GB168364A - Improvements in or relating to aircraft blades, planes, aerocurves and the like - Google Patents
Improvements in or relating to aircraft blades, planes, aerocurves and the likeInfo
- Publication number
- GB168364A GB168364A GB1394320A GB1394320A GB168364A GB 168364 A GB168364 A GB 168364A GB 1394320 A GB1394320 A GB 1394320A GB 1394320 A GB1394320 A GB 1394320A GB 168364 A GB168364 A GB 168364A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- propellers
- aerocurves
- planes
- relating
- 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
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/467—Aerodynamic features
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
168,364. Davidson, G. L. O. May 20, 1920. Screw and like propellers.-Propellers for aircraft are constructed with a number of blades of aerofoil section set close together, the rear upper surface of each blade being turned up to direct the air current on to the convex upper surface at the front of the next blade. The undersurfaces are flat or slightly concave and their chords are horizontal. Fig. 2 shows blades 7 set by means of tongues 8 in concentric rings 4 supported by spokes 5 and wire bracing 6 from discs on a central sleeve. The hub is covered to the outer ring 4, which has a radius greater than the length of the blades 7. The blades 7 are inclined radially towards the direction of thrust, and the outer edges are clamped between two rings 10 with interposed filling-pieces.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1394320A GB168364A (en) | 1920-05-20 | 1920-05-20 | Improvements in or relating to aircraft blades, planes, aerocurves and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1394320A GB168364A (en) | 1920-05-20 | 1920-05-20 | Improvements in or relating to aircraft blades, planes, aerocurves and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
GB168364A true GB168364A (en) | 1921-08-22 |
Family
ID=10032169
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1394320A Expired GB168364A (en) | 1920-05-20 | 1920-05-20 | Improvements in or relating to aircraft blades, planes, aerocurves and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB168364A (en) |
-
1920
- 1920-05-20 GB GB1394320A patent/GB168364A/en not_active Expired
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