Communications: electrical – Condition responsive indicating system – Specific condition
Patent
1984-08-03
1987-02-24
Swann, III, Glen R.
Communications: electrical
Condition responsive indicating system
Specific condition
250392, 250390, 324 713, G08B 2100
Patent
active
046460683
ABSTRACT:
A layer of hydrogenous material, such as ice which may accumulate on an outer airplane surface, is monitored according to neutron moderation by the layer.
A source of fast neutrons and a detector of slow neutrons are mounted on one side of a mounting plate which may be the skin of an airplane. As a layer of ice or other hydrogenous material accumulates on the outer surface of the mounting plate, some of the fast neutrons collide with hydrogen nuclei therein to lose energy and be scattered into the slow neutron detector where each detected slow neutron generates an electrical pulse. The electrical pulses are transformed into a signal which corresponds to the amount of hydrogenous material per unit area.
REFERENCES:
patent: 2967937 (1961-01-01), McKay
patent: 3621714 (1971-11-01), Puccinelli
patent: 3838281 (1974-09-01), Dean et al.
patent: 4039809 (1977-08-01), Bailey
Skala Stephen F.
Swann III Glen R.
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