GB1077220A - D.c. induction pump - Google Patents
D.c. induction pumpInfo
- Publication number
- GB1077220A GB1077220A GB3667364A GB3667364A GB1077220A GB 1077220 A GB1077220 A GB 1077220A GB 3667364 A GB3667364 A GB 3667364A GB 3667364 A GB3667364 A GB 3667364A GB 1077220 A GB1077220 A GB 1077220A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- magnetic material
- sleeve
- space
- conduits
- 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
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K44/00—Machines in which the dynamo-electric interaction between a plasma or flow of conductive liquid or of fluid-borne conductive or magnetic particles and a coil system or magnetic field converts energy of mass flow into electrical energy or vice versa
- H02K44/02—Electrodynamic pumps
- H02K44/06—Induction pumps
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1,077,220. Pumps operating by electromagnetic interaction with fluids. UNITED AIRCRAFT CORPORATION. Sept. 8, 1964, No. 36673/64. Heading H2A. A D.C. induction pump, for pumping a number of independent conductive liquid circuits, comprises a rotor 12 of magnetic material having polar projections and a stator comprising wound cores 32, which project from longitudinally extending bars 30 formed integrally with radially extending parts 28, and have their inner ends joined by annular sleeve 36 of magnetic material which surrounds the rotor. The fluid conduits 42, 44 are located in the space between the rotor and inner surface of sleeve 36 and are thermally insulated from the magnetic material by insulation 38, 46. The conduits are run in pairs each occupying half the annular space and are embedded in a sleeve 40 of conducting material, e.g. silver. In operation, for use in a space vehicle, rotor 12 is driven by a turbine and each fluid conduit is connected to a segment of a radiator.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3667364A GB1077220A (en) | 1964-09-08 | 1964-09-08 | D.c. induction pump |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3667364A GB1077220A (en) | 1964-09-08 | 1964-09-08 | D.c. induction pump |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1077220A true GB1077220A (en) | 1967-07-26 |
Family
ID=10390254
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3667364A Expired GB1077220A (en) | 1964-09-08 | 1964-09-08 | D.c. induction pump |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1077220A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114640233A (en) * | 2022-05-09 | 2022-06-17 | 浙江大学 | Electromagnetic pump |
-
1964
- 1964-09-08 GB GB3667364A patent/GB1077220A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114640233A (en) * | 2022-05-09 | 2022-06-17 | 浙江大学 | Electromagnetic pump |
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