GB191217933A - Improvements in and relating to Aerial Machines. - Google Patents
Improvements in and relating to Aerial Machines.Info
- Publication number
- GB191217933A GB191217933A GB191217933DA GB191217933A GB 191217933 A GB191217933 A GB 191217933A GB 191217933D A GB191217933D A GB 191217933DA GB 191217933 A GB191217933 A GB 191217933A
- Authority
- GB
- United Kingdom
- Prior art keywords
- propellers
- planes
- framework
- vanes
- driven
- 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
- 230000035939 shock Effects 0.000 abstract 2
- 244000286663 Ficus elastica Species 0.000 abstract 1
- RRHGJUQNOFWUDK-UHFFFAOYSA-N Isoprene Chemical compound CC(=C)C=C RRHGJUQNOFWUDK-UHFFFAOYSA-N 0.000 abstract 1
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 238000010276 construction Methods 0.000 abstract 1
- 229920001195 polyisoprene Polymers 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
Abstract
17,933. Ayers, T. G. I. Aug. 2. Aerial machines without aerostats; shock of landing, deadening; framework.-An aerial machine comprises a pyramidal framework a with one or more lifting-propellers n, rand one or more driving-propellers 18, the two sets of propellers being driven by the same or separate motors. Lowered planes or planes hinged to the framework and adapted to be automatically or manually raised into an horizontal position are provided. The lower ends of the member a are provided with parts 19 sliding in hollow parts 21 under spring control and having india-rubber feet 20 to absorb shock of landing. Propelling.-The propellers are shown driven by a single engine 6, Fig. 4, mounted so as to be vertically adjustable, but two engines may be used. The propellers m, r on the shafts h, p are oppositely driven through the gearing shown. During the ascent, the propeller 18 on the shaft 10 is put out of action by the engagement of a hook with a collar 14 fixed to the shaft 10, which causes the clutches 8, 9 to be put out of gear. Release of the hook enables the spring 11 to place the clutches in gear. Steering; planes, arrangement and construction of.-Upper and lower frames 26 carrying pivoted vanes 28 are fixed to the frame a at opposite sides. A greater area is arranged at one side than at the other of the vane axles in order that they will be closed by air pressure. The vanes may be operated all by a single lever, or separate levers for the two sides of the machine, arranged so as to be connected together for simultaneous operation may be used. The lower sets of planes may be operated separately. The planes may be hinged so as to rise automatically when the machine falls. Racks and pinions or links may be used for operating the vanes. An elevator 34 is provided. Cars.-The car is mounted on the cross-stays f and is provided with windows. The outside of the cabin is given a stream line formation in the upward and forward directions.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB191217933T | 1912-08-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB191217933A true GB191217933A (en) | 1913-07-24 |
Family
ID=32642582
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB191217933D Expired GB191217933A (en) | 1912-08-02 | 1912-08-02 | Improvements in and relating to Aerial Machines. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB191217933A (en) |
-
1912
- 1912-08-02 GB GB191217933D patent/GB191217933A/en not_active Expired
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