 | 2010-12-16 | Icon Aircraft, Inc. | Wingtip and sponson interaction on an amphibious aircraft |
EP2440455A1 (en) * | 2009-06-10 | 2012-04-18 | Icon Aircraft, Inc. | Wingtip and sponson interaction on an amphibious aircraft |
CN102438900A (en) * | 2009-06-10 | 2012-05-02 | 图标飞机制造公司 | Wingtip and sponson interaction on an amphibious aircraft |
EP2440455A4 (en) * | 2009-06-10 | 2013-10-16 | Icon Aircraft Inc | Wingtip and sponson interaction on an amphibious aircraft |
CN102438900B (en) * | 2009-06-10 | 2017-02-08 | 图标飞机制造公司 | Wingtip and sponson interaction on an amphibious aircraft |
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