Patent ID: 11858629
Assignee: TEXTRON INNOVATIONS INC.
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 0:
1. A wing apparatus for an aircraft, comprising:
a wing body configured to provide lift to an aircraft during flight;
a fowler flap apparatus comprising a fowler flap, a first attachment and a first deployer, the first attachment configured to couple the fowler flap to the wing body, and the first deployer configured to deploy the fowler flap in an aft direction from a stowed flap position to a deployed flap position in which the fowler flap is aft of the wing body; and
a sliding panel apparatus comprising a sliding panel, a second attachment, and a second deployer, the second attachment configured to couple the sliding panel to the wing body, and the second deployer configured to deploy the sliding panel in a forward direction from a stowed panel position to a deployed panel position in which the sliding panel is prone on top of the wing body.