GB191225825A - Improvements in Aeroplanes. - Google Patents
Improvements in Aeroplanes.Info
- Publication number
- GB191225825A GB191225825A GB191225825DA GB191225825A GB 191225825 A GB191225825 A GB 191225825A GB 191225825D A GB191225825D A GB 191225825DA GB 191225825 A GB191225825 A GB 191225825A
- Authority
- GB
- United Kingdom
- Prior art keywords
- propellers
- casings
- curtains
- planes
- drawn
- 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
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
Abstract
25,825. Bernard, R. L. Nov. 10, 1911, [Convention date]. Aerial machines without aerostats; planes, construction of ; stopping way; steering; propelling.- An aeroplane is provided with a series of lifting- propellers 11 fitted inside conical casings 12 on the planes 1. Curtains 17 strengthened by buttons 18 may be drawn across the tops of the casings in case the motor stops. The motor 8 is connected to the propellers 11 through a clutch, by belt or chain gearing and by another clutch to the driving-propeller 7 so that either or both sets of propellers may be driven. The curtains 17 which are drawn across the casings 12 to check the descent are operated by cords 21 connected to a drum which is operated through toothed gearing from a hand-lever which can be locked in position.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US191225825XA | 1911-11-10 | 1911-11-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191225825A true GB191225825A (en) | 1913-06-05 |
Family
ID=32597117
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191225825D Expired GB191225825A (en) | 1911-11-10 | 1912-11-11 | Improvements in Aeroplanes. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191225825A (en) |
-
1912
- 1912-11-11 GB GB191225825D patent/GB191225825A/en not_active Expired
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