FIELD: aircraft engineering. SUBSTANCE: device has probe 1 with a flow parameter measuring system, a probe carrier in the form of a flying vehicle and a flexible link. The system has pressure head 5 with impact and static pressure difference sensors 6 and unit 7 for pressure head 5 with members for measuring its angular position in the form of potentiometers 8, 9 and 10 orientation down the flow. EFFECT: improved operational characteristics and measuring accuracy. 2 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
RU2029958C1 |
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| DEVICE FOR EXTENSION-RETRACTION OF TOWED OBJECT | 1995 |
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RU2015075C1 |
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|
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|
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| HELICOPTER OUTER CARGO SUSPENSION SYSTEM | 1992 |
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RU2015074C1 |
