专利内容由知识产权出版社提供
专利名称：ANTI-ICING SYSTEM AND AIRCRAFT发明人：Gento Ichikawa,Yoichi Uefuji,Toshiyuki
Ishida,Masatoshi Morishita,Kazuhiro Kawai
申请号：US15420465申请日：20170131
公开号：US20170233084A1公开日：20170817
专利附图：
摘要：An anti-icing system according to the present invention blows heated air to acurved inner surface of a main wing of an aircraft. The anti-icing system includes: a piccolotube that includes a flow path through which the heated air flows in a longitudinal
direction from a rear end to a front end, and a plurality of ejection holes provided alongthe longitudinal direction to make the flow path communicate with an outside; and anengine that supplies the heated air toward the piccolo tube. The heated air ejected fromthe ejection holes of the piccolo tube is ejected toward an upper limit position and alower limit position of an outside airflow stagnation point that are virtually formed on themain wing.
申请人：MITSUBISHI AIRCRAFT CORPORATION
地址：Aichi JP
国籍：JP
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