초록 ▼

A surface mounted heater assembly for an aerospace component having a support layer, an electrically resistive heater foil element supported by the support layer, a coating covering the heater element; and an adhesive to secure said support layer to the component is provided. The coating has two lay

A surface mounted heater assembly for an aerospace component having a support layer, an electrically resistive heater foil element supported by the support layer, a coating covering the heater element; and an adhesive to secure said support layer to the component is provided. The coating has two layers that are visually distinct to permit identification of potential exposure of the heater foil element. A surface mounted heater having a multiple layer assembly having a support layer; a heater element and a transition layer to couple the support layer to the aerospace component is provided.

대표청구항 ▼

1. A surface mounted heater assembly for an aerospace component comprising: a support layer, wherein said support layer has a thickness within a range of 0.001 to 0.010 inches;an electrically resistive heater foil element supported by said support layer, wherein said heater foil element has a thickn

1. A surface mounted heater assembly for an aerospace component comprising: a support layer, wherein said support layer has a thickness within a range of 0.001 to 0.010 inches;an electrically resistive heater foil element supported by said support layer, wherein said heater foil element has a thickness within a range of 0.0005 to 0.005 inches;a coating covering said heater element;an adhesive to secure said support layer to said component, wherein said adhesive has a thickness within a range of 0.0005 to 0.010 inches, wherein said coating comprises two layers, said two layers being visually distinct to permit identification of potential exposure of said heater foil element, one of said two layers is an erosion protection layer, the other of said two layers being an erosion indicator layer, said erosion protection layer being exposed to a gas turbine flow path, wherein said erosion protection layer has a thickness within a range of 0.005 to 0.009 inches, and wherein said erosion indicator layer has a thickness within a range of 0.0005 to 0.001 inches; andwherein said erosion protection layer, said erosion indicator layer, said support layer, said heater layer and said adhesive have a total thickness within a range of 0.007 to 0.035 inches. 2. The heater assembly of claim 1, wherein said heater element is made from a material selected from the groups consisting of titanium, titanium alloys, copper, copper alloys, nickel and nickel alloys. 3. The heater assembly of claim 1, wherein said erosion protection layer, said erosion indicator layer, said support layer and said adhesive comprise a polymer. 4. The heater assembly of claim 3, wherein said polymer being applied by a method selected from the group consisting of spraying, electrostatic spraying, roll coating and powder coating. 5. The heater assembly of claim 1, wherein said support layer is directly secured to said component by said adhesive.