GB696930A - Airplane rudders - Google Patents
Airplane ruddersInfo
- Publication number
- GB696930A GB696930A GB1977251A GB1977251A GB696930A GB 696930 A GB696930 A GB 696930A GB 1977251 A GB1977251 A GB 1977251A GB 1977251 A GB1977251 A GB 1977251A GB 696930 A GB696930 A GB 696930A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plates
- fuselage
- rudder
- shaft
- fast
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
696,930. Aircraft rudders. GLIWA, M. Aug. 22, 1951. No. 19772/51. Class 4. A rudder for an aircraft comprises a plate 17 connected to diverging plates 14 in turn connected at their upper and lower edges by end plates 15 fast with a vertical shaft 16. The rudder is mounted at the rear end of a fuselage which has end walls converging parallel to the plates 14 and supporting a bearing block 13 in which the shaft 16 is rotatably mounted. Plates 28 are secured to the fuselage to restrict the entry of air into the space formed between the plates 14 and the panels 11. The shaft 16 carries an extension rod 18 on which is mounted a spring loaded detent 27 arranged to engage with the teeth of a serrated plate 22 fast with the fuselage. The rudder may be mounted at the front end of the fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1977251A GB696930A (en) | 1951-08-22 | 1951-08-22 | Airplane rudders |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1977251A GB696930A (en) | 1951-08-22 | 1951-08-22 | Airplane rudders |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB696930A true GB696930A (en) | 1953-09-09 |
Family
ID=10134965
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1977251A Expired GB696930A (en) | 1951-08-22 | 1951-08-22 | Airplane rudders |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB696930A (en) |
-
1951
- 1951-08-22 GB GB1977251A patent/GB696930A/en not_active Expired
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB696930A (en) | Airplane rudders | |
| GB732657A (en) | Improvements to rotary wing aircraft | |
| GB786778A (en) | Improvements in or relating to machines for sonic or supersonic flight | |
| GB679897A (en) | Improvements in airplane construction | |
| GB548407A (en) | Improvements in aeroplane wings of variable camber and area | |
| GB924082A (en) | Improvements in airplanes powered by jet propulsion engines | |
| AU150930B2 (en) | Improvements in or relating to variable-pitch propellers | |
| AU150489B2 (en) | Improvements in or relating to aircraft fuel system | |
| AU522151A (en) | Improvements in or relating to variable-pitch propellers | |
| AU275051A (en) | Improvements in or relating to aircraft fuel system | |
| CA478238A (en) | Aircraft with sustaining airscrews | |
| CA475992A (en) | Aircraft utilizing magnus effect | |
| GB1007375A (en) | Means for permitting a vertical take-off aircraft to achieve forward flight at high speed | |
| AU154411B2 (en) | Improvements in or relating to rotary wing aircraft | |
| GB223966A (en) | Main plane incidence control for aeroplanes and the like | |
| GB784271A (en) | Improved air brakes | |
| GB609449A (en) | Aircraft incorporating an aerodynamic laboratory | |
| CA479411A (en) | Airplanes with high-lift channeled wings | |
| GB655931A (en) | Improvements in or relating to aircraft | |
| AU155000B2 (en) | Improvements in or relating to parachute releasing mechanisms | |
| CA467813A (en) | Variable pitch propellers with multiple tandem blades for aircraft | |
| CA491290A (en) | Aircraft sustaining rotor blade with airflow control | |
| AU154451A (en) | Improvements in or relating to rotary wing aircraft | |
| AU150679B2 (en) | Improvements in or relating to sheet classifier plant | |
| AU132496B2 (en) | Improvements in or relating to air intakes for highspeed flight |