GB294663A - Improvements in aircraft - Google Patents
Improvements in aircraftInfo
- Publication number
- GB294663A GB294663A GB21871/28A GB2187128A GB294663A GB 294663 A GB294663 A GB 294663A GB 21871/28 A GB21871/28 A GB 21871/28A GB 2187128 A GB2187128 A GB 2187128A GB 294663 A GB294663 A GB 294663A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- biplane
- nuts
- lowering
- frames
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/54—Varying in area
- B64C3/546—Varying in area by foldable elements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/54—Varying in area
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Tires In General (AREA)
Abstract
294,663. Tammeo, A., and Caminada, E. July 29, 1927, [Convention date]. Aeroplanes; planes, arrangement and construction of; controlling.-A monoplane is convertible during flight into a biplane (or a biplane into a triplane) by lowering a wing 2 nested under the main wing 1 by screws acting on frames 5<1>, 7 attached to the wing- spars. By unequally lowering the front and back spars the wing 2 can be given varying incidence. The screws are enclosed in stream-line struts 4<1>, slotted to give passage to the brackets 21 connecting the nuts 15 to frames 5<1> and reinforced by bars 17', 17" which are grooved to serve as guides for the nuts. The wing 2 moves between inclined struts connecting the plane 1 to the fuselage, and in one form, no provision is made for varying the incidence of the wing 2.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT294663X | 1927-07-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB294663A true GB294663A (en) | 1929-01-10 |
Family
ID=11227038
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB21871/28A Expired GB294663A (en) | 1927-07-29 | 1928-07-27 | Improvements in aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB294663A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5681014A (en) * | 1992-05-15 | 1997-10-28 | Palmer; Harry W. | Torsional twist airfoil control means |
-
1928
- 1928-07-27 GB GB21871/28A patent/GB294663A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5681014A (en) * | 1992-05-15 | 1997-10-28 | Palmer; Harry W. | Torsional twist airfoil control means |
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