GB650526A - Improvements in rotary wing systems for aircraft - Google Patents
Improvements in rotary wing systems for aircraftInfo
- Publication number
- GB650526A GB650526A GB21751/49A GB2175149A GB650526A GB 650526 A GB650526 A GB 650526A GB 21751/49 A GB21751/49 A GB 21751/49A GB 2175149 A GB2175149 A GB 2175149A GB 650526 A GB650526 A GB 650526A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- propeller
- aircraft
- rotary wing
- crank
- 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
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/006—Paddle wheels
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Soil Working Implements (AREA)
Abstract
650,526. Propellers. OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AERONAUTIQUES (O.N.E.R.A.). Aug. 15, 1947, No. 21751/49. Convention date, May 15, 1944. Divided out of 650,460. [Classes 4 and 114] A propeller producing a force perpendicular to its axis, in addition to axial thrust, cornprises one or more pairs of aligned blades 1, 1a which are arranged to reciprocate in a casing 3 as the propeller revolves. As shown, reciprocation of the blades 1 is effected by a crank 14 integral with the driving shaft 15, the crank engaging an eccentric 13 freely rotatable in an annular member 12 to which the propeller blades are attached.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR650526X | 1944-05-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB650526A true GB650526A (en) | 1951-02-28 |
Family
ID=9004042
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB21751/49A Expired GB650526A (en) | 1944-05-15 | 1947-08-15 | Improvements in rotary wing systems for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB650526A (en) |
-
1947
- 1947-08-15 GB GB21751/49A patent/GB650526A/en not_active Expired
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