GB116914A - A Flying Machine. - Google Patents
A Flying Machine.Info
- Publication number
- GB116914A GB116914A GB880517A GB880517A GB116914A GB 116914 A GB116914 A GB 116914A GB 880517 A GB880517 A GB 880517A GB 880517 A GB880517 A GB 880517A GB 116914 A GB116914 A GB 116914A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shafts
- wing
- pair
- wings
- engine
- 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
- B64C33/00—Ornithopters
- B64C33/02—Wings; Actuating mechanisms therefor
Abstract
116,914. Roots, J. D. June 19, 1917. Aerial machines without aerostats; propelling.- A propelling- apparatus for ornithopter machines comprises a pair of shafts rotated in opposite directions and each carrying an obliquelyarranged disk rotating freelv within a carrier to which the wing is secured. Fig. 1 shows the two disks A, A' mounted on shafts C, C' and rotating within carriers G fixed to the wing spars 1. The two carriers are connected together by links M, or each may be connected by a link to the frame of the machine. The shafts are rotated in opposite directions by wheels J, J<1> engaging a worm L on the engine shaft. Several engines may be arranged behind one another with their shafts fore and aft and with a pair of wings in front and a pair behind each engine. Clutches may be provided between contiguous engines and on the wing shafts. The pair of wings, at one end of an engine may be 90 or 180 degrees in advance of the pair at the other end. In a modification, the disks A, A<1> are formed with double flanges at their peripheries embracing single flanges on the carriers. Specification 6418/09 is referred to. Steering and balancing.-The leading or other engine and wings may be bodily adjustable so as to alter the angles of incidence of the wings. Planes, construction of.-The rear portion of a wing is made flexible and may be composed of two or more strips of steel I<4>. I<5>, Fig. 4, arranged at intervals along the wing and covered with canvas, &c.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB880517A GB116914A (en) | 1917-06-19 | 1917-06-19 | A Flying Machine. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB880517A GB116914A (en) | 1917-06-19 | 1917-06-19 | A Flying Machine. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB116914A true GB116914A (en) | 1918-06-19 |
Family
ID=32670730
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB880517A Expired GB116914A (en) | 1917-06-19 | 1917-06-19 | A Flying Machine. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB116914A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2514639A (en) * | 1945-08-31 | 1950-07-11 | William F Haack | Oscillating vane aircraft |
CN109353498A (en) * | 2018-12-04 | 2019-02-19 | 南京航空航天大学 | The wing of flapping wing aircraft |
-
1917
- 1917-06-19 GB GB880517A patent/GB116914A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2514639A (en) * | 1945-08-31 | 1950-07-11 | William F Haack | Oscillating vane aircraft |
CN109353498A (en) * | 2018-12-04 | 2019-02-19 | 南京航空航天大学 | The wing of flapping wing aircraft |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2584115A (en) | Torque equalizer for counterrotating propellers | |
GB116914A (en) | A Flying Machine. | |
US1838327A (en) | Gyroscopic airplane | |
US2120821A (en) | Propelling device for aeroplanes | |
US2529033A (en) | Multirotor helicopter | |
US1858762A (en) | Airplane engine arrangement | |
US1450454A (en) | Lever-controlled paddle-action flying machine | |
US2436113A (en) | Airplane propeller | |
GB364986A (en) | Aeroplane with vertically oscillatable wings | |
US2649920A (en) | Cable drive for airplanes | |
US1883336A (en) | Screw propeller for aircraft | |
GB538046A (en) | Improvements in or relating to aircraft | |
GB214305A (en) | A combination helicopter aeroplane | |
US1418849A (en) | Toy aeroplane | |
US1973290A (en) | Turbine | |
US1230045A (en) | Flying-machine. | |
GB360275A (en) | Improvements in or relating to heavier than air aircraft | |
GB536865A (en) | Improvements in or relating to aircraft | |
US1854364A (en) | Airplane engine arrangement | |
US1818588A (en) | Aeroplane | |
US1557790A (en) | Motor arrangement for aircraft | |
GB191108394A (en) | Improvements in or connected with Propelling Mechanism for Mechanical Flying Machines. | |
US1358487A (en) | Flying-machine | |
GB461010A (en) | Improvements in and relating to propulsive systems for aircraft | |
GB191402080A (en) | Improvements in Propelling Devices for Flying Machines. |