RU94039948A - Axial three-stage compressor - Google Patents

Axial three-stage compressor

Info

Publication number
RU94039948A
RU94039948A RU94039948/06A RU94039948A RU94039948A RU 94039948 A RU94039948 A RU 94039948A RU 94039948/06 A RU94039948/06 A RU 94039948/06A RU 94039948 A RU94039948 A RU 94039948A RU 94039948 A RU94039948 A RU 94039948A
Authority
RU
Russia
Prior art keywords
rotor
thickness
compressor
vane
side planes
Prior art date
Application number
RU94039948/06A
Other languages
Russian (ru)
Other versions
RU2136974C1 (en
Inventor
И.И. Попков
Original Assignee
И.И. Попков
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.И. Попков filed Critical И.И. Попков
Priority to RU94039948A priority Critical patent/RU2136974C1/en
Publication of RU94039948A publication Critical patent/RU94039948A/en
Application granted granted Critical
Publication of RU2136974C1 publication Critical patent/RU2136974C1/en

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Abstract

FIELD: compressor engineering. SUBSTANCE: compressor has rotor with vanes. Each vane is inclined at an individual angle to the axis of rotation of the rotor. The length of each vane vary due to varying its guide portion within each sector into which the outer side of the rotor is separated to form air sucking spaces. The thickness of compression portions of each vane increases in the direction to their kicking out portions the thickness of which in turn is constant. The side planes and side planes of the adjacent vanes form slot passageways. EFFECT: simplified design.

Claims (1)

Изобретение относится к осевым многоступенчатым компрессорам. Цель изобретения - повышение создаваемого давления и упрощение конструкции компрессора. Компрессор содержит ротор с лопастями. Новым в конструкции является то, что каждая лопасть имеет составляющие части, направленные под разными углами к оси вращения ротора. Так же изменяется длина каждой лопасти за счет ее направляющей части в пределах каждого сектора, на которые разделена наружная поверхность ротора. Это способствует образованию воздухозаборных полостей. Толщина компрессионных частей каждой лопасти увеличивается в направлении к их сбрасывающим частям, толщина которых остается постоянной, а ее боковые плоскости образуют с боковыми плоскостями соседних лопастей щелевые каналы.The invention relates to axial multistage compressors. The purpose of the invention is to increase the generated pressure and simplify the design of the compressor. The compressor contains a rotor with blades. New in design is that each blade has component parts directed at different angles to the axis of rotation of the rotor. The length of each blade also changes due to its guide part within each sector into which the outer surface of the rotor is divided. This contributes to the formation of air intakes. The thickness of the compression parts of each blade increases toward their discharge parts, the thickness of which remains constant, and its side planes form slotted channels with the side planes of adjacent blades.
RU94039948A 1994-10-25 1994-10-25 Axial three-staged compressor RU2136974C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94039948A RU2136974C1 (en) 1994-10-25 1994-10-25 Axial three-staged compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94039948A RU2136974C1 (en) 1994-10-25 1994-10-25 Axial three-staged compressor

Publications (2)

Publication Number Publication Date
RU94039948A true RU94039948A (en) 1996-11-27
RU2136974C1 RU2136974C1 (en) 1999-09-10

Family

ID=20162068

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94039948A RU2136974C1 (en) 1994-10-25 1994-10-25 Axial three-staged compressor

Country Status (1)

Country Link
RU (1) RU2136974C1 (en)

Also Published As

Publication number Publication date
RU2136974C1 (en) 1999-09-10

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