GB488967A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB488967A GB488967A GB18468/37A GB1846837A GB488967A GB 488967 A GB488967 A GB 488967A GB 18468/37 A GB18468/37 A GB 18468/37A GB 1846837 A GB1846837 A GB 1846837A GB 488967 A GB488967 A GB 488967A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- adjustable
- controlling
- independently
- articulated
- 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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
488,967. Controlling aircraft. POLLOPAS PATENTS, Ltd. (RougÚ, C. R. A.-M. de) July 2, 1937, No. 18468. [Class 4] In an aircraft provided with controlling and stabilizing surfaces disposed above the supporting-planes, the surface comprises a plurality of independently adjustable units mounted one behind the other, side by side, or on universal joints. In one form, two independent surfaces 2, 3 are articulated on the axle 1. In a modification the part 2 is fixed relatively to the aircraft and, in a further form, a central section 11 is pivotally mounted on a support 14 and carries adjustable articulated surfaces 10, 12. In a still further form, three adjustable surfaces are disposed side by side on a common axle. In another modification the surfaces are adjustable on axles universally pivoted to the support and independently adjustable. The surfaces may be adjusted independently of, or together with, the usual aircraft controlling and stabilizing surfaces if provided. Specifications 362,776 and 459,639 are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB18468/37A GB488967A (en) | 1937-07-02 | 1937-07-02 | Improvements in or relating to aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB18468/37A GB488967A (en) | 1937-07-02 | 1937-07-02 | Improvements in or relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB488967A true GB488967A (en) | 1938-07-18 |
Family
ID=10112932
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB18468/37A Expired GB488967A (en) | 1937-07-02 | 1937-07-02 | Improvements in or relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB488967A (en) |
-
1937
- 1937-07-02 GB GB18468/37A patent/GB488967A/en not_active Expired
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