Aeronautics and astronautics – Aircraft structure – Ice prevention
Patent
1994-03-22
1996-08-20
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft structure
Ice prevention
B64D 1516
Patent
active
055471501
ABSTRACT:
A deicer for attachment to an airfoil substructure includes a segmented outer shell, with adjacent segments being decoupled from one another utilizing elastomeric decoupling members. The outer edges of the outer periphery shell segments are likewise decoupled from the airfoil structure utilizing elastomeric decoupling members. Each segment of the deicer is deflected by a respective deflection means which are provided energy from a controller.
REFERENCES:
patent: 2432669 (1947-12-01), Kliever
patent: 4613102 (1986-09-01), Kageorge
patent: 5129598 (1992-07-01), Adams et al.
patent: 5356096 (1994-10-01), Rauckhorst et al.
Adams Lowell J.
Leffel Kevin L.
Tenison Gary V.
Weisend, Jr. Norbert A.
Barefoot Galen L.
Romanchik Richard A.
The B.F. Goodrich Company
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