FIELD: aircraft technology.
SUBSTANCE: invention relates to signaling devices that react to the formation of ice on the surface of aircraft. The noise-resistant optoelectronic icing detector contains a generator of rectangular pulse packs and control signals 1, an optical emitter power controller 2, an optical emitter 3, an optically transparent element of a section of the airframe’s aerodynamic surface exposed to icing 4, a photodetector 6, an optically transparent element of a section of the airframe’s aerodynamic surface exposed to icing 5, a photodetector 7, a comparator 8, a peak detector with closed input 9, a rectangular pulse generator 10, a logic element “AND” 11, a pulse counter 12, a pulse counter 13, a code comparator 14, an icing signal generation device 15 based on a signal from the comparator about the coincidence of the states of the counters.
EFFECT: increase in the noise immunity of the optoelectronic icing detector.
1 cl, 4 dwg
Title | Year | Author | Number |
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OPTOELECTRONIC ICE SIGNALING SYSTEM FOR AN UNMANNED AIRCRAFT | 2021 |
|
RU2758565C1 |
ICE DETECTOR | 2023 |
|
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|
RU2791724C1 |
ICING INDICATOR | 2014 |
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SIGNALLING DEVICE FOR ICING OVER BLADES OF ROTOR AGGREGATE | 2012 |
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RU2473972C1 |
ICING INDICATOR | 2013 |
|
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ICING INDICATOR | 2010 |
|
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HELICOPTER ROTOR BLADE ICING WARNING INDICATOR | 2012 |
|
RU2507125C2 |
OPTOELECTRONIC ICING INDICATOR | 2007 |
|
RU2332724C1 |
HELICOPTER ROTOR BLADE ICING WARNING INDICATOR | 2010 |
|
RU2446080C1 |
Authors
Dates
2022-10-28—Published
2021-12-21—Filed