GB437465A - Improvements in or relating to wing tip floats for seaplanes - Google Patents
Improvements in or relating to wing tip floats for seaplanesInfo
- Publication number
- GB437465A GB437465A GB1910134A GB1910134A GB437465A GB 437465 A GB437465 A GB 437465A GB 1910134 A GB1910134 A GB 1910134A GB 1910134 A GB1910134 A GB 1910134A GB 437465 A GB437465 A GB 437465A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cylinder
- float
- wing
- seaplane
- dashpot
- 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)
- Toys (AREA)
- Earth Drilling (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Abstract
437,465. Hydraulic shock-absorbers. SHORT, H. O., and GOUGE, A., Seaplane Works, Rochester, Kent. June 28, 1934, No. 19101. [Class 108 (iii)] [See also Group XXXIII] A dashpot or equivalent frictional connection is interposed between a seaplane wing and a wing tip float in order to absorb oscillations occurring in the wing and float and thus to prevent the wing and float from oscillating together as a unit. Swinging movements of the float are controlled by a dashpot contained in a telescopic diagonal strut comprising a tube 15 carrying an oil cylinder 81 which is a sliding fit within a tube 16 which carries a piston rod 19 passing through stuffing boxes on plugs fitted at either end of cylinder 18. A perforated piston 20 is mounted on rod 19 substantially midway of cylinder 18 and provides an abutment for coiled springs 23, 123. The outer end of spring 123 abuts against a thrust bearing 27 carried by cylinder closing plug 29. Cylinder 18 is filled with oil through an aperture normally closed by a screw 40, a second screw serving to close an air vent. Expansion of the strut is limited by a stop 31 carried by piston rod 19 and contraction by the opposed ends of cylinders 15, 16.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1910134A GB437465A (en) | 1934-06-28 | 1934-06-28 | Improvements in or relating to wing tip floats for seaplanes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1910134A GB437465A (en) | 1934-06-28 | 1934-06-28 | Improvements in or relating to wing tip floats for seaplanes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB437465A true GB437465A (en) | 1935-10-30 |
Family
ID=10123787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1910134A Expired GB437465A (en) | 1934-06-28 | 1934-06-28 | Improvements in or relating to wing tip floats for seaplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB437465A (en) |
-
1934
- 1934-06-28 GB GB1910134A patent/GB437465A/en not_active Expired
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