A sealed assembly comprising: a first member; a second member spaced apart from said first member; and a fire seal positioned between said first member and said second member, said fire seal comprising: an acute bend comprising a first end portion and a second end portion; a first engagement extension extending from said first end portion of said acute bend, said first engagement extension being in touching engagement with said first member; and a second engagement extension extending from said second end portion of said acute bend, wherein said second engagement extension is at an acute angle relative to said first engagement extension to define a partially enclosed volume between said first engagement extension and said second engagement extension, said second engagement extension being in touching engagement with said second member; wherein said first engagement extension is connected to the first member with at least one mechanical fastener; wherein said acute bend comprises a radius, wherein said first engagement extension comprises a width which is a linear distance that the first engagement extension extends from the first end portion of the acute bend, and wherein said radius is at least about 10 percent of said width; wherein said fire seal is formed as a layered structure comprising a first layer and a second layer, said first layer comprising a plurality of first segments and said second layer comprising a plurality of second segments, wherein said plurality of first segments are staggered from said plurality of second segments; and wherein said first member is a nozzle of an engine of an aircraft, and said second member is a pylon fairing of said aircraft, and wherein said fire seal is positioned such that said acute bend protrudes toward an aft end of said engine such that said fire seal opens toward a forward end of said engine. a first member; a second member spaced apart from said first member; and a fire seal positioned between said first member and said second member, said fire seal comprising: an acute bend comprising a first end portion and a second end portion; a first engagement extension extending from said first end portion of said acute bend, said first engagement extension being in touching engagement with said first member; and a second engagement extension extending from said second end portion of said acute bend, wherein said second engagement extension is at an acute angle relative to said first engagement extension to define a partially enclosed volume between said first engagement extension and said second engagement extension, said second engagement extension being in touching engagement with said second member; wherein said first engagement extension is connected to the first member with at least one mechanical fastener; wherein said acute bend comprises a radius, wherein said first engagement extension comprises a width which is a linear distance that the first engagement extension extends from the first end portion of the acute bend, and wherein said radius is at least about 10 percent of said width; wherein said fire seal is formed as a layered structure comprising a first layer and a second layer, said first layer comprising a plurality of first segments and said second layer comprising a plurality of second segments, wherein said plurality of first segments are staggered from said plurality of second segments; and wherein said first member is a nozzle of an engine of an aircraft, and said second member is a pylon fairing of said aircraft, and wherein said fire seal is positioned such that said acute bend protrudes toward an aft end of said engine such that said fire seal opens toward a forward end of said engine. an acute bend comprising a first end portion and a second end portion; a first engagement extension extending from said first end portion of said acute bend, said first engagement extension being in touching engagement with said first member; and a second engagement extension extending from said second end portion of said acute bend, wherein said second engagement extension is at an acute angle relative to said first engagement extension to define a partially enclosed volume between said first engagement extension and said second engagement extension, said second engagement extension being in touching engagement with said second member; wherein said first engagement extension is connected to the first member with at least one mechanical fastener; wherein said acute bend comprises a radius, wherein said first engagement extension comprises a width which is a linear distance that the first engagement extension extends from the first end portion of the acute bend, and wherein said radius is at least about 10 percent of said width; wherein said fire seal is formed as a layered structure comprising a first layer and a second layer, said first layer comprising a plurality of first segments and said second layer comprising a plurality of second segments, wherein said plurality of first segments are staggered from said plurality of second segments; and wherein said first member is a nozzle of an engine of an aircraft, and said second member is a pylon fairing of said aircraft, and wherein said fire seal is positioned such that said acute bend protrudes toward an aft end of said engine such that said fire seal opens toward a forward end of said engine.