Thermal insulation structure
AssigneeThe Boeing Company
InventorsAnna L. Bendig, Douglas McLaren
Life of this patent
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AssigneeThe Boeing Company
InventorsAnna L. Bendig, Douglas McLaren
Estimating the term…
A thermal insulating structure for providing thermal insulation, structural load accommodations, and noise attenuation for surfaces in aerospace systems that are exposed to high temperatures. At the side adjacent the structure to be protected is a high-temperature solid back sheet to which is adhesively bonded a honeycomb core having a perforated buried septum. A layer of cast fiber-ceramic insulation is secured to the honeycomb core, filling portions of the core outward from the septum and extending beyond the outer face of the core. To absorb structural loads, a densified top coat overlies the insulating layer. To minimize the transmission of shear-inducing loads into the insulating layer, the outer face of the honeycomb core has an irregular surface. Core cell vents extending through the walls of adjacent cells provide a controlled airspace between the back sheet and the buried septum through which a fluid coolant may be circulated.
Thermal ceramic insulation, comprising:
Dependencies are inferred from the claim text.