发明名称 AIRCRAFT DE-ICING AND RECOVERY SYSTEM
摘要 A system (12) for collecting and recovering de-icing fluid (16) that is sprayed onto an aircraft (10). The de-icing system (12) includes a mat (20) that is assembled onto the approaching ramp of a runway (26). The de-icing mat (20) has a plurality of channels (28) that collect and direct the de-icing fluid (16) to the outer edges of the mat (20). The de-icing fluid (16) is removed fromthe mat (20) by a vacuum system (34). Coupled to the vacuum system (34) is a filter system (38) that separates the de-icing fluid (16) from other fluids such as oil, water, etc., so that the de-icing fluid (16) can be used again. The mat (20) has a plurality of heating elements (30) that prevent the de-icing fluid (16) from freezing on the mat (20) and provide heat to the underside of the aircraft (10).
申请公布号 WO9531368(A1) 申请公布日期 1995.11.23
申请号 WO1995US06033 申请日期 1995.05.12
申请人 TARICCO, TODD 发明人 TARICCO, TODD
分类号 B64F5/00 主分类号 B64F5/00
代理机构 代理人
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