FIELD: automatic control systems for different objects, namely for controlling gas turbine engines of airplanes.
SUBSTANCE: system includes two shaping units, normalizing unit, two units for testing pickups and frequency values, storage unit, two units for conversion and analysis, two unit for forming orders, control order outputting unit, unit for monitoring control orders and calculating unit. And in addition such system includes nine units for receiving-transmitting successive code and unit for controlling single signals.
EFFECT: enhanced safety of flights of airplane due to high functional reliability of system and certainty of output control orders provided by enlarged automatic control of system operation.
7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DATA STORAGE INFORMATION MEASURING SYSTEM OF AIRCRAFT POWER PLANT | 2004 |
|
RU2280774C2 |
| DATA STORAGE DISPLAY SYSTEM OF AIRCRAFT MULTIPLE ENGINE POWER PLANT | 2004 |
|
RU2280775C2 |
| SYSTEM TO CONTROL, CHECK AND RECORD PARAMETERS OF GAS-TURBINE ENGINE | 2005 |
|
RU2293196C1 |
| INFORMATION MEASUREMENT STORAGE SYSTEM FOR FLYING VEHICLE POWER PLANT | 2004 |
|
RU2267629C1 |
| SYSTEM FOR CONTROLLING PARAMETERS OF MULTI-FUNCTIONAL SYSTEMS | 2004 |
|
RU2267804C1 |
| GAS-TURBINE ENGINE CONTROL AND PARAMETER MONITORING SYSTEM | 2005 |
|
RU2295646C1 |
| SHAFT ANGULAR SPEED INDICATOR | 0 |
|
SU597968A1 |
| GAS-TURBINE ENGINE CONTROL SYSTEM | 0 |
|
SU726360A1 |
| DEVICE FOR MONITORING OIL PRESSURE DROP IN GAS-TURBINE ENGINE | 0 |
|
SU665115A1 |
| VEHICLE AND REAL PROPERTY SECURITY PROTECTION SYSTEM | 2008 |
|
RU2345914C1 |
