FIELD: engines and pumps.
SUBSTANCE: invention relates to measurements of plasma engine parameters. Claimed device comprises resilient vertical thread of suspension, propulsor angular displacement recorder, magnetic deflecting system with supply circuit and switch. Note here that it is provided with platform suspended from said resilient vertical thread of suspension aligned with vertical rotary axis and weight dispended therefrom. Sleeve is rigidly fixed for resilient thread to pass there through. Note here that the switch is connected in deflecting magnetic system supply circuit.
EFFECT: higher accuracy of measurements.
4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE TO MEASURE TORQUE AND TRANSVERSE FORCE AT AIRCRAFT | 1973 |
|
SU1841107A1 |
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SU569989A1 |
| 0 |
|
SU524977A1 | |
| 0 |
|
SU318112A1 |
