FIELD: aviation. SUBSTANCE: invention relates to aviation instrumentation and to control of unsteady temperature of gas flows. Device measuring temperature of gas has unit 1 of thermoelectric temperature transducers, two adders 2, 17, three dividers 3, 7, 12, two differentiators 4, 10, two multipliers 5, 13, transducer 6 of full pressure downstream from compressor, subtractor 8, transducer 9 of rotational speed of rotor of turbocompressor, transducer 11 of gas pressure downstream from turbine, squarer 14, two functional converters 15, 16. EFFECT: enhanced operational reliability and stability. 2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR DETERMINING REDUCED R.P.M. OF GAS-TURBINE ROTOR | 0 |
|
SU734743A1 |
| DEVICE FOR MEASUREMENT OF PHYSICAL QUANTITIES | 1994 |
|
RU2082099C1 |
| COMPREHENSIVE DEVICE FOR MONITORING PARAMETERS | 0 |
|
SU1520482A1 |
| GAS TEMPERATURE METER OF GAS TURBINE ENGINE | 2016 |
|
RU2617221C1 |
| TURBOCOMPRESSOR STALL-AND-SURGE PROTECTION DEVICE | 2003 |
|
RU2254499C1 |
| GAS-TURBINE ENGINE AUTOMATIC CONTROL SYSTEM | 2000 |
|
RU2172857C1 |
| METHOD OF AND DEVICE TO PROTECT COMPRESSOR FROM STALL AND SURGE | 2003 |
|
RU2254498C1 |
| POWER PLANT AUTOMATIC CONTROL SYSTEM | 2001 |
|
RU2204044C2 |
| DEVICE TO CONTROL INVERTER WITH PULSE-WIDTH MODULATION | 1999 |
|
RU2159002C1 |
| INSTRUMENT TO MEASURE A PHYSICAL QUALITY | 0 |
|
SU1691685A1 |
