Invention Grant
US08590834B1 Aircraft control surface actuation system with helical actuation path
有权
具有螺旋驱动路径的飞机控制面驱动系统
- Patent Title: Aircraft control surface actuation system with helical actuation path
- Patent Title (中): 具有螺旋驱动路径的飞机控制面驱动系统
-
Application No.: US13295187Application Date: 2011-11-14
-
Publication No.: US08590834B1Publication Date: 2013-11-26
- Inventor: Paul E. Nelson
- Applicant: Paul E. Nelson
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agency: Walters & Wasylyna LLC
- Main IPC: B64C3/50
- IPC: B64C3/50
Abstract:
An aircraft control surface actuation system including a wing member and an aircraft control surface hingedly connected to the wing member along a pivot axis, wherein the aircraft control surface is configured to axially move along the pivot axis when the aircraft control surface pivots relative to the wing member about the pivot axis.
Information query
