Conclusion
Aircraft Icing : Airborne Measurements for Certification Purposes
Article REF: TRP4002 V1
Conclusion
Aircraft Icing : Airborne Measurements for Certification Purposes

Author : Guy FEBVRE

Publication date: March 10, 2015 | Lire en français

Logo Techniques de l'Ingenieur You do not have access to this resource.
Request your free trial access! Free trial

Already subscribed?

4. Conclusion

As part of aircraft certification for icing conditions, in-flight tests are carried out to prove that the various de-icing systems are correctly sized and operate correctly. The aircraft used for these tests is fitted with measuring instruments designed to measure the water content and median volume diameter of the cloud conditions encountered.

Two families of instruments are currently used systematically, an airborne laser granulometer (of the CDP type) and a hot-wire sensor (such as the LWC 200 or WCM-2000). These instruments can explore water contents of up to several grams per cubic meter, and document the dimensional spectrum of drops between 2 and 50 μm. This information is currently sufficient to comply with current regulations.

These instruments, particularly the airborne laser granulometers, were developed for atmospheric physics...

You do not have access to this resource.
Logo Techniques de l'Ingenieur

Exclusive to subscribers. 97% yet to be discovered!

You do not have access to this resource. Click here to request your free trial access!

Already subscribed?


Article included in this offer

"Aerospace systems"

( 77 articles )

Complete knowledge base

Updated and enriched with articles validated by our scientific committees

Services

A set of exclusive tools to complement the resources

View offer details