公开(公告)号：US20180297691A1

公开(公告)日：2018-10-18

申请号：US15949232

申请日：2018-04-10

Applicant: Textron Aviation Inc.

Inventor： Stephen M. Eddy ,  Jeremy Phillip Taylor ,  Steven G. Hagerott ,  Philippe A. Ciholas

IPC: B64C13/12 ,  B64C13/50 ,  B64C13/28 ,  B64C13/18 ,  B64C13/04 ,  B64C13/10

Abstract: An interconnected flight controller for an aircraft includes a mechanical linkage connecting a pilot interface with a copilot interface. When an input is provided to either of the pilot or copilot interfaces, coordinated motion is provided between them of a proportional magnitude and direction. A mechanical-disconnect element within the mechanical linkage is adapted to actuate mechanical decoupling between the pilot interface and the copilot interface. One or more sensors is coupled to the mechanical linkage to sense inputs and communicate the inputs to a fly-by-wire flight controller. An autopilot servo is coupled to the mechanical linkage for providing autopilot control or feedback and a force-feedback subsystem is connected to the mechanical linkage to simulate and apply an opposing force of aircraft control surfaces to the pilot interface and the copilot interface.

公开(公告)号：US11014648B2

公开(公告)日：2021-05-25

申请号：US15949232

申请日：2018-04-10

Applicant: Textron Aviation Inc.

Inventor： Stephen M. Eddy ,  Jeremy Phillip Taylor ,  Steven G. Hagerott ,  Philippe A. Ciholas

IPC: B64C13/12 ,  B64C13/50 ,  B64C13/10 ,  B64C13/18 ,  B64C13/04 ,  B64C13/28 ,  B64C13/16

Abstract: An interconnected flight controller for an aircraft includes a mechanical linkage connecting a pilot interface with a copilot interface. When an input is provided to either of the pilot or copilot interfaces, coordinated motion is provided between them of a proportional magnitude and direction. A mechanical-disconnect element within the mechanical linkage is adapted to actuate mechanical decoupling between the pilot interface and the copilot interface. One or more sensors is coupled to the mechanical linkage to sense inputs and communicate the inputs to a fly-by-wire flight controller. An autopilot servo is coupled to the mechanical linkage for providing autopilot control or feedback and a force-feedback subsystem is connected to the mechanical linkage to simulate and apply an opposing force of aircraft control surfaces to the pilot interface and the copilot interface.