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Patent Searching and Data


Title:
TURBO VACUUM PUMP
Document Type and Number:
Japanese Patent JPS6355396
Kind Code:
A
Abstract:

PURPOSE: To permit exhaust in a wide vacuum range, by using an axial flow blade as a first exhaust element, a mixed flow blade as a second exhaust element of a suction stage and a swirl flow blade as a third exhaust element on an exhaust side.

CONSTITUTION: A rotor impeller 4 of an axial flow blade is provided on an outside surface of an upper stage of a rotor 1 and rotor impellers of mixing flow blades comprising a plurality of dynamic blade grooves disposed in a circumferential direction are provided with its exhaust side. A swirl flow blade 9 is provided on an outside circumference of a second rotor 2. With the arrangement, performance of exhaust elements such as an axial flow blade, a mixing flow blade or the like disposed on an outside circumference of a bell-shaped rotor can be effected sufficiently, whereby a single pump can exhaust gas in a range covering an atmospheric pressure to an ultra high vacuum pressure.


Inventors:
OKAWADA TAKESHI
MATSUBARA KATSUMI
MASE MASAHIRO
UEDA SHINJIRO
AWATA YOSHIHISA
NAKAMORI KAZUAKI
Application Number:
JP19642786A
Publication Date:
March 09, 1988
Filing Date:
August 21, 1986
Export Citation:
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Assignee:
HITACHI LTD
International Classes:
F04D19/04; F04D23/00; (IPC1-7): F04D19/04; F04D23/00
Attorney, Agent or Firm:
Tatsuyuki Unuma