Anticorrosion film on the aerodynamic force face that is heated

Anticorrosion film on the aerodynamic force face that is heated

  • CN 101,778,916 B
  • Filed: 07/28/2008
  • Issued: 09/23/2015
  • Est. Priority Date: 08/10/2007
  • Status: Active Grant
First Claim
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1. an anti-corrosion structure, comprising:

  • A) aircraft parr, comprising;

    I) there is the aircraft skin part of outside surface, andIi) the anti-mechanism of ice that described outside surface can be heated to above the temperature of 65 DEG C be connected with described aircraft skin part;

    B) adhesive tape, comprising;

    I) at least one deck comprises the layer of cross-linked polymer, and described cross-linked polymer is selected from cross-linked polyurethane, crosslinked polyureas and crosslinked mixing polyurethane/polyurea polymkeric substance, andIi) binder layer;

    Wherein said adhesive tape is adhered to the described outside surface of described aircraft skin part by described binder layer.

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