| 摘要 |
A wake vortex visualizer for an aircraft having a selfcontained device that is installed within the wing tip to emit a smoke-like trail from the wing tip automatically by the use of simple ball check valve connected between an orifice on the wing tip and a tank of vapor forming fluid during takeoff and landing of the aircraft such that other following aircraft may see and avoid the vortex generated by said aircraft during takeoff and landing.
|
