Aircraft flight control surface actuation system communication architecture
First Claim
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1. An aircraft flight control system, comprising:
- a plurality of independent communication channels;
a flight control avionics channel operable to supply flight control surface position commands representative of a commanded flight control surface position via each of the independent communication channels;
a plurality of actuators, each actuator adapted to couple to an aircraft flight control surface, each actuator coupled to receive actuator position commands and operable, upon receipt thereof, to move to an actuator position corresponding to the commanded flight control surface position; and
a plurality of remote electronic control units disposed remote from the flight control avionics channel, each remote electronic control unit associated with one of the plurality of actuators, and each remote electronic control unit;
(i) coupled to receive the flight control surface position commands supplied from each of the independent communication channels and operable, in response thereto, to supply the actuator position commands to its associated actuator, and (ii) coupled to receive one or more signals representative of operability of one or more of the plurality of actuators and one or more other remote electronic control units and operable, in response thereto, to determine to whether one or more of the plurality of actuators are operating improperly and whether one or more of the other remote electronic control units are operating improperly.
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Abstract
A flight control surface actuation system includes a plurality of smart actuators to move aircraft flight control surfaces between extended and retracted positions. The system includes a high availability network between the flight control avionics and the smart actuators, and between each of the smart actuators. The system configuration allows network nodes associated with each smart actuator to monitor and control one another, under higher level control of the aircraft flight control avionics, to provide multiple levels of health monitoring, control, and shutdown capability.
82 Citations
21 Claims
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1. An aircraft flight control system, comprising:
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a plurality of independent communication channels;
a flight control avionics channel operable to supply flight control surface position commands representative of a commanded flight control surface position via each of the independent communication channels;
a plurality of actuators, each actuator adapted to couple to an aircraft flight control surface, each actuator coupled to receive actuator position commands and operable, upon receipt thereof, to move to an actuator position corresponding to the commanded flight control surface position; and
a plurality of remote electronic control units disposed remote from the flight control avionics channel, each remote electronic control unit associated with one of the plurality of actuators, and each remote electronic control unit;
(i) coupled to receive the flight control surface position commands supplied from each of the independent communication channels and operable, in response thereto, to supply the actuator position commands to its associated actuator, and (ii) coupled to receive one or more signals representative of operability of one or more of the plurality of actuators and one or more other remote electronic control units and operable, in response thereto, to determine to whether one or more of the plurality of actuators are operating improperly and whether one or more of the other remote electronic control units are operating improperly. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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16. An aircraft flight control system, comprising:
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a plurality of independent communication channels;
a flight control avionics channel operable to supply flight control surface position commands representative of a commanded flight control surface position via each of the independent communication channels;
a plurality of communication hubs, each communication hub having a plurality of ports, each communication hub coupled to receive the flight control surface position commands supplied from one of the independent communication channels and operable, upon receipt thereof, to supply the received flight control surface position commands;
a plurality of remote electronic control units, each remote electronic control unit coupled to one of the communication hubs to receive the flight control surface position commands supplied therefrom, each of the remote electronic control units operable, upon receipt of the flight surface position commands, to supply actuator position commands; and
a plurality of actuators, each actuator adapted to couple to an aircraft flight control surface, each actuator coupled to receive the actuator position commands from one of the remote electronic control units and operable, upon receipt thereof, to move to an actuator position corresponding to the commanded flight control surface position. - View Dependent Claims (17, 18, 19, 20)
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21. An aircraft flight control system, comprising:
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a plurality of independent communication channels;
a flight control avionic channel operable to supply flight control surface position commands representative of a commanded flight control surface position via each of the independent communication channels;
a plurality of actuators, each actuator adapted to couple to an aircraft flight control surface, each actuator coupled to receive actuator position commands and operable, upon receipt thereof, to move to an actuator position corresponding to the commanded flight control surface position;
a plurality of communication hubs, each communication hub having a plurality of ports, and each communication hub coupled to receive the flight control surface position commands supplied from one of the independent communication channels and operable, upon receipt thereof, to supply the received flight control surface position commands; and
a plurality of remote electronic control units disposed remote from the flight control avionics channel, each remote electronic control unit associated with one of the plurality of actuators, and each remote electronic control unit;
(i) coupled to one of the communication hubs to receive the flight control surface position commands supplied therefrom and operable, in response thereto, to supply the actuator position commands to its associated actuator, and (ii) coupled to receive one or more signals representative of operability of one or more of the plurality of actuators and one or more other remote electronic control units and operable, in response thereto, to determine to whether one or more of the plurality of actuators are operating improperly and whether one or more of the other remote electronic control units are operating improperly.
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Specification