GB464607A - Improvements relating to aeroplanes, seaplanes and the like - Google Patents
Improvements relating to aeroplanes, seaplanes and the likeInfo
- Publication number
- GB464607A GB464607A GB16196/36A GB1619636A GB464607A GB 464607 A GB464607 A GB 464607A GB 16196/36 A GB16196/36 A GB 16196/36A GB 1619636 A GB1619636 A GB 1619636A GB 464607 A GB464607 A GB 464607A
- Authority
- GB
- United Kingdom
- Prior art keywords
- arm
- wings
- crank
- vibratory
- wing
- 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
- 239000004744 fabric Substances 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C33/00—Ornithopters
- B64C33/02—Wings; Actuating mechanisms therefor
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
464,607. Vibratory propellers for aircraft. OWEN, B. June 10, 1936, No. 16196. Convention date, June 13, 1935. [Class 4] In an aeroplane or the like in addition to the ordinary supporting wings one or more pairs of wings are arranged to project laterally from the fuselage and are actuated mechanically with a part-rotary part-reciprocatory movement. As shown in Fig. 2, a wing 2 is formed at its root with an arm 4 carried through the intermediary of a flexible joint by a longitudinally disposed link 6 one end of which is slotted to embrace a fixed pivot 12, and the other end provided with a bearing 7 to receive a driving crank or eccentric 8 ; the inner end of arm 4 is located in a fixed flexible bearing 5. Crank 8 is formed on an engine driven shaft 9 which is common to one pair of wings. The flexible joints comprise metal liners connected to their respective housings by rubber or rubber and fabric bushes, and whilst permitting universal movement to arm 4 do not allow of its rotation. Pivot 12, crank-shaft bearings 10 and universal joint 5 are carried by a frame 17, Fig. 3, which is angularly adjustable by the worm gearing shown to alter the mean angle of incidence of the vibratory wing.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NZ464607X | 1935-06-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB464607A true GB464607A (en) | 1937-04-21 |
Family
ID=19915816
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB16196/36A Expired GB464607A (en) | 1935-06-13 | 1936-06-10 | Improvements relating to aeroplanes, seaplanes and the like |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB464607A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2504369A (en) * | 2013-03-05 | 2014-01-29 | Cvr Ltd | Aircraft wing with reciprocating outer aerofoil sections |
-
1936
- 1936-06-10 GB GB16196/36A patent/GB464607A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2504369A (en) * | 2013-03-05 | 2014-01-29 | Cvr Ltd | Aircraft wing with reciprocating outer aerofoil sections |
| GB2504369B (en) * | 2013-03-05 | 2014-06-25 | Cvr Ltd | Aircraft wing |
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