Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
150 words
An engine component comprising a substrate metal and having a composite thermal shield covering a portion of an external surface of said component, said composite shield comprising an external solid metal layer, a first layer of permeable metal bonded to said external solid metal layer, an internal solid metal layer, and a second permeable metal layer, said internal solid metal layer positioned intermediately of and bonded on its opposed sides to said first and second permeable metal layers, wherein the interstices of said second permeable metal layer are substantially filled with said substrate metal, whereby said composite thermal shield is mechanically affixed to the substrate metal of said engine component, and wherein said substrate metal extends into said interstices of only said second permeable metal layer, said internal solid metal layer being disposed for preventing substrate metal from entering said first layer of permeable metal during manufacture of said component.
Claim 2
Dependent Claim
150 words
An engine component comprising a substrate metal and having a composite thermal shield covering a portion of an external surface of said component, said composite shield comprising an external solid metal layer, a first layer of permeable metal bonded to said external solid metal layer, an internal solid metal layer, and a second permeable metal layer, said internal solid metal layer positioned intermediately of and bonded on its opposed sides to said first and second permeable metal layers, wherein the interstices of said second permeable metal layer are substantially filled with said substrate metal, whereby said composite thermal shield is mechanically affixed to the substrate metal of said engine component, and wherein said substrate metal extends into said interstices of only said second permeable metal layer, said internal solid metal layer being disposed for preventing substrate metal from entering said first layer of permeable metal during manufacture of said component.
Claim 3
Dependent Claim
25 words
The engine component of claim 1, wherein said first solid metal layer extends over both top and edge portions of said first permeable metal layer.
Claim 4
Dependent Claim
16 words
The engine component of claim 1 wherein said first solid metal layer comprises a stainless steel.
Claim 5
Dependent Claim
16 words
The engine component of claim 1 wherein said first solid metal layer comprises a tungsten alloy.
Claim 6
Dependent Claim
17 words
The engine component of claim 1 wherein said first solid metal layer comprises an alloy of palladium.
Claim 7
Dependent Claim
18 words
The engine component of claim 1 wherein said first solid metal layer comprises a nickel and chrome alloy.
Claim 8
Dependent Claim
17 words
The engine component of claim 1 wherein said permeable metal is comprised of a filamentary wire mesh.
Claim 9
Dependent Claim
29 words
The engine component of claim 1 wherein said permeable metal is comprised of a filamentary wire mesh, and wherein said filamentary wire mesh comprises woven layers of stainless steel.
Claim 10
Dependent Claim
17 words
The engine component of claim 1 wherein said permeable metal is comprised of a metallic skeletal material.
Claim 11
Dependent Claim
14 words
The engine component of claim 1 wherein said substrate metal is an aluminum alloy.
Claim 12
Dependent Claim
13 words
The engine component of claim 1 wherein said substrate metal is cast iron.
Claim 13
Independent Claim
89 words
A method of forming a composite thermal shield in combination with a member of an internal combustion engine formed of a substrate metal, said method comprising the steps of bonding a first solid layer of metal to one face of a first layer of permeable metal, bonding a second solid layer of metal to the opposite face of said first layer of permeable metal, bonding a second layer of permeable metal to said second solid layer of metal, and casting said substrate metal into said second permeable metal layer.
Claim 14
Independent Claim
89 words
A method of forming a composite thermal shield in combination with a member of an internal combustion engine formed of a substrate metal, said method comprising the steps of bonding a first solid layer of metal to one face of a first layer of permeable metal, bonding a second solid layer of metal to the opposite face of said first layer of permeable metal, bonding a second layer of permeable metal to said second solid layer of metal, and casting said substrate metal into said second permeable metal layer.
Claim 15
Dependent Claim
23 words
The method of claim 12 wherein said casting step includes application of pressure in the range of ten thousand pounds per square inch.