RU97101255A - TURBINE - Google Patents

TURBINE

Info

Publication number
RU97101255A
RU97101255A RU97101255/06A RU97101255A RU97101255A RU 97101255 A RU97101255 A RU 97101255A RU 97101255/06 A RU97101255/06 A RU 97101255/06A RU 97101255 A RU97101255 A RU 97101255A RU 97101255 A RU97101255 A RU 97101255A
Authority
RU
Russia
Prior art keywords
disk
channels
stator
rotor
cavity
Prior art date
Application number
RU97101255/06A
Other languages
Russian (ru)
Other versions
RU2142054C1 (en
Inventor
М.М. Лесковский
Original Assignee
М.М. Лесковский
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 М.М. Лесковский filed Critical М.М. Лесковский
Priority to RU97101255A priority Critical patent/RU2142054C1/en
Priority claimed from RU97101255A external-priority patent/RU2142054C1/en
Publication of RU97101255A publication Critical patent/RU97101255A/en
Application granted granted Critical
Publication of RU2142054C1 publication Critical patent/RU2142054C1/en

Links

Claims (1)

Турбина, состоящая из статора, рабочего колеса о каналами, диска с сопловыми канавками в диске, отводящей и подводящей трубы, расположенной в центре диска, отличающаяся тем, что в герметезированной полости статора расположен полый герметизированный ротор центрифуги, полости которого расположено рабочее колесо с каналами, расположенными около оси на расстоянии L-R, и часть статора в виде диска с рабочими каналами на диске и в диске каналы расположены по дуге L>R диска с входами каналов, расположенных на периферии диска, а выходы заходят за центр диска образуя вихревое движение теплоносителя в центральной полости диска, и тепловыделяющий элемент расположен в центре полости ротора, а подводящая труба расположена внутри отводящей, последняя расположена соосно с диском и ротором в котором осуществляется замкнутое тороиодапьно-вихревое движение теплоносителя относительно неподвижного диска.A turbine consisting of a stator, an impeller about the channels, a disk with nozzle grooves in the disk, an outlet and inlet pipe located in the center of the disk, characterized in that a hollow sealed centrifuge rotor is located in the sealed cavity of the stator, the cavities of which have an impeller with channels, located near the axis at a distance LR, and part of the stator in the form of a disk with working channels on the disk and in the disk, the channels are located along the arc L> R of the disk with the channel inputs located on the periphery of the disk, and the outputs go beyond the prices tr of the disk forming a vortex motion of the coolant in the central cavity of the disk, and the fuel element is located in the center of the rotor cavity, and the inlet pipe is located inside the outlet, the latter is located coaxially with the disk and the rotor in which the closed toroidal-vortex coolant movement relative to the stationary disk is carried out.
RU97101255A 1997-01-24 1997-01-24 Turbine RU2142054C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97101255A RU2142054C1 (en) 1997-01-24 1997-01-24 Turbine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU95102614 1995-03-03
RU97101255A RU2142054C1 (en) 1997-01-24 1997-01-24 Turbine

Publications (2)

Publication Number Publication Date
RU97101255A true RU97101255A (en) 1999-02-20
RU2142054C1 RU2142054C1 (en) 1999-11-27

Family

ID=20189395

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97101255A RU2142054C1 (en) 1997-01-24 1997-01-24 Turbine

Country Status (1)

Country Link
RU (1) RU2142054C1 (en)

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