GB967841A - Improvements in fluid moving rotors - Google Patents
Improvements in fluid moving rotorsInfo
- Publication number
- GB967841A GB967841A GB18062A GB18062A GB967841A GB 967841 A GB967841 A GB 967841A GB 18062 A GB18062 A GB 18062A GB 18062 A GB18062 A GB 18062A GB 967841 A GB967841 A GB 967841A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- axially
- air
- jan
- draws
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D1/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D1/02—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
-
- 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
- B64C11/001—Shrouded propellers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Abstract
967,841. Self-propelled missiles. W. F. DARLING. Jan. 2, 1962 [Jan. 3, 1961], No. 180/62. Heading F3A. [Also in Divisions B7 and F1] A rotor which may be used for missile propulsion comprises two or more scoops 11 each closed at one end and joined to a shaft 12. Rotation of the rotor in the direction of the arrow, Fig. 1, causes air which enters the openings 14 to be expelled axially under pressure at the open ends 15. Rotation in the opposite direction causes air to be drawn in axially at the open end 15, and expelled through the openings 14. Fig. 6 shows a rotating missile having rotors 24 and 25 disposed forward and aft. The rotor 24 draws in air axially and passes it out circumferentially to reduce drag. The rotor 25 draws in air circumferentially and expels it axially to provide a thrust.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU6/61A AU246738B2 (en) | 1961-01-03 | Improvements in fluid moving rotors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB967841A true GB967841A (en) | 1964-08-26 |
Family
ID=3690908
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18062A Expired GB967841A (en) | 1961-01-03 | 1962-01-02 | Improvements in fluid moving rotors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB967841A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2153982A (en) * | 1984-02-02 | 1985-08-29 | Dynamit Nobel Ag | Flight body |
GB2314384A (en) * | 1996-06-18 | 1997-12-24 | Lin Solas Yun Jin | Motorboat Propeller |
GB2412948A (en) * | 2004-04-08 | 2005-10-12 | Alfred Learmonth | Wind or water-driven generator |
CN101737089B (en) * | 2009-12-15 | 2012-09-19 | 浙江工业大学 | Bidirectional blade for ocean power generation turbine |
-
1962
- 1962-01-02 GB GB18062A patent/GB967841A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2153982A (en) * | 1984-02-02 | 1985-08-29 | Dynamit Nobel Ag | Flight body |
GB2314384A (en) * | 1996-06-18 | 1997-12-24 | Lin Solas Yun Jin | Motorboat Propeller |
GB2412948A (en) * | 2004-04-08 | 2005-10-12 | Alfred Learmonth | Wind or water-driven generator |
GB2412948B (en) * | 2004-04-08 | 2007-02-28 | Alfred Learmonth | Wind or water motor |
CN101737089B (en) * | 2009-12-15 | 2012-09-19 | 浙江工业大学 | Bidirectional blade for ocean power generation turbine |
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