GB574151A - Improvements relating to aircraft rudders - Google Patents
Improvements relating to aircraft ruddersInfo
- Publication number
- GB574151A GB574151A GB389/44A GB38944A GB574151A GB 574151 A GB574151 A GB 574151A GB 389/44 A GB389/44 A GB 389/44A GB 38944 A GB38944 A GB 38944A GB 574151 A GB574151 A GB 574151A
- Authority
- GB
- United Kingdom
- Prior art keywords
- corrector
- flap
- rudder
- aircraft
- improvements relating
- 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)
- Tires In General (AREA)
Abstract
574,151. Controlling aircraft. ARMSTRONG WHITWORTH AIRCRAFT, Ltd., SIR W. G., and LLOYD, J. Jan. 8, 1944, No. 389. [Class 4] A rudder 23 is mounted on a corrector flap 22 which can be set to introduce correction in any desired direction by irreversible mechanism, such as a hydraulic jack 29 attached to the vertical fin 20. The rudder may be provided with a servo tab 24, and at its leading edge may carry a balancing vane 26 which projects into a recess 27 at the trailing edge portion of the corrector flap. The corrector flap and rudder together occupy about one-half of the overall cord length. Specification 573,084 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB389/44A GB574151A (en) | 1944-01-08 | 1944-01-08 | Improvements relating to aircraft rudders |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB389/44A GB574151A (en) | 1944-01-08 | 1944-01-08 | Improvements relating to aircraft rudders |
Publications (1)
Publication Number | Publication Date |
---|---|
GB574151A true GB574151A (en) | 1945-12-21 |
Family
ID=9703550
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB389/44A Expired GB574151A (en) | 1944-01-08 | 1944-01-08 | Improvements relating to aircraft rudders |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB574151A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2582348A (en) * | 1946-07-08 | 1952-01-15 | Northrop Aircraft Inc | Control system for aircraft control surfaces |
US2661170A (en) * | 1950-02-11 | 1953-12-01 | A V Roe Canada Ltd | Means for controlling aircraft in flight |
-
1944
- 1944-01-08 GB GB389/44A patent/GB574151A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2582348A (en) * | 1946-07-08 | 1952-01-15 | Northrop Aircraft Inc | Control system for aircraft control surfaces |
US2661170A (en) * | 1950-02-11 | 1953-12-01 | A V Roe Canada Ltd | Means for controlling aircraft in flight |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB574151A (en) | Improvements relating to aircraft rudders | |
GB582206A (en) | Improvements in tailless airplanes | |
GB550713A (en) | Improvements in or relating to aerofoils | |
GB837809A (en) | An improved split flap arrangement in aircraft | |
GB628684A (en) | Improvements in aircraft control surfaces | |
GB432124A (en) | Improvements in aircraft of the helicopter type | |
GB520962A (en) | Improvements in or relating to means for balancing the control surfaces of aircraft | |
GB519236A (en) | Improvements in and relating to supporting surfaces for aircraft | |
GB574152A (en) | Improvements in aircraft aerofoils incorporating control surfaces | |
GB558216A (en) | Improvements relating to aircraft | |
GB1014985A (en) | Improvements in or relating to aircraft | |
GB568910A (en) | Improvements relating to the control surfaces of aircraft | |
GB558047A (en) | Improvements relating to the control of aircraft | |
GB519718A (en) | Improvements in or relating to retractable aircraft wing flaps | |
GB456177A (en) | Improvements in or relating to aircraft provided with rotating wings | |
GB593932A (en) | Improvements in the construction of aeroplanes | |
GB596971A (en) | Improvements in automatic variable pitch propeller | |
GB559810A (en) | Improvements in aircraft elevators | |
HOSOKAWA | Application of transonic linearization to airfoil with round leading edge | |
GB591933A (en) | Improvements relating to high speed water-craft | |
GB652248A (en) | Improvements relating to aircraft | |
GB143953A (en) | Improvements in or connected with the planes of aeroplanes | |
GB664171A (en) | Improvements in wings for axial flow fans | |
GB759622A (en) | Improvements in or relating to rotary wing aircraft | |
GB739080A (en) | Improvements relating to servo-tabs for aircraft control surfaces |