SU1295838A1 - Paddle axial turbomachine - Google Patents

Paddle axial turbomachine

Info

Publication number
SU1295838A1
SU1295838A1 SU3908319/06A SU3908319A SU1295838A1 SU 1295838 A1 SU1295838 A1 SU 1295838A1 SU 3908319/06 A SU3908319/06 A SU 3908319/06A SU 3908319 A SU3908319 A SU 3908319A SU 1295838 A1 SU1295838 A1 SU 1295838A1
Authority
SU
USSR - Soviet Union
Prior art keywords
shortened
axial turbomachine
blades
blade
rounded
Prior art date
Application number
SU3908319/06A
Other languages
Russian (ru)
Inventor
З.Р. Гуревич
В.И. Тихонов
Original Assignee
З.Р. Гуревич
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 З.Р. Гуревич filed Critical З.Р. Гуревич
Priority to SU3908319/06A priority Critical patent/SU1295838A1/en
Application granted granted Critical
Publication of SU1295838A1 publication Critical patent/SU1295838A1/en

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1. Лопаточная решетка осевой турбомашины, содержащая расположенные между наружной и внутренней обечайками лопатки и размещенные между последними на внутренней стороне наружной и (или) на внешней стороне внутренней обечаек укороченные лопатки со скругленными входными кромками, отличающаяся тем, что, с целью уменьшения потерь, укороченные лопатки выполнены с переменной высотой, увеличивающейся от входа к выходу решетки.2. Решетка по п.1, отличающаяся тем, что торец каждой укороченной лопатки скруглен по форме ее входной кромки.1. A blade grate of an axial turbomachine, containing blades located between the outer and inner shells and placed between the latter on the inner side of the outer and / or on the outer side of the inner shells shortened blades with rounded inlet edges, characterized in that, in order to reduce losses, shortened the blades are made with a variable height, increasing from the entrance to the exit of the lattice. Lattice according to claim 1, characterized in that the end of each shortened blade is rounded in the shape of its input edge.

SU3908319/06A 1985-06-05 1985-06-05 Paddle axial turbomachine SU1295838A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3908319/06A SU1295838A1 (en) 1985-06-05 1985-06-05 Paddle axial turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3908319/06A SU1295838A1 (en) 1985-06-05 1985-06-05 Paddle axial turbomachine

Publications (1)

Publication Number Publication Date
SU1295838A1 true SU1295838A1 (en) 2006-01-27

Family

ID=60543007

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3908319/06A SU1295838A1 (en) 1985-06-05 1985-06-05 Paddle axial turbomachine

Country Status (1)

Country Link
SU (1) SU1295838A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU170008U1 (en) * 2016-06-27 2017-04-11 федеральное государственное бюджетное образовательное учреждение высшего образования "Ивановский государственный энергетический университет имени В.И. Ленина" (ИГЭУ) AXIAL TURBO MACHINE SHOVEL

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU170008U1 (en) * 2016-06-27 2017-04-11 федеральное государственное бюджетное образовательное учреждение высшего образования "Ивановский государственный энергетический университет имени В.И. Ленина" (ИГЭУ) AXIAL TURBO MACHINE SHOVEL

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