| 摘要 |
A system for controlling at least two variable-geometry equipments (10, 110) of a turbomachine, the first equipment (10) being a variable pitch stator blade stage of a compressor of a first core moving between a closed position at idle speed and an open position at high speed, the second equipment (110) being at least one bleed valve of a compressor of a second core moving between an open position at idle speed and a closed position at high speed. The actuator operates over a portion of its travel a first branch (34, 341) of an angle transmission member (26) which actuates the first equipment (10) and leaves this branch at rest on an abutment (64) over the rest of its travel; moreover it operates the second equipment (110) via a sliding junction member (120) arranging a free travel in the actuation of said second equipment.
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