Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
HIGH-ROTATION-SPEED OIL-GAS SEPARATOR FOR TURBINE ENGINE
Document Type and Number:
WIPO Patent Application WO/2022/100150
Kind Code:
A1
Abstract:
A high-rotation-speed oil-gas separator for a turbine engine, the oil-gas separator comprising a hollow rotating shaft (77), wherein the upper portion of the rotating shaft (77) is provided with an oil input cavity assembly; the upper middle portion of the rotating shaft (77) is provided with a separation cavity assembly; and the lower portion of the rotating shaft (77) is provided with a driving mechanism. The separation cavity assembly comprises: a separator cavity (12) located on the periphery of the upper middle portion of the rotating shaft (77); a partition layer, which is located in the middle portion of the rotating shaft (77) in the separator cavity (12); a first centrifugal disc (19) located on the upper portion of the partition layer; a second centrifugal disc (20) located on the lower portion of the partition layer; a plurality of first through holes (21) located on the periphery of the first centrifugal disc (19); a plurality of second through holes (22) located on the periphery of the second centrifugal disc (20); an oil guide groove (17) that is located in the separator cavity (12) and is in communication with the plurality of first through holes (21); and an oil outlet (12a) that is located in the separator cavity (12) and is in communication with the oil guide groove (17). A gas outlet (7a) is provided at the bottom portion of the rotating shaft (77). The high-rotation-speed oil-gas separator is self-powered for driving, is not affected by the working condition of an engine, has high separation efficiency and can satisfy the volume and weight of a high-rotation-speed turbine engine.

More Like This:
Inventors:
LI JIYONG (CN)
XU WANG (CN)
LI TAO (CN)
LI FANG (CN)
MA YANG (CN)
CHEN LIANG (CN)
Application Number:
PCT/CN2021/108592
Publication Date:
May 19, 2022
Filing Date:
July 27, 2021
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
SICHUAN AEROSPACE ZHONGTIAN POWER EQUIPMENT CO LTD (CN)
International Classes:
F01D25/18; F02C7/06
Foreign References:
CN112392563A2021-02-23
US20040226442A12004-11-18
CN109322747A2019-02-12
CN104303279A2015-01-21
CN1300240A2001-06-20
CN1390158A2003-01-08
Attorney, Agent or Firm:
CHENG DU HONG YI TIAN CHENG INTELLECTUAL PROPERTY AGENCY CO., LTD (CN)
Download PDF: