US2007081889A1PendingUtilityA1
Multi-stage friction vacuum pump
Est. expiryNov 13, 2023(expired)· nominal 20-yr term from priority
Inventors:Heinrich Engländer
F04D 19/046F04D 17/127F04D 17/168F04D 17/02
34
PatentIndex Score
0
Cited by
0
References
0
Claims
Abstract
A multi-stage vacuum pump includes at least one turbo-compressor stage ( 11 ) and is equipped with a circular compressor stage ( 33 ) on the pressure side of the turbo-compressor stage. The pump has small axial dimensions, enabling the compression to be increased without significantly increasing the space requirement.
Claims
exact text as granted — not AI-modified1 . A multi-stage friction vacuum pump comprising:
at least one axially compressing turbo-compressor stage with a rotor rotating about its axis and having rotor discs projecting between stationary stator discs; a radially compressing circular compressor stage arranged on the compressor side of the turbo-compressor stage, said circular compressor stage comprising a rotor having axially projecting rotor blades arranged on circular paths and a stator having axially projecting stator blades arranged on circular paths, the stator blades engaging in radial gaps between adjacent circular paths of rotor blades.
2 . The friction vacuum pump of claim 1 , wherein the rotor blades of the circular compressor stage are arranged on a rotor body of the turbo-compressor stage carrying the rotor discs.
3 . The friction vacuum pump of claim 1 , wherein the stator blades are arranged on a stator body of the turbo-compressor stage carrying the stator discs.
4 . The friction vacuum pump of claim 1 , as a multi-inlet pump, further including:
at least two axially spaced, serially compressing turbo-compressor stages between which an intermediate inlet is situated, and a circular compressor stage on the compressor side of the first turbo-compressor stage.
5 . The friction vacuum pump of claim 1 , as a multi-inlet pump, further including:
at least two axially spaced, serially compressing turbo-compressor stages between which an intermediate inlet is situated, and a circular compressor stage on the compressor side of the second turbo-compressor stage.
6 . The friction vacuum pump of claim 1 , wherein the circular compressor stage compresses radially inward.
7 . The friction vacuum pump of claim 1 , wherein in that the circular compressor stage is designed with at least two stages and alternately compresses one of radially inward and radially outward.
8 . The friction vacuum pump of claim 1 , wherein the rotor blades have an axial length that tapers in a direction of compression.Cited by (0)
No later patents cite this yet.
References (0)
No backward citations on record.