Aeronautics and astronautics – Aircraft structure – Ice prevention
Patent
1997-04-16
1999-05-18
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft structure
Ice prevention
244134D, B64D15/12
Patent
active
059043229
ABSTRACT:
A deicer comprises a skin heating means immediately subjacent an outer skin overlying an apex of a leading edge, and a skin deflection means immediately subjacent the outer skin chordwise aft of the apex. The skin heating means prevents the formation of ice over the apex and the skin deflection means deflects the outer skin to expulse ice formed chordwise aft of the apex.
REFERENCES:
patent: 5314145 (1994-05-01), Rauckhorst, III
patent: 5356096 (1994-10-01), Rauckhorst, III et al.
patent: 5547150 (1996-08-01), Adams et al.
patent: 5609314 (1997-03-01), Rauckhorst, III et al.
patent: 5657952 (1997-08-01), Goldberg
Giamati Michael J.
Sweet David B.
Wilson, Jr. Tommy M.
Barefoot Galen L.
Romanchik Richard A.
The BFGoodrich Company
LandOfFree
Hybrid deicer does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Hybrid deicer, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Hybrid deicer will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1754441