FIELD: measurement equipment.
SUBSTANCE: invention refers to measurement equipment and can be used in aviation and space technology. Obtaining temperature sensor and heat flow may be implemented directly on model surface of various degree of curvature without cockles and damage of integrity of the model and physical process of flowing on model surface and gas flow. Sensors thermocouples are manufactured from chromel-constantan film by method of cathode sputtering in vacuum. As insulating foil between the model and thermocouple, between thermocouples, chosen is aluminium oxide. Upper surface of thermocouple is protected from oxidation by heat resisting insulating foil with width of 0.80-0.1 mcm. Width of coating with thermocouple outputs is 0.3-0.4 mcm. Coatings with outputs are formed through masks (from metal or polyimide film) and by method of electrography by "pencil" voltage of 6-10 V.
EFFECT: increasing functional capabilities of temperature sensors and heat flow.
2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| PRESSURE AND TEMPERATURE-SENSITIVE ELEMENT | 1998 |
|
RU2145064C1 |
| CAPACITIVE PRESSURE SENSOR AND METHOD OF ITS MANUFACTURE | 1996 |
|
RU2099681C1 |
| METHOD TO PRODUCE HEAT-LOSS ANEMOMETER (VERSIONS) | 2013 |
|
RU2548612C2 |
| PYROELECTRIC PRESSURE TRANSDUCER AND METHOD FOR ITS ASSEMBLY | 1999 |
|
RU2157979C1 |
| CAPACITIVE PRESSURE SENSOR AND METHOD OF ITS MANUFACTURE | 1995 |
|
RU2099680C1 |
| MATRIX THIN-FILM TRANSDUCER | 1992 |
|
RU2063009C1 |
| CAPACITIVE INERTIAL PRESSURE SENSOR, METHOD OF ITS ASSEMBLY AND METHOD OF PRESSURE MEASURING | 2015 |
|
RU2589494C1 |
| DEVICE FOR PRESSURE AND TEMPERATURE MEASURING | 2015 |
|
RU2603446C1 |
| PRESSURE AND TEMPERATURE SENSITIVE ELEMENT | 1996 |
|
RU2110778C1 |
| PRESSURE, TEMPERATURE AND HEAT FLOW MEASURING DEVICE | 2011 |
|
RU2476842C1 |
