GB416326A - Improved control surfaces for air and water-craft - Google Patents
Improved control surfaces for air and water-craftInfo
- Publication number
- GB416326A GB416326A GB13730/33A GB1373033A GB416326A GB 416326 A GB416326 A GB 416326A GB 13730/33 A GB13730/33 A GB 13730/33A GB 1373033 A GB1373033 A GB 1373033A GB 416326 A GB416326 A GB 416326A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aileron
- leading edge
- span
- craft
- air
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C2009/005—Ailerons
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Treatment Of Fiber Materials (AREA)
- Toys (AREA)
Abstract
416,326. Controlling aircraft and submarines. HARTSHORN, A. S., Royal Aircraft Establishment, South Farnborough, Hampshire. May 11, 1933, No. 13730. [Classes 4 and 114.] A balanced aileron or other control surface has the whole or a part of its leading portion of a section varying in the direction of its span so that as the trailing edge is moved upwards the leading edge 4 progressively projects below the lower surface of a fixed plane 3. Figs. 1, 2, 3 show sections through a wing and aileron at three successive points along the span, the leading edge 4 of the aileron being continuously inclined with respect to its hinge axis 2. This inclination may extend over a portion only of the aileron, or the aileron may be divided into two or more portions each of which has its leading edge so inclined. In alternative constructions the leading edge rises from the position shown in Fig. 3 at one end to that shown in Fig. 2 at the other, or both ends may be shaped as shown in Fig. 3 and the centre section formed as shown in Fig. 2. The invention may be applied to underwater craft.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13730/33A GB416326A (en) | 1933-05-11 | 1933-05-11 | Improved control surfaces for air and water-craft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13730/33A GB416326A (en) | 1933-05-11 | 1933-05-11 | Improved control surfaces for air and water-craft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB416326A true GB416326A (en) | 1934-09-11 |
Family
ID=10028320
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13730/33A Expired GB416326A (en) | 1933-05-11 | 1933-05-11 | Improved control surfaces for air and water-craft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB416326A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2285960A (en) * | 1994-01-31 | 1995-08-02 | John Graham Walker | Wingsail |
-
1933
- 1933-05-11 GB GB13730/33A patent/GB416326A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2285960A (en) * | 1994-01-31 | 1995-08-02 | John Graham Walker | Wingsail |
GB2285960B (en) * | 1994-01-31 | 1998-02-04 | John Graham Walker | Monoplane and low thrust wingsail arrangements |
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