GB191006388A - Aerial Machines. - Google Patents
Aerial Machines.Info
- Publication number
- GB191006388A GB191006388A GB191006388DA GB191006388A GB 191006388 A GB191006388 A GB 191006388A GB 191006388D A GB191006388D A GB 191006388DA GB 191006388 A GB191006388 A GB 191006388A
- Authority
- GB
- United Kingdom
- Prior art keywords
- planes
- blades
- fixed
- shaft
- propellers
- 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
- 230000004048 modification Effects 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 2
- 238000010276 construction Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 abstract 1
- 230000003028 elevating effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
- B64C39/006—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a vertical axis
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
Abstract
6388. Losse, E. March 14. Aerial machines without aerostats; planes, arrangement of. - An aeroplane comprises a body a, Figs. 1 and 2, of semicylindrical shape, rear fixed planes b, d, forward circular revolving planes e adapted to act also as propellers, front and rear elevators h, i, a fixed vertical plane 11 at the rear, and screw propellers f. In a modification, Fig. 10, the front elevator and the screw propellers are dispensed with, the propulsion being effected solely by the rotary propellers e, and elevating by a tail 12. Moreover, the planes b, d are replaced by planes b<1>, and a rear rudder 13 is provided. Propelling is effected by means of feathering blades x, y, Figs. 7 and 8, mounted on a pair of oppositely rotating disks e, which are connected to vertical shafts o driven from the engine, and consist of circular planes of canvas connected to centre-pieces n and stretched by spokes m. The blades x, y are secured at right-angles to each other upon a shaft v, which is connected to the disks e and mounted to rotate in a bearing w fixed to the shaft o. Feathering is effected by means of arms z fixed to the shaft v and fitted with rollers 2, which engage a cam 3 mounted at the top of a sleeve 4. The shafts o are further fitted with auxiliary blades 6, Figs. 1 and 2. In a modification, Figs. 10 and 12, two blades x<1>, y<1> are mounted upon separate shafts v<1>, v<2>, one of which has an arm engaging the cam 3 described above and communicates its motion derived therefrom to the other shaft for feathering, by means of pinions 14, 15. The blades may be arranged at either side of the disk e, and they may be connected at their outer corners 16 to the disk e by ropes, which serve to take the strain when the blades are open. The blades x<1>, y<1> are slightly concave, as shown at 17, Fig. 10, and are strengthened by stays 19. They are further provided in their concavities with transverse blades 20, Fig. 12, which are also concave towards the disk e and aid in the propelling effect. Planes, construction of. - The supporting- surfaces consist of a semicylindrical body a provided at opposite sides with fixed planes b, d, Fig. 2, or b<1>, Fig. 10, and also of rotating disks e consisting of circular planes of canvas connected to a centre-piece n, Fig. 7, and stretched by spokes m. Steering.-In the machine shown in Figs. 1 and 2, rear elevators i are arranged to be adjusted independently by the same gear that is used to operate the steering-wheel k. A fixed vertical plane 11 is also provided to aid in steering. Balancing.-The rotating disks e mounted at opposite sides of the machine serve to increase the stability of the machine.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB191006388T | 1910-03-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191006388A true GB191006388A (en) | 1911-03-14 |
Family
ID=32637719
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191006388D Expired GB191006388A (en) | 1910-03-14 | 1910-03-14 | Aerial Machines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191006388A (en) |
-
1910
- 1910-03-14 GB GB191006388D patent/GB191006388A/en not_active Expired
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