SU671745A3 - Turbomachine - Google Patents

Turbomachine

Info

Publication number
SU671745A3
SU671745A3 SU772493452A SU2493452A SU671745A3 SU 671745 A3 SU671745 A3 SU 671745A3 SU 772493452 A SU772493452 A SU 772493452A SU 2493452 A SU2493452 A SU 2493452A SU 671745 A3 SU671745 A3 SU 671745A3
Authority
SU
USSR - Soviet Union
Prior art keywords
turbomachine
blades
radial
edges
protrusions
Prior art date
Application number
SU772493452A
Other languages
Russian (ru)
Inventor
Гундльах Владыслав
Порохницки Ежы
Прывэр Ежы
Карэвич Богуслав
Потапчык Анджэй
Зеленов Кшыштоф
Original Assignee
Политехника Лудзка(Инопредприятие)
Заклады Мэханичнэ Им.Гэн.Кароля Сверчевскего(Инопредприятие)
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 Политехника Лудзка(Инопредприятие), Заклады Мэханичнэ Им.Гэн.Кароля Сверчевскего(Инопредприятие) filed Critical Политехника Лудзка(Инопредприятие)
Priority to SU772493452A priority Critical patent/SU671745A3/en
Application granted granted Critical
Publication of SU671745A3 publication Critical patent/SU671745A3/en

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

(54) ТУРБОМАШИНА(54) TURBO MACHINE

между радиальными выступами 5 и кромками лопаток 2. Сила, прижим.ающа  выступы 5 к кромкам лопаток 2, зависит от скорости вращени  ротора 1. По достижении максимальных оборотов ротора зазор 8 между выступами 5 и кромками лопаток 2 выбираетс  полностью.between the radial protrusions 5 and the edges of the blades 2. The force that presses the protrusions 5 to the edges of the blades 2 depends on the speed of rotation of the rotor 1. When the maximum rotor speed is reached, the gap 8 between the projections 5 and the edges of the blades 2 is completely selected.

Выполнение на бандажах осевых лопаток радиальных выступов с утолщени ми на концах, обращенна  к радиальным лопаткам поверхность которых образует с кромками последних увеличивающийс  к периферии зазор, обеспечивает надежность работы турбомащины за счет демпфировани  колебаний радиальных лопаток и способствует увеличению экономичности посредством исключени  радиальных зазоров в рабочем колесе.The axial vanes on the bandages perform radial protrusions with thickening at the ends facing the radial blades of which, with the edges of the blades, an increase in the periphery of the gap ensures the operation of the turbo-belt due to the damping of oscillations of the radial blades and contributes to increased efficiency by eliminating the radial gaps in the impeller.

Claims (1)

1. Авторское свидетельство 1. Copyright certificate СССР №200711, кл. F 04D 29/30, 1966.USSR №200711, cl. F 04 D 29/30, 1966. LL Vuz. гVuz. g
SU772493452A 1977-06-09 1977-06-09 Turbomachine SU671745A3 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU772493452A SU671745A3 (en) 1977-06-09 1977-06-09 Turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU772493452A SU671745A3 (en) 1977-06-09 1977-06-09 Turbomachine

Publications (1)

Publication Number Publication Date
SU671745A3 true SU671745A3 (en) 1979-06-30

Family

ID=20712132

Family Applications (1)

Application Number Title Priority Date Filing Date
SU772493452A SU671745A3 (en) 1977-06-09 1977-06-09 Turbomachine

Country Status (1)

Country Link
SU (1) SU671745A3 (en)

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