FIELD: measurement technology. SUBSTANCE: sensor has restoring element 1 in the form of hollow truncated cone with flange 2 close to base and hub 3 at vertex. Sensor is attached to engine 4 with flange 2 and with hub 3 it is made fast to lathe or airplane engines. Deformation of action of thrust and torque is taken by resistance strain gauges 6, 7 mounted along generating lines of internal surface of truncated cone. EFFECT: increased reliability of measurements. 2 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MAGNETIC-WAVE FRICTION VARIABLE-SPEED DRIVE (DESIGN VERSIONS) | 1995 |
|
RU2115046C1 |
| MAGNETOWAVE FRICTIONAL SPEED REGULATOR (VERSIONS) | 1997 |
|
RU2138709C1 |
| METHOD AND DEVICE FOR SILENCING JET NOISE OF ENGINES | 1994 |
|
RU2079686C1 |
| MULTICHANNEL AEROMETRIC PROBE | 1993 |
|
RU2037157C1 |
| METHOD FOR MAKING AXIALLY SYMMETRICAL PRODUCTS BY ROLLING OUT | 1995 |
|
RU2085321C1 |
| DEVICE FOR MEASURING FORCES ACTING ON WHEEL | 2000 |
|
RU2181194C2 |
| PISTON SEAL FOR INTERNAL COMBUSTION ENGINE | 1991 |
|
RU2022146C1 |
| ENGINE JET SILENCER | 1994 |
|
RU2079687C1 |
| METHOD OF DIAGNOSTICS OF TECHNICAL STATE OF AIRCRAFT GAS TURBINE JET ENGINES | 1996 |
|
RU2118810C1 |
| METHOD FOR MEASURING OF THREE-DIMENSIONAL DISTRIBUTION OF PHYSICAL FIELD | 1993 |
|
RU2082100C1 |
