FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering, in particular, to calibration devices used for calibration of force-measuring systems of test benches of small-size gas turbine engines (SGTE). Calibration device comprises bellows-type force-setting device (1), adjusting unit (2), transmitting force from bellows (1) pressure through metal ball (3) to setting sensor (4), force-measuring sensor (5), beam (6) (rigid structure of U-type), transmitting force through movable frame (7) of force-measuring machine to force-measuring sensor (5), which is installed on fixed frame (8) of force-measuring machine, adjusting unit (11) located between movable frame (7) and force-measuring sensor (5), nozzle (10), through which air is supplied from the bench system to bellows-type force-setting device (1), weighing converters (9) with digital indicators and polished element (12) of movable frame (7).
EFFECT: higher accuracy of SGTE thrust measurement during its testing, simplified calibration procedure of the force-measuring machine.
5 cl, 1 dwg
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Authors
Dates
2024-05-17—Published
2024-01-10—Filed