GB148293A - Auxiliary steering gear for aircraft - Google Patents
Auxiliary steering gear for aircraftInfo
- Publication number
- GB148293A GB148293A GB20204/20A GB2020420A GB148293A GB 148293 A GB148293 A GB 148293A GB 20204/20 A GB20204/20 A GB 20204/20A GB 2020420 A GB2020420 A GB 2020420A GB 148293 A GB148293 A GB 148293A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plane
- auxiliary
- planes
- arms
- pilot
- 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
Abstract
148,293. Flettner, A. Sept. 22, 1917, [Convention date]. Steering and balancing. - In aircraft steering-apparatus in which adjustment of a main steering-plane by the pilot moves an auxiliary plane into position to assist the operation, the auxiliary plane is arranged to have a translational as well as a pivotal movement. The Figure shows a control plane b connected by linkage r, s, t to arms c, c' which carry the auxiliary plane a, movement of which about its pivot is caused by a connexion d, i to a fixed point k. As the plane b is adjusted by the pilot, the plane a is moved bodily upwards or downwards as well as about its pivot. The auxiliary plane may be set at a greater angle than the control plane, and the rod and lever connexion may be replaced by wires, toothed sectors, &c. The Specification as open to inspection under Sect. 91 (3) (a) comprises also the following, which does not appear in the Specification as accepted : Steering and balancing.-Fig. 1 (Cancelled) shows the auxiliary plane a carried by arms c geared by toothed sectors to the control plane o, the plane a being, in this case, adjusted directly by the pilot, whereupon the air pressure thereon effects an adjustment of the plane b in the same sense. In another form, the connexion between the planes a, b comprises linkage r, s, t as described above, but the auxiliary plane is moved directly by the pilot by control wires passing over pulleys on the axis of the arms c, c'. Fig. 4 (Cancelled) shows gearing whereby a second auxiliary plane a<1> carried beyond the auxiliary plane a is actuated by the pilot; or the second plane a' may be arranged within the arms c, c<1> of the first plane a. Fig. 6 (Cancelled) shows a modified arrangement with two auxiliary planes a, a' operated by control wires, as shown. A pair of auxiliary planes may be arranged one at each side of the fuselage for adjusting the elevators, in which case the arms carrying the auxiliary planes may be arranged within the fuselage with the free ends projecting through slots in the sides of the fuselage and carrying tho auxiliary planes. One auxiliary plane may serve to operate several wing- flaps. To protect the auxiliary planes against squalls, protective planes may be arranged at the sides. Planes, construction of.-In some cases, the arms carrying the auxiliary planes may be arranged within the main planes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE148293X | 1917-09-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB148293A true GB148293A (en) | 1922-01-09 |
Family
ID=5672591
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB20204/20A Expired GB148293A (en) | 1917-09-22 | 1920-07-09 | Auxiliary steering gear for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB148293A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2255537A (en) * | 1991-05-01 | 1992-11-11 | Peter John Croft Phillips | Aircraft control systems. |
-
1920
- 1920-07-09 GB GB20204/20A patent/GB148293A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2255537A (en) * | 1991-05-01 | 1992-11-11 | Peter John Croft Phillips | Aircraft control systems. |
GB2255537B (en) * | 1991-05-01 | 1995-02-08 | Peter John Croft Phillips | Aircraft control systems |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2665084A (en) | Flap actuator and control system | |
US2908454A (en) | Aircraft wing | |
GB148293A (en) | Auxiliary steering gear for aircraft | |
US2720368A (en) | Aerodynamic balance for aircraft | |
US2678179A (en) | Hydraulic trim control | |
GB747507A (en) | Improvements in control systems for actuating the control surfaces of an airplane, particularly control systems for conjointly operating the airplane ailerons and landing flaps | |
US2699687A (en) | Mechanical movement | |
US3386690A (en) | Direct lift control system | |
US3070334A (en) | Flying control system for aircraft | |
GB148172A (en) | Improvements relating to the steering planes of air-craft | |
US2974903A (en) | Aircraft having wings provided with flaps and gas blowing means | |
GB582380A (en) | Improvements in or relating to means for controlling the synchronous operation of a plurality of hydraulic jacks | |
US3016215A (en) | Aerodynamic aircraft control system | |
US2553694A (en) | Aircraft control surface | |
GB1223602A (en) | Improvements in or relating to flight control systems for controlling lift and propulsion devices | |
US3166274A (en) | Pre-tensioned control system for control surfaces of an aircraft | |
US1605398A (en) | Controlling device for aeroplanes | |
US3709056A (en) | Coordinate transformer for transforming control signals in airplanes | |
US2682381A (en) | Combined aileron and landing flap | |
GB417898A (en) | Improvements in or relating to the controlling mechanism of aeroplanes | |
GB485794A (en) | Improvements in or relating to aircraft | |
US2758806A (en) | Airplane safety control system | |
GB558006A (en) | Improvements in or relating to the control surfaces of aircraft | |
USRE23143E (en) | Aileron-rudder tab linkage | |
GB517895A (en) | Improvements in or relating to lifting surfaces of aircraft |