Aeronautics and astronautics – Aircraft structure – Ice prevention
Patent
1985-10-04
1987-06-23
Peters, Jr., Joseph F.
Aeronautics and astronautics
Aircraft structure
Ice prevention
244207, 244134R, 138104, 138114, B64D 1504
Patent
active
046747141
ABSTRACT:
The duct (16) which delivers hot air (F) to the inside surface of the leading edge of a turbo-fan inlet cowl, for de-icing of the leading edge (11), is made double-walled (16,21) in order to safeguard from overheating the materials from which the cowl is constructed in the event of rupture of the duct. Preferably the flow of hot air in the outer duct blows open a hinged door (26) in the skin (10) of the cowl to provide a visual indication of the rupture of the inner duct. The outer duct can be made narrow enough to maintain working pressure in the inner duct after rupture.
REFERENCES:
patent: 327996 (1885-10-01), Brick
patent: 2636666 (1953-04-01), Lombard
patent: 2668596 (1954-02-01), Elliott
patent: 2820601 (1958-01-01), Crawford
patent: 3749336 (1973-07-01), Christensen et al.
patent: 3830290 (1974-08-01), Thamasett et al.
patent: 3917193 (1975-11-01), Runnels
patent: 3933327 (1976-01-01), Rosenthal et al.
patent: 4482114 (1984-11-01), Waters et al.
Arnold Michael J.
Cole Derek
Corl Rodney
Peters Jr. Joseph F.
Short Brothers PLC
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