Flight Testing a Liquid Ice Protection System on a Single-Engine Airplane Crew Systems Consultants, Yellow Springs, OH

Format:

Conference/Event

Author/Creator:

Newman, Richard L., author.

Conference Name:

General Aviation Aircraft Meeting and Exposition (1985-04-16 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1985

Summary:

AbstractA fluid depressant ice protection system has been installed on a Cessna 206 airplane. The system exudes an ethylene glycol solution over the leading edges of the wings, empennage, and lift struts. A slinger ring is used to distribute fluid to the propeller. The windshield is de-iced with a glycol spraybar. The system adds about thirty pounds to the empty weight of the airplane.Installation of ice protection equipment on a fixed-gear, single-engine airplane presents some unique instrumentation problems since probes must avoid the residual glycol spray from the propeller. Satisfactory anti-icing performance has been demonstrated within the FAR 25, Appendix C continuous maximum and intermittent maximum envelopes during flights in natural icing conditions

Notes:

Vendor supplied data

Publisher Number:

850923

Access Restriction:

Restricted for use by site license