Tip gap control systems with active blade tips
AssigneeTextron Innovations Inc.
InventorsJonathan Andrew Knoll, George Matthew Thompson, Nicholas Ralph Carlson
Life of this patent
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AssigneeTextron Innovations Inc.
InventorsJonathan Andrew Knoll, George Matthew Thompson, Nicholas Ralph Carlson
Estimating the term…
A tip gap control system for a ducted aircraft includes a flight control computer including a blade length control module configured to generate a blade tip actuator command and a proprotor system in data communication with the flight control computer. The proprotor system includes a duct and proprotor blades surrounded by the duct. Each of the proprotor blades includes an active blade tip movable into various positions including a retracted position and an extended position. The tip gap control system also includes one or more actuators coupled to the active blade tips. The one or more actuators move the active blade tips between the various positions based on the blade tip actuator command, thereby controlling a tip gap between the proprotor blades and the duct.
A tip gap monitoring and control system for a ducted aircraft having a vertical takeoff and landing flight mode and a forward flight mode, the tip gap monitoring and control system comprising:
A rotorcraft having a vertical takeoff and landing flight mode and a forward flight mode, the rotorcraft comprising:
A method for controlling a tip gap for a ducted aircraft having a vertical takeoff and landing flight mode and a forward flight mode, the method comprising:
Dependencies are inferred from the claim text.