FIELD: removal of gases from working main lines of complicated hydraulic drives and various liquid (fuel, oil, etc) systems; applicable in mechanical engineering, aviation, transport, etc. SUBSTANCE: method includes pumping through main lines of working fluid with drainage through drainage unit of liquid system and identification of undissolved gas in system. Pumping through is effected in pulse regime with frequency from 0 to 100 Hz and excessive average pressure of at least 0.1 MPa in system. Working fluid is used in the form of degassed fluid. As gas removal fluid proceeds, pulse frequency is increased. With noticeable retardation of process, coefficient of pulse filling is changed to allow displacement of zone of maximum pulsation amplitude to highly throttled channels of liquid system with gas plugs. In the course of gas removal provision is made for continuous repeated use of drained working fluid, and also quantitative identification of gas in system. EFFECT: higher efficiency. 6 cl
Title | Year | Author | Number |
---|---|---|---|
LIQUID SYSTEM SERVICEABILITY PRESERVATION METHOD | 2001 |
|
RU2201538C1 |
PROCESS TESTING TIGHTNESS OF ARTICLES | 2001 |
|
RU2204118C2 |
METHOD OF FILLING SPACECRAFT TEMPERATURE CONTROL SYSTEM WITH LIQUID HEAT-TRANSFER AGENT AND DEVICE FOR REALIZATION OF THIS METHOD | 2005 |
|
RU2300492C1 |
DEVICE FOR CONTROL OVER LIQUID-PROPELLANT ROCKET ENGINE PERFORMANCE | 1991 |
|
RU2133866C1 |
PYROVALVE | 1998 |
|
RU2142085C1 |
AVIATION COMPLEX (MODIFICATIONS) | 2003 |
|
RU2242404C2 |
DEVICE FOR HEAT-TRANSFER FLUID FILLING OF SPACECRAFT THERMOREGULATING SYSTEM | 2007 |
|
RU2339552C1 |
POWER PLANT LIQUID COOLING SYSTEM AND EXPANSION TANK USED WITH THIS SYSTEM (DESIGN VERSIONS OF TANK) | 2000 |
|
RU2170830C1 |
NEAT ENGINE AND METHOD OF ITS OPERATION | 1991 |
|
RU2067192C1 |
METHOD OF CHANGING OPERATING CONDITIONS OF LIQUID PROPELLANT ROCKET ENGINE AND ENGINE FOR IMPLEMENTATION OF THIS METHOD | 1998 |
|
RU2125177C1 |
Authors
Dates
2002-09-10—Published
2001-02-20—Filed