GB614348A - Improvements in or relating to electric motors - Google Patents
Improvements in or relating to electric motorsInfo
- Publication number
- GB614348A GB614348A GB2074746A GB2074746A GB614348A GB 614348 A GB614348 A GB 614348A GB 2074746 A GB2074746 A GB 2074746A GB 2074746 A GB2074746 A GB 2074746A GB 614348 A GB614348 A GB 614348A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spindle
- rotor
- hollow shaft
- cavity
- partly
- 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
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/14—Structural association with mechanical loads, e.g. with hand-held machine tools or fans
- H02K7/16—Structural association with mechanical loads, e.g. with hand-held machine tools or fans for operation above the critical speed of vibration of the rotating parts
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Spinning Or Twisting Of Yarns (AREA)
Abstract
614,348. Universal joints. GENERAL ELECTRIC CO., Ltd., and JACOBY, H. C. E. July 11, 1946, Nos. 20747/46 and 13112/47. [Class 80 (ii)] [Also in Group XXXV] A relatively long spindle driving a spinning bowl or the like passes into the hollow rotor shaft of the motor and is flexibly connected thereto in an enlarged cavity on the hollow shaft between the rotor and its lower bearing, a flexible disc or the equivalent being connected both to the spindle and the cavity wall. As shown, the spindle 10 is supported in the hollow shaft 4 partly by the flexible washers 8 in the cavity 7 and partly by a rubber sleeve 17 or a resilient metal member engaging both shafts, or there may be a ball on the spindle engaged in a socket on the side of the hollow shaft near the centre of the rotor. The resilient metal coupling member may be formed by cutting sections out of a disc (Figs. 6-9, not shown), or be shaped as in Figs. 4, 5 or 10. Specification 369,642, [Group XXXV], is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2074746A GB614348A (en) | 1946-07-11 | 1946-07-11 | Improvements in or relating to electric motors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2074746A GB614348A (en) | 1946-07-11 | 1946-07-11 | Improvements in or relating to electric motors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB614348A true GB614348A (en) | 1948-12-14 |
Family
ID=10150977
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2074746A Expired GB614348A (en) | 1946-07-11 | 1946-07-11 | Improvements in or relating to electric motors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB614348A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE955528C (en) * | 1953-06-13 | 1957-01-03 | Siemens Ag | Electric motor for driving centrifuges |
EP0742634A2 (en) * | 1995-05-12 | 1996-11-13 | Capstone Turbine Corporation | Compound shaft |
DE102005058661B4 (en) | 2005-12-07 | 2018-11-29 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Coupling for compensating an axial offset |
-
1946
- 1946-07-11 GB GB2074746A patent/GB614348A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE955528C (en) * | 1953-06-13 | 1957-01-03 | Siemens Ag | Electric motor for driving centrifuges |
EP0742634A2 (en) * | 1995-05-12 | 1996-11-13 | Capstone Turbine Corporation | Compound shaft |
EP0742634A3 (en) * | 1995-05-12 | 1998-10-28 | Capstone Turbine Corporation | Compound shaft |
DE102005058661B4 (en) | 2005-12-07 | 2018-11-29 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Coupling for compensating an axial offset |
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