GB696760A - Improvements in or relating to windings for rotors - Google Patents
Improvements in or relating to windings for rotorsInfo
- Publication number
- GB696760A GB696760A GB1305250A GB1305250A GB696760A GB 696760 A GB696760 A GB 696760A GB 1305250 A GB1305250 A GB 1305250A GB 1305250 A GB1305250 A GB 1305250A GB 696760 A GB696760 A GB 696760A
- Authority
- GB
- United Kingdom
- Prior art keywords
- slot
- bolts
- conductors
- turns
- coils
- 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
- H02K3/00—Details of windings
- H02K3/46—Fastening of windings on the stator or rotor structure
- H02K3/50—Fastening of winding heads, equalising connectors, or connections thereto
- H02K3/51—Fastening of winding heads, equalising connectors, or connections thereto applicable to rotors only
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Windings For Motors And Generators (AREA)
Abstract
696,760. Conductors for dynamo-electric machines. PARSONS & CO., Ltd., C. A. March 19, 1951 [May 24, 1950], No. 13052/50. Class 35. In order to reduce the temperature gradient of the slot of an alternator rotor the latter is wound with conductor strips having their flat surface substantially parallel and approximately equal in radial depth to the central radial plane of the slot. Fig. 1 shows a slot 1 accommodating a number of turns 6 of copper or aluminium strip arranged parallel to the radial plane of the slot. At the base of the slot there is a ventilating channel 5 and on top of the slot below the wedge 3 there is a damping winding 4. The turns 6 are separated by insulation 7. In a modification shown in Fig. 2, the conductors 6 are tapered in section to produce a wedging action at high speeds. In a further modification, the turns 6 are insulated in pairs and each pair is surrounded by a metal sheath 8, Fig. 3 (not shown) to dissipate heat. Fig. 4 shows how the turns 9 forming the winding are built up and joined at their end portions at 11. These joints are effected by welding, riveting, bolting or similar means. Fig. 5 shows how the ends of the coils are secured by insulated bolts 14 which pass through the coils, the bolts also secure the end supporting ring 13 against the coil retaining ring 12. Alternatively, additional separate bolts 16 are employed to brace the coil ends. Fig. 9 shows the bolts 14 arranged to pass underneath the coils 9 and not through them and therefore the conductors are suitably cut at their inner part to accommodate the bolts 14. The conductors can also be partly aluminium and partly copper. The end coils may be modified in section so as to reduce their width and lessen the weight of the windings supported by the rotor coil retaining ring.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1305250A GB696760A (en) | 1950-05-24 | 1950-05-24 | Improvements in or relating to windings for rotors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1305250A GB696760A (en) | 1950-05-24 | 1950-05-24 | Improvements in or relating to windings for rotors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB696760A true GB696760A (en) | 1953-09-09 |
Family
ID=10015905
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1305250A Expired GB696760A (en) | 1950-05-24 | 1950-05-24 | Improvements in or relating to windings for rotors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB696760A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008062633A2 (en) * | 2006-11-24 | 2008-05-29 | Toyota Jidosha Kabushiki Kaisha | Motor stator and motor stator manufacturing method |
US20160099624A1 (en) * | 2014-10-07 | 2016-04-07 | Hamilton Sundstrand Corporation | End turn support and cooling fixture |
US10063116B2 (en) | 2014-10-07 | 2018-08-28 | Hamilton Sundstrand Corporation | Lamination clamping structure |
EP3709483A1 (en) * | 2019-03-11 | 2020-09-16 | Ge Aviation Systems Llc, Inc. | Rotor assembly |
-
1950
- 1950-05-24 GB GB1305250A patent/GB696760A/en not_active Expired
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008062633A2 (en) * | 2006-11-24 | 2008-05-29 | Toyota Jidosha Kabushiki Kaisha | Motor stator and motor stator manufacturing method |
WO2008062633A3 (en) * | 2006-11-24 | 2008-07-31 | Toyota Motor Co Ltd | Motor stator and motor stator manufacturing method |
KR100985339B1 (en) * | 2006-11-24 | 2010-10-04 | 도요타지도샤가부시키가이샤 | Motor stator and motor stator manufacturing method |
US20160099624A1 (en) * | 2014-10-07 | 2016-04-07 | Hamilton Sundstrand Corporation | End turn support and cooling fixture |
US9812917B2 (en) * | 2014-10-07 | 2017-11-07 | Hamilton Sundstrand Corporation | End turn support and cooling fixture |
US10063116B2 (en) | 2014-10-07 | 2018-08-28 | Hamilton Sundstrand Corporation | Lamination clamping structure |
EP3709483A1 (en) * | 2019-03-11 | 2020-09-16 | Ge Aviation Systems Llc, Inc. | Rotor assembly |
CN111682692A (en) * | 2019-03-11 | 2020-09-18 | 通用电气航空系统有限责任公司 | Rotor assembly |
US11381142B2 (en) | 2019-03-11 | 2022-07-05 | Ge Aviation Systems Llc | Rotor assembly |
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