FIELD: automatic control for industrial devices which supply liquid from chamber at constant pressure. SUBSTANCE: feedback detector 13, which controls pressure, is located at input of liquid user. Tank 8 is connected to users through turbine usage transducer 14 and valves 12-1, ..., 12- α. turbine usage transducer 14 and frequency-to-code converter 24 measure fuel usage per second. This value is used by calculation unit 25 which controls characteristics of usage control unit 2 in order to set gas usage constituent G
| Title | Year | Author | Number | 
|---|---|---|---|
| METHOD OF CONTROL OF LIQUID-PROPELLANT ROCKET ENGINE AND DEVICE FOR REALIZATION OF THIS METHOD | 1993 | 
									
  | 
                RU2085755C1 | 
| LIQUID VOLUME FLOW CALCULATING DEVICE | 1991 | 
									
  | 
                RU2012848C1 | 
| METHOD FOR STARTING LIQUID PROPELLANT ENGINES OF SECTIONAL ROCKET AND DEVICE FOR IMPLEMENTING THE SAME | 1994 | 
									
  | 
                RU2079690C1 | 
| PRESSURE REGULATOR | 0 | 
									
  | 
                SU1674075A1 | 
| CAPACITIVE DIFFERENTIAL TRANSMITTER SIGNAL DIGITIZER | 1999 | 
									
  | 
                RU2205446C2 | 
| DEVICE FOR WRITING AND READING MULTIPLE- CHANNEL DIGITAL INFORMATION | 1995 | 
									
  | 
                RU2107953C1 | 
| DEVICE FOR MEASUREMENT OF LIQUID PARAMETERS | 0 | 
									
  | 
                SU1830460A1 | 
| DEVICE FOR MONITORING AXIAL DISPLACEMENT OF SHAFT | 1996 | 
									
  | 
                RU2129212C1 | 
| DISPLACEMENT SPEED/CODE CONVERTER | 1990 | 
									
  | 
                RU2011293C1 | 
| DIRECTION FINDER | 1991 | 
									
  | 
                RU2073880C1 | 
Authors
Dates
1997-01-27—Published
1992-03-11—Filed