SU130100A1 - Turbine Rotor Winding - Google Patents
Turbine Rotor WindingInfo
- Publication number
- SU130100A1 SU130100A1 SU639090A SU639090A SU130100A1 SU 130100 A1 SU130100 A1 SU 130100A1 SU 639090 A SU639090 A SU 639090A SU 639090 A SU639090 A SU 639090A SU 130100 A1 SU130100 A1 SU 130100A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- winding
- turbine rotor
- rotor winding
- axial
- channels
- Prior art date
Links
Landscapes
- Windings For Motors And Generators (AREA)
Description
Насто щее изобретение относитс к обмоткам ротора турбогенератора с непос1)едственньгм ох/гаждением меди с-бмотки в местах входа газа.The present invention relates to windings of a rotor of a turbo-generator with an indirect effect of oh / copper deposition from a winding in places of gas inlet.
Предлагаема обмотка отличаетс от известных тем, что каждый из осевых каналов ротора сообщаетс с отдельным радиа.тьным каналом, по которому Подаетс охлаждающий газ.The proposed winding is different from the known ones in that each of the axial channels of the rotor is connected to a separate radio channel through which the cooling gas is supplied.
Такое вы1полнение обмотки позво.т ет уменьшить потери :npii выходе газа в осевые каналы.Such a winding makes it possible to reduce losses: npii gas outflow into axial channels.
На фиг. 1 :И 2 изображены схемы предлагаемой обмотки в двух вариантах «сполнени .FIG. 1: And 2 depicts the schemes of the proposed winding in two variants of “filling.
Обмотка ротора турбогенератора в месте входа в пее газа выполн етс таким образом, чтобы каждому осевому каналу / соответствовал радиальный канал 2, по которому газ проходит в осевой канал. Дл сокрангени длины входного участка обмотки возмол но через один радиальный каНа.т подавать газ в два осевых.The winding of the rotor of the turbogenerator at the point of entry into the gas stream is performed in such a way that each axial channel / corresponds to a radial channel 2 through which gas passes into the axial channel. To shorten the length of the input section of the winding, it is possible through one radial channel to feed gas into two axial ones.
И р е дм е т изобретени And the invention is
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU639090A SU130100A1 (en) | 1959-09-19 | 1959-09-19 | Turbine Rotor Winding |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU639090A SU130100A1 (en) | 1959-09-19 | 1959-09-19 | Turbine Rotor Winding |
Publications (1)
Publication Number | Publication Date |
---|---|
SU130100A1 true SU130100A1 (en) | 1959-11-30 |
Family
ID=48401231
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU639090A SU130100A1 (en) | 1959-09-19 | 1959-09-19 | Turbine Rotor Winding |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU130100A1 (en) |
-
1959
- 1959-09-19 SU SU639090A patent/SU130100A1/en active
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