GB838868A - Screw propeller - Google Patents
Screw propellerInfo
- Publication number
- GB838868A GB838868A GB32265/58A GB3226558A GB838868A GB 838868 A GB838868 A GB 838868A GB 32265/58 A GB32265/58 A GB 32265/58A GB 3226558 A GB3226558 A GB 3226558A GB 838868 A GB838868 A GB 838868A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- outer end
- edge
- nearest
- rear edge
- 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
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H1/00—Propulsive elements directly acting on water
- B63H1/02—Propulsive elements directly acting on water of rotary type
- B63H1/12—Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
- B63H1/14—Propellers
- B63H1/26—Blades
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Investigating Or Analysing Biological Materials (AREA)
Abstract
838,868. Screw propellers. VAGHI, J. Oct. 9, 1958 [Feb. 12, 1958], No. 32265/58. Class 114. In a propeller having a hut 10 from which blades extend ir radial direction, each blade has. a straight leading edge 11 and a rear edge 12 including convexly concavely curved continuous portions 13, 14 extending between the hub and the outer end of the blade, concave de pressions 15, 21 being formed ir the blade and (depression 15 extending from the rear edge 12 across the rear surface of the blade at that portion (13 nearest the outer end of the blade and (depression 21) across the forward surface at another portion (14) of the blade, saic depressions gradually decreasing in depth from the rear edge 12 to adjacent said leading edge 11, said portion 13 nearest the outer end of the blade as well as said other portion 14 of the blade being formed with a convex ridge 17 and 23 respectively extending from the rear edge 12 across the blade and decreasing in height to adjacent the straight edge 11, the convex ridge 17 being formed in the forward surface of said portion 13 nearest the outer end of the blade and (convex ridge 23) in said rear surface of said other portion 14, said blades being feathered so as to be inclined to a plane at right angles to the axis of rotation.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US838868XA | 1958-02-12 | 1958-02-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB838868A true GB838868A (en) | 1960-06-22 |
Family
ID=22181303
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32265/58A Expired GB838868A (en) | 1958-02-12 | 1958-10-09 | Screw propeller |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB838868A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4886421A (en) * | 1984-01-09 | 1989-12-12 | Wind Feather, United Science Asc. | Wind turbine air foil |
WO2020077520A1 (en) * | 2018-10-16 | 2020-04-23 | Hewlett-Packard Development Company, L.P. | Impellers |
-
1958
- 1958-10-09 GB GB32265/58A patent/GB838868A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4886421A (en) * | 1984-01-09 | 1989-12-12 | Wind Feather, United Science Asc. | Wind turbine air foil |
WO2020077520A1 (en) * | 2018-10-16 | 2020-04-23 | Hewlett-Packard Development Company, L.P. | Impellers |
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