Home pageSite mapContacts
Home page


Products
       
Visual Ice indicator / detector

 

 

  Water drop model
  Tube model
  Visual Ice Detector
 

Ice is the most dangerous natural element affecting the security of commercial carriers. As soon as the presence of ice is detected, adapted flight procedures - switch on deicing system, increasing engine power, exit auto-pilot mode, etc. - must be promptly performed.

Therefore, it is critical that the crew's decision-making process be supported by easily available and reliable information about ice build-up.

If ice detection is performed on the latest aircraft generation by using Electronics Sensors, authorities require that Visual Icing Indicator (Ice Cue) be installed. As a result of recent accidents, this recommendation has been restated by FAA.
It is to be noted that such indicators - propeller cone, windshield wipers, wings edge, thin metal plate - are often not lighted and cannot be used at night without an external dedicated spotlight and are positioned behind and far from the cockpit.
These devices do conform to authorities recommendations, but they are troublesome and creates unnecessary workload to the crew, especially during critical flight phases such as landing. More importantly, their legibility is often not reliable.

 

To address the foregoing concerns, a new concept of Lighted Icing Indicator has been developed by Aerospatiale and Madelec Aero engineers, based on the followings attributes :

Designed and positioned to always be the first point where ice build up.

The length of the aerodynamic shape is designed in order that the extremity (1) is outside of the boundary layer (2). A socket (3) allows the mounting on the aircraft.

Dimensioned to be installed in the crew's direct field of view.

The indicator is perfectly legible by both pilot and co-pilot. Ice build-up is immediately, continuously and easily monitored by a simple glance out the windshield.

Internally lighted to enable their use during night flights.

The "probe" (1) is lighted by an internal source (2). Thus the ice build up on the probe masks the light source and ice accumulation is easily noticed by the crew.

The addition of an internal heating resistance allows to convert the Ice Indicator into an Ice Detector.

  Copyright © Madelec Aero - All rights reserved.