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SU1510471A1 - Turbo Cooler Support Damper - Google Patents

Turbo Cooler Support Damper

Info

Publication number
SU1510471A1
SU1510471A1 SU4120189/27A SU4120189A SU1510471A1 SU 1510471 A1 SU1510471 A1 SU 1510471A1 SU 4120189/27 A SU4120189/27 A SU 4120189/27A SU 4120189 A SU4120189 A SU 4120189A SU 1510471 A1 SU1510471 A1 SU 1510471A1
Authority
SU
USSR - Soviet Union
Prior art keywords
order
turbo
cooler support
support damper
turbo cooler
Prior art date
Application number
SU4120189/27A
Other languages
Russian (ru)
Inventor
И.С. Сапрыкин
В.Г. Иванников
И.Н. Антипенко
Original Assignee
И.С. Сапрыкин
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 И.С. Сапрыкин filed Critical И.С. Сапрыкин
Priority to SU4120189/27A priority Critical patent/SU1510471A1/en
Application granted granted Critical
Publication of SU1510471A1 publication Critical patent/SU1510471A1/en

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  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1. Демпфирующее средство опоры турбохолодильника, содержащее упругое кольцо с выступами, расположенными равномерно на его наружной и внутренней поверхностях с симметричным смещением один относительно другого, отличающееся тем, что, с целью повышения демпфирующей способности, кольцо выполнено составным в виде двух концентрично расположенных элементов, зафиксированных один относительно другого и выполненных с разрезом по образующей, смещенным диаметрально один относительно другого, при этом элемент фиксации размещен в месте одного из разрезов.2. Средство по п.1, отличающееся тем, что, с целью упрощения технологии изготовления, кольца выполнены свернутыми из ленты с выступами.1. The damping means of the support of a turbo-cooler, containing an elastic ring with protrusions located uniformly on its outer and inner surfaces with symmetrical displacement relative to each other, characterized in that, in order to increase the damping capacity, the ring is made composite in the form of two concentrically arranged elements fixed one relative to the other and made with a cut along a generatrix that is diametrically offset from one another, with the fixation element placed in the place of one of cuts. The tool according to claim 1, characterized in that, in order to simplify the manufacturing technology, the rings are rolled up from the tape with the projections.

SU4120189/27A 1986-07-04 1986-07-04 Turbo Cooler Support Damper SU1510471A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4120189/27A SU1510471A1 (en) 1986-07-04 1986-07-04 Turbo Cooler Support Damper

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4120189/27A SU1510471A1 (en) 1986-07-04 1986-07-04 Turbo Cooler Support Damper

Publications (1)

Publication Number Publication Date
SU1510471A1 true SU1510471A1 (en) 2006-07-20

Family

ID=60528301

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4120189/27A SU1510471A1 (en) 1986-07-04 1986-07-04 Turbo Cooler Support Damper

Country Status (1)

Country Link
SU (1) SU1510471A1 (en)

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