GB219664A - - Google Patents
Info
- Publication number
- GB219664A GB219664A GB15542/24A GB1554224A GB219664A GB 219664 A GB219664 A GB 219664A GB 15542/24 A GB15542/24 A GB 15542/24A GB 1554224 A GB1554224 A GB 1554224A GB 219664 A GB219664 A GB 219664A
- Authority
- GB
- United Kingdom
- Prior art keywords
- skin
- plane
- blade
- suction side
- cylinders
- 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
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/08—Influencing air flow over aircraft surfaces, not otherwise provided for using Magnus effect
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
- Hydraulic Turbines (AREA)
Abstract
219,664. Naamlooze Vennootschap Instituut voor Aero-en Hydro-Dynamiek. June 28, 1923, [Convention date]. Paddle-wheels and endless band propellers; rudders. - The rudders and sails of ships and the blades of propellers have the whole or a portion of their surface skin movable around or along the surface in order to increase the reaction of the plane or blade. The skin is positively driven by a prime mover or by separate vanes acted upon by the fluid current, or is dragged round by the skin friction of the fluid current on the suction side of the plane or blade. Fig. 3 shows an aircraft plane having fixed profile members e, f and an endless flexible skin d passed over rollers b, c, the upper part moving in the direction of the airstream, and both parts assuming their correct shape under air pressure. Either or both of the profile members e, f may be omitted. Fig. 8 shows a modification in which the movable skin d is exposed only on the suction side of the plane or blade. The movable skin may be replaced by a series of rollers partially embedded in the suction side of the plane, or a single cylindrical member h, Fig. 5, may be placed between front and rear profile members e, f, or, as shown in Fig. 7, within a recess in a profile member k so as to form a tapering passage around the cylinder. Or rotating cylinders may be used alone, a cylinder rotating about a vertical axis or having a rotary skin being described for use on a ship, the direction of rotation of the surface controlling the direction of motion of the vessel. Such cylinders may be made in telescopic sections. Profiled extension pieces controlled by auxiliary surfaces may be provided with the cylinders when used as sails.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE219664T | 1923-07-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB219664A true GB219664A (en) | 1925-10-27 |
Family
ID=31893409
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15542/24A Expired GB219664A (en) | 1923-07-28 | 1924-06-27 |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB219664A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2532899A (en) * | 1945-08-24 | 1950-12-05 | Dubost Charles | Aerodynamic lifting device |
US2569983A (en) * | 1943-01-19 | 1951-10-02 | Onera (Off Nat Aerospatiale) | Aircraft wing flap with a leading edge roller |
US5314308A (en) * | 1992-12-11 | 1994-05-24 | Dynamic Engineering, Inc. | System for controlling higher harmonic vibrations in helicopter rotor blades |
US20170175705A1 (en) * | 2015-12-22 | 2017-06-22 | Theodore M. Garver | Fluid interface devices with stabilization features as well as airfoil assemblies including same |
-
1924
- 1924-06-27 GB GB15542/24A patent/GB219664A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2569983A (en) * | 1943-01-19 | 1951-10-02 | Onera (Off Nat Aerospatiale) | Aircraft wing flap with a leading edge roller |
US2532899A (en) * | 1945-08-24 | 1950-12-05 | Dubost Charles | Aerodynamic lifting device |
US5314308A (en) * | 1992-12-11 | 1994-05-24 | Dynamic Engineering, Inc. | System for controlling higher harmonic vibrations in helicopter rotor blades |
US20170175705A1 (en) * | 2015-12-22 | 2017-06-22 | Theodore M. Garver | Fluid interface devices with stabilization features as well as airfoil assemblies including same |
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