GB330513A - Improvements in aircraft employing rotative wings or supporting surfaces - Google Patents
Improvements in aircraft employing rotative wings or supporting surfacesInfo
- Publication number
- GB330513A GB330513A GB693829A GB693829A GB330513A GB 330513 A GB330513 A GB 330513A GB 693829 A GB693829 A GB 693829A GB 693829 A GB693829 A GB 693829A GB 330513 A GB330513 A GB 330513A
- Authority
- GB
- United Kingdom
- Prior art keywords
- centre
- gravity
- engine
- rotative wings
- starting
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/02—Gyroplanes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
330,513. Cierva Autogiro Co., Ltd., and La Cierva, J. de. March 4, 1929. Machines with rotary wing systems; controlling; starting. -The forward propelling means of an aircraft having freely rotative wings are mounted so that normally their r total thrust has substantially no moment about the centre of gravity. In a machine having a fixed engine the axis of the tractor propeller if produced would pass through the centre of gravity. Fig. 2 illustrates a machine in which the engine 35 is rockably mounted on trunnions 38<x> to allow of varying the, axis of thrust to positions above and below the centre of gravity. Control is effected by sector-and-pinion gear operated from a chainwheel 45, which, as shown, is provided with a hand-wheel 46 but may be mounted on or geared to the control cross-shaft operating the elevators. According to the Provisional Specification the engine may be tilted to cause the; slipstream therefrom to pass through the disc area of the rotative wings 32 for starting them in rotation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB693829A GB330513A (en) | 1929-03-04 | 1929-03-04 | Improvements in aircraft employing rotative wings or supporting surfaces |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB693829A GB330513A (en) | 1929-03-04 | 1929-03-04 | Improvements in aircraft employing rotative wings or supporting surfaces |
Publications (1)
Publication Number | Publication Date |
---|---|
GB330513A true GB330513A (en) | 1930-06-04 |
Family
ID=9823577
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB693829A Expired GB330513A (en) | 1929-03-04 | 1929-03-04 | Improvements in aircraft employing rotative wings or supporting surfaces |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB330513A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3149802A (en) * | 1961-09-11 | 1964-09-22 | Voorhis F Wigal | Autogiro |
-
1929
- 1929-03-04 GB GB693829A patent/GB330513A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3149802A (en) * | 1961-09-11 | 1964-09-22 | Voorhis F Wigal | Autogiro |
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