THRUST-REVERSAL SYSTEM FOR AN AIRCRAFT AND AIRCRAFT INCLUDING SUCH A SYSTEM

    公开(公告)号:US20230366364A1

    公开(公告)日:2023-11-16

    申请号:US18246395

    申请日:2021-10-13

    CPC classification number: F02K1/763 F02K1/766 F05D2270/52 F05D2270/62

    Abstract: A thrust-reversal cowling selectively movable between a retracted position for leaving unchanged the thrust of an aircraft turbine engine, and a deployed position for reversing the thrust of the turbine engine; an electrical actuator of the cowling; a local control module to receive commands from a global control module to control the electrical actuator to move the cowling, these commands including a retraction command and a deployment command; and a connection between the global control module and the local control module for conveying at least one analogue signal. The local control module identifies one among a plurality of predefined ranges of values, in which each analogue signal is located at a given instant, each command being associated with one or more value ranges; and determining the received command as being that associated with the identified range or ranges of values.

Patent Agency Ranking