GB190928195A - Improvements in or relating to Aeroplanes or the like. - Google Patents
Improvements in or relating to Aeroplanes or the like.Info
- Publication number
- GB190928195A GB190928195A GB190928195DA GB190928195A GB 190928195 A GB190928195 A GB 190928195A GB 190928195D A GB190928195D A GB 190928195DA GB 190928195 A GB190928195 A GB 190928195A
- Authority
- GB
- United Kingdom
- Prior art keywords
- machine
- planes
- operated
- motor
- clutched
- 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
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
Abstract
28,195. Verity, C. H. A. Dec. 2. [Cognate Application, 10,902/10.] Aerial machines without aerostats; planes, arrangement of. -A flying-machine comprises upper and lower fixed planes or series of planes A, B connected together by framework E so that the upper planes A form an inverted dihedral and the lower planes B form a dihedral angle, as shown in Fig. 4. When series of planes are used, they are spaced apart and arranged in steps as shown in Fig. 1, and the angle of incidence or the area of the planes may increase towards the rear to give increased lifting effect. Moreover, each upper plane may be of greater area than the one below it; for example, each upper plane may extend at each side of the machine a distance of two feet beyond the lower plane. The machine is moreover provided with duplicated motors and propellers N, N' and F, F', elevators C operated by duplicate controls M, and rudders S<2> operated by duplicate pedals P<1>. Vertical fins may be fixed at or near the ends of each plane. Propelling.-The machine is provided with two propellers F, F' arranged as shown and driven independently by separate motors N, N'. The propellers are mounted loosely on their motor shafts but may be clutched thereto, the arrangement being such that, when only one motor is being used, the other propeller is unclutched and is rotated by the head-wind, so that when clutched to its motor shaft, its momentum serves to start the motor. Steering and balancing; stopping way.-The machine is steered vertically and balanced by elevators C hinged at each side of the machine to the rear of the top front planes A, and controlled independently by wires D connected to controlling-gear M placed at each side of the aviator. Two pairs of control gear M are provided for use by two drivers, and are connected together so as to facilitate teaching. Each control wheel M is fixed to a drum D', Fig. 3, to which the cables D are connected, and is operated by a lever T mounted loosely on the shaft S<1>. The lever T is clutched to the wheel M by pressing a spring push T<2>, and is simultaneously unclutched from a fixed boss C<1> by the withdrawal of spring bolts T<1> operated by wires W<1>. The machine is further provided with two rear rudders S<2> operated by pedals P<1>, which are also duplicated. The elevators and rudders may be moved at right-angles to the line of flight for braking the machine after landing. Shock of landing, deadening.-The machine is provided with land-wheels W mounted on long flexible shafts H, which bend upwards so that skids P come into contact with the ground when the shock of landing is severe.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB190928195T | 1909-12-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190928195A true GB190928195A (en) | 1910-12-01 |
Family
ID=32447044
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190928195D Expired GB190928195A (en) | 1909-12-02 | 1909-12-02 | Improvements in or relating to Aeroplanes or the like. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB190928195A (en) |
-
1909
- 1909-12-02 GB GB190928195D patent/GB190928195A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1568765A (en) | Helicopter | |
US1869326A (en) | Control system for airplanes and the like | |
US1652554A (en) | Aircraft | |
GB190928195A (en) | Improvements in or relating to Aeroplanes or the like. | |
US1815341A (en) | Aeroplane machine | |
US2172813A (en) | Control for airplane vehicles and ground steering gear therefor | |
US1819863A (en) | Helicopter | |
US2216489A (en) | Machine for training student pilots in handling airplanes | |
US1781910A (en) | Flying machine | |
US1859716A (en) | Airplane | |
US1987606A (en) | Combined front and rear propelling and steering mechanism for aircraft | |
US1132049A (en) | Flying-machine. | |
US1046895A (en) | Flying-machine. | |
US991686A (en) | Apparatus for aerial navigation. | |
US1322976A (en) | Aeropiane | |
US1570121A (en) | Helicopter | |
US1141347A (en) | Monoplane. | |
US1037657A (en) | Aeroplane. | |
US1074281A (en) | Apparatus for aerial navigation. | |
US1272712A (en) | Aeroplane. | |
US1468847A (en) | Helicopter | |
US1429730A (en) | Aeroplane | |
US906406A (en) | Aeroplane flying-machine. | |
US1183799A (en) | Flying-machine. | |
US1032967A (en) | Flying-machine. |