GB696760A - Improvements in or relating to windings for rotors - Google Patents

Improvements in or relating to windings for rotors

Info

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
Application number
GB1305250A
Inventor
William Douglass Horsley
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CA Parsons and Co Ltd
Original Assignee
CA Parsons and Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by CA Parsons and Co Ltd filed Critical CA Parsons and Co Ltd
Priority to GB1305250A priority Critical patent/GB696760A/en
Publication of GB696760A publication Critical patent/GB696760A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K3/00Details of windings
    • H02K3/46Fastening of windings on the stator or rotor structure
    • H02K3/50Fastening of winding heads, equalising connectors, or connections thereto
    • H02K3/51Fastening 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.
GB1305250A 1950-05-24 1950-05-24 Improvements in or relating to windings for rotors Expired GB696760A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (9)

* Cited by examiner, † Cited by third party
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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