SYSTEMS AND METHODS FOR PROVIDING DIFFERENTIAL MOTION TO WING HIGH LIFT DEVICE
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Abstract
Systems and methods for providing differential motion to wing high lift devices are disclosed. A system in accordance with one embodiment of the invention includes a wing having a leading edge, a trailing edge, a first deployable lift device with a first spanwise location, and a second deployable lift device with a second spanwise location different than the first. The wing system can further include a drive system having a drive link operatively coupleable to both the first and second deployable lift devices, and a control system operatively coupled to the drive system. The control system can have a first configuration for which the drive link is operatively coupled to the first and second deployable lift devices, and activation of at least a portion of the drive link moves the first and second deployable lift devices together. In a second configuration, the drive link is operatively coupled to at least the first deployable lift device and operatively decoupled from the second deployable lift device, so that actuation of at least a portion of the drive link moves the first deployable lift device relative to the second deployable lift device.
102 Citations
82 Claims
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1-67. -67. (canceled)
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68. An aircraft wing system, comprising:
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a wing having a leading edge and a trailing edge; a first deployable lift device having a first spanwise location and being movable relative to the wing from a stowed position to at least one first deployed position; a second deployable lift device having a second spanwise location different than the first and being movable relative to the wing from a stowed position to at least one second deployed position; a drive system that includes; a first motor; a first motor brake coupled to the first motor to selectively inhibit the first motor; a second motor; a second motor brake coupled to the second motor to selectively inhibit the second motor; and a drive link that includes a mechanical shaft, wherein the first and second motors are individually coupleable to the mechanical shaft, and wherein the drive link is connected to the first deployable lift device; a differential having a single power input, the single power input being connected to the mechanical shaft, the differential further having an output connected to the second deployable lift device; a differential brake coupled to the differential; a lift device brake coupled to the differential; and a controller connected to the drive system, the differential, the differential brake and the lift device brake, the controller being programmed with instructions that, when executed; connect the first and second deployable lift devices to the first motor via the drive link and engage the differential brake to move the first and second deployable lift devices together; and disconnect the first and second deployable lift devices from the first motor, connect the first deployable lift device to the second motor via the drive link, and engage the lift device brake to move the first deployable lift device relative to the second deployable lift device. - View Dependent Claims (69, 70, 71, 72)
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73. An aircraft wing system, comprising:
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a wing having a leading edge and a trailing edge; a first deployable lift device having a first spanwise location and being movable relative to the wing from a stowed position to at least one first deployed position; a second deployable lift device having a second spanwise location different than the first and being movable relative to the wing from a stowed position to at least one second deployed position; a drive system that includes; a first motor; a second motor; and a drive link, wherein the first and second motors are individually coupleable to the drive link, and wherein the drive link is connected to the first deployable lift device; a differential having a single power input, the single power input being connected to the drive link, the differential further having an output connected to the second deployable lift device; and a controller connected to the drive system and the differential, the controller being programmed with instructions that, when executed; connect the first and second deployable lift devices to the first motor via the drive link and the differential to move the first and second deployable lift devices together; and disconnect the first and second deployable lift devices from the first motor, prevent motion of the second deployable lift device at the differential, and connect the first deployable lift device to the second motor via the drive link to move the first deployable lift device relative to the second deployable lift device. - View Dependent Claims (74, 75, 76)
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77. A method for operating an aircraft wing, comprising:
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rotating a drive link with a first motor; moving a first deployable lift device with the first motor via the drive link, the first deployable lift device having a first spanwise location along the wing; receiving power from the first motor via the drive link at a single power input of a differential; placing the differential in a first configuration to drive both the first deployable lift device and a second deployable lift device together, the second deployable lift device having a second spanwise location different than the first; changing the configuration of the differential from the first configuration to a second configuration; rotating the drive link with a second motor; receiving power from the second motor via the drive link at the single power input of the differential; and moving the first deployable lift device relative to the second deployable lift device via the second motor while the differential has the second configuration. - View Dependent Claims (78, 79, 80, 81, 82)
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Specification