FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to fueling unit taper gage. The latter consists of ball joint with casing with aerodynamic cone. A number of through rectangular slots are made on ball joint tapered section. Strain gages are fitted on webs between said slots and connected in measuring circuit with its output connected to memory unit. Casing of the latter is fitted on sleeve that enters said ball joint.
EFFECT: possibility to measure forces acting on fuel taper gage in flight.
3 dwg
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