To provide methods and apparatus for detecting icing conditions and/or ice formation on an aircraft in a more reliable manner and/or under a wider array of atmospheric conditions.SOLUTION: A method comprises disposing an ice detector 100 on an exterior surface of an aircraft, the ice detector comprising a probe surface 110 and a pyroelectric material layer 120 disposed on at least a portion of the probe surface. The method further comprises generating a charge on a surface of the pyroelectric material layer to increase the local freezing point of water on the surface of the pyroelectric material layer.SELECTED DRAWING: Figure 8
【課題】より確実に、及び/又は、より広範囲の大気条件下において、航空機の着氷状況及び/又は氷の形成を検出するための方法及び装置を提供する。【解決手段】航空機の外面に氷検出器100を設け、氷検出器は、プローブ表面110と、プローブ表面の少なくとも一部に設けられた焦電材料層120とを含む。焦電材料層の表面に電荷を形成することによって、焦電材料層の表面における水の局所的凝固点を上昇させることを更に含む。【選択図】図8
METHODS AND APPARATUS FOR DETECTING ICE FORMATION ON AIRCRAFT
航空機における氷の形成を検出するための方法及び装置
2019-04-18
Patent
Electronic Resource
Japanese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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