FIELD: precision instrumentation.
SUBSTANCE: invention is related to devices for measuring parameters of movement of an aircraft and can be used in manufacturing of pendulum compensation accelerometers designed to measure linear accelerations. A through annular slot is formed in the support ring, dividing the support ring into an inner and an outer one, moreover, the pads combined into one whole in the place of the formed elastic suspensions and located symmetrically along the longitudinal axis of the sensing element are formed on the inner side of the outer support ring. Above and below the pads in the support ring, internal through slots are made, teeth are formed on the outer side of the outer support ring opposite the pads, and external through slots are formed on the support ring above and below the teeth.
EFFECT: improved measurement accuracy.
1 cl, 2 dwg
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Authors
Dates
2023-05-17—Published
2022-12-29—Filed