SU1623350A1 - Turbine - Google Patents

Turbine

Info

Publication number
SU1623350A1
SU1623350A1 SU4633993/06A SU4633993A SU1623350A1 SU 1623350 A1 SU1623350 A1 SU 1623350A1 SU 4633993/06 A SU4633993/06 A SU 4633993/06A SU 4633993 A SU4633993 A SU 4633993A SU 1623350 A1 SU1623350 A1 SU 1623350A1
Authority
SU
USSR - Soviet Union
Prior art keywords
housing
turbine
washers
annular grooves
disks
Prior art date
Application number
SU4633993/06A
Other languages
Russian (ru)
Inventor
С.В. Иванников
Original Assignee
С.В. Иванников
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 С.В. Иванников filed Critical С.В. Иванников
Priority to SU4633993/06A priority Critical patent/SU1623350A1/en
Application granted granted Critical
Publication of SU1623350A1 publication Critical patent/SU1623350A1/en

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)

Abstract

1. Турбоагрегат, содержащий установленный в корпусе ротор с дисками рабочих колес турбины и нагнетателя на газодинамических подшипниках с лепестковыми элементами, имеющими антифрикционное покрытие, отличающийся тем, что, с целью увеличения ресурса работы, в корпусе со стороны дисков выполнены кольцевые проточки, а турбоагрегат дополнительно содержит шайбы, которые установлены между подшипниками и корпусом на внутренних поверхностях кольцевых проточек с возможностью поворота и осевого перемещения относительно корпуса посредством шпилек, закрепленных в основании шайб и пропущенных через прорези в корпусе.2. Турбоагрегат по п.1, отличающийся тем, что на внутренних поверхностях кольцевых проточек выполнена разнонаправленная резьба, а шпильки соединены между собой муфтой с возможностью одновременного поворота шайб и их перемещения навстречу друг другу.1. A turbine unit containing a rotor mounted in a housing with disks of turbine impellers and a supercharger on gas-dynamic bearings with petal elements having an anti-friction coating, characterized in that, in order to increase the service life, annular grooves are made in the housing from the disks, and the turbine additionally contains washers that are installed between the bearings and the housing on the inner surfaces of the annular grooves with the possibility of rotation and axial movement relative to the housing by means of a spy lek, fixed in the base of the washers and passed through the slots in the housing.2. Turbine unit according to claim 1, characterized in that multidirectional threads are made on the inner surfaces of the annular grooves, and the studs are interconnected by a coupling with the possibility of simultaneous rotation of the washers and their movement towards each other.

SU4633993/06A 1989-01-09 1989-01-09 Turbine SU1623350A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4633993/06A SU1623350A1 (en) 1989-01-09 1989-01-09 Turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4633993/06A SU1623350A1 (en) 1989-01-09 1989-01-09 Turbine

Publications (1)

Publication Number Publication Date
SU1623350A1 true SU1623350A1 (en) 2006-10-20

Family

ID=60531426

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4633993/06A SU1623350A1 (en) 1989-01-09 1989-01-09 Turbine

Country Status (1)

Country Link
SU (1) SU1623350A1 (en)

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