Method and device for controlling a wingtip of an aircraft
An aircraft and controller technology, applied in the field of aircraft folding wingtips, can solve the problem of not being able to provide enough
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0020] Disclosed herein are example devices and methods that, prior to transitioning the wingtip from an extended position to a folded position, by moving one or more control surfaces on the wing to create more or less air load on the wingtip Multiple vantage points to control the air loads on the aircraft wingtips. Examples disclosed herein enable the use of smaller, lighter wingtip actuation systems, thereby reducing the weight of the wingtip and reducing the space required to accommodate the wingtip actuation system in the wing of an aircraft. As a result, the wings can be thinner and lighter and thus result in more efficient flight.
[0021] Before turning to detailed aspects of the disclosed aircraft control systems and methods, a brief discussion of folding wingtips is provided. It is generally known that longer, lighter and / or thinner wings are more aerodynamically efficient than shorter, heavier wings. Likewise, a higher aspect ratio wing produces more efficient flig...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


