SU130100A1 - Turbine Rotor Winding - Google Patents

Turbine Rotor Winding

Info

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
Application number
SU639090A
Other languages
Russian (ru)
Inventor
Г.А. Чебыкин
Original Assignee
Г.А. Чебыкин
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 Г.А. Чебыкин filed Critical Г.А. Чебыкин
Priority to SU639090A priority Critical patent/SU130100A1/en
Application granted granted Critical
Publication of SU130100A1 publication Critical patent/SU130100A1/en

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  • 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)

1.Обмотка ротора турбогенератора с пепосредствеиным охлаждением меди в месте входа газа, о т ; и ч а ю щ а   с   тем, что, с целью уменьщени  потерь напора при входе в осевые каналы, каждый из них сообщаетс  с отдельным радиальным каналом, по которому охлаждаюн:ий газ проходит в соответствующий ему осевой канал.1. Winding of the rotor of the turbogenerator with copper cooling at the point of gas inlet, о t; And so that, in order to reduce head losses at the entrance to the axial channels, each of them communicates with a separate radial channel through which the cooling gas passes into the corresponding axial channel. 2.Обмотка по п. 1, от л и ч а ю щ а   с   тем, что, с целью сокращени  длины входного участка, с каждым из радиальных каналов сообН1аютс  два осевых.2. The winding of claim 1, from l and h and with that, in order to reduce the length of the input section, two axial channels are connected with each of the radial channels. . . Выход газаGas outlet
SU639090A 1959-09-19 1959-09-19 Turbine Rotor Winding SU130100A1 (en)

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)

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