Systems and methods for heat shield assemblies
AssigneeGoodrich Corporation
InventorsJoshua Craig Houser, Katrina Lynn King
Life of this patent
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Abstract
Systems and methods disclosed herein may be useful for aircraft heat shield assemblies. In this regard, a heat shield assembly is provided comprising a heat shield having an aperture, the aperture comprising an end portion and an insertion portion, the insertion portion having a width larger than the end portion, a spacer comprising an upper portion, an undermount flange and a gap between the upper portion and the undermount flange, wherein a surface of the gap is engaged with the heat shield, and wherein the undermount flange has a width less than the insertion portion of the aperture and greater than the width of the end portion.
Claims12
1-4. (canceled)
A heat shield spacer comprising:
- an upper portion having a first width;
- an undermount flange having a second width, wherein the second width is less than the first width;
- and
- a gap between the upper portion and the undermount flange, wherein the gap has a third width, wherein the third width is less than the first width and the second width,
- wherein the gap extends along a length of the spacer and along a terminus of the spacer.
15-18. (canceled)
Dependencies are inferred from the claim text.