GB131648A - - Google Patents
Info
- Publication number
- GB131648A GB131648A GB131648DA GB131648A GB 131648 A GB131648 A GB 131648A GB 131648D A GB131648D A GB 131648DA GB 131648 A GB131648 A GB 131648A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- resultant
- pressure
- levasseur
- deflexion
- 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.)
- Active
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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
131,648. Levasseur, P. March 16, 1918, [Convention date]. Screw propellers.-Comprises an aerial propeller in which the blades are inclined slightly in the direction of the resultant of the strains due to the centrifugal force and the air pressure on the blades, so that the said pressure may be wholly or partially eliminated by the resultant action of the centrifugal forces acting upon the parts of each blade, for the purpose of relieving the blades of any deflexion strain at their roots. Three modifications are shown in Figs. 1, 2, and 4, the method of connecting the blades to the hub being shown in Figs. 1 and 2.
Publications (1)
Publication Number | Publication Date |
---|---|
GB131648A true GB131648A (en) |
Family
ID=1725198
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB131648D Active GB131648A (en) |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB131648A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2451106A (en) * | 1944-04-22 | 1948-10-12 | United Aircraft Corp | Propeller blade construction |
US3851994A (en) * | 1972-01-20 | 1974-12-03 | Bbc Brown Boveri & Cie | Blading for axial flow turbo-machine |
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0
- GB GB131648D patent/GB131648A/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2451106A (en) * | 1944-04-22 | 1948-10-12 | United Aircraft Corp | Propeller blade construction |
US3851994A (en) * | 1972-01-20 | 1974-12-03 | Bbc Brown Boveri & Cie | Blading for axial flow turbo-machine |
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