Thermal insulation blanket and thermal insulation blanket assembly
A thermal insulation blanket assembly having a thermal insulation blanket including an aerogel insulation material having a first surface and a second surface that is oppositely-disposed from the first surface, a backing covering the second surface of the aerogel insulation material, and a skin layer covering the first surface of the aerogel insulation material.
1. A thermal insulation cover, comprising:
an aerogel insulation material having a first surface and a second surface that is oppositely-disposed from the first surface;
a backing covering the second surface of the aerogel insulation material; and
a metallic foil skin layer covering the first surface of the aerogel insulation material and wrapping around an end of the aerogel insulation material and a portion of the backing and a portion of the second surface.
2. The thermal insulation cover of claim 1 wherein the backing is a polyimide film.
3. The thermal insulation cover of claim 1 , further comprising adhesive located between at least a portion of the skin layer and the backing.
4. The thermal insulation cover of claim 3 , further comprising an integral fastener having a head and a screw portion.
5. The thermal insulation cover of claim 4 wherein the head of the integral fastener is located within the adhesive.
6. The thermal insulation cover of claim 5 wherein the screw portion projects through the skin layer.
7. The thermal insulation cover of claim 4 wherein the thermal insulation cover is installed via the integral fastener in a core engine of a gas turbine engine.
8. The thermal insulation cover of claim 7 wherein the thermal insulation cover is installed so as to thermally protect a cowl that defines a boundary of a bypass duct of the gas turbine engine.
9. The thermal insulation cover of claim 7 wherein the backing forms a cold side barrier and the skin layer forms a hot side barrier in the gas turbine engine.
10. The thermal insulation cover of claim 1 wherein the aerogel insulation material is sealed at a set of edges by the skin layer.
11. A thermal insulation blanket assembly covering at least a portion of a core engine of a gas turbine engine, comprising:
a thermal insulation blanket having a layered construction, comprising:
an aerogel insulation material having a first surface and a second surface that is oppositely-disposed from the first surface;
a backing covering the second surface of the aerogel insulation material;
a skin layer covering the first surface of the aerogel insulation material and wrapping around an end of the aerogel insulation material, a portion of the backing, and a portion of the second surface; and
a fastener integrated into the blanket and configured to operably fasten to a cowl of the core engine; and
an attachment structure mounted to a cowl of the core engine, wherein the attachment structure comprises an attachment flange having a coupling post that is configured to retain a portion of the fastener.
12. The thermal insulation blanket assembly of claim 11 wherein the attachment flange is metallic and the coupling post is nylon.
13. The thermal insulation blanket assembly of claim 11 wherein the fastener comprises a head retained by the skin layer and a screw portion that projects away from the second surface and is configure to be retained within the coupling post.
14. The thermal insulation blanket assembly of claim 11 wherein the skin layer is a metallic foil that is configured to seal edges of the aerogel insulation material.
15. The thermal insulation blanket assembly of claim 11 wherein the backing is a polyimide film.
16. A thermal insulation blanket assembly for a gas turbine engine, comprising:
a thermal insulation blanket, comprising:
an aerogel insulation material having oppositely-disposed first and second surfaces;
a metal skin layer covering the first surface of the aerogel insulation material and wrapping around an end to cover an edge of the second surface; and
an integrated fastener configured to mate with a structure on a cowl of the gas turbine engine; and
wherein the thermal insulation blanket has a thickness ranging from 1.2 mm to 7.5 mm.
17. The thermal insulation blanket assembly of claim 16 , further comprising at least one of a glass fiber insulation material or a ceramic insulation material.
18. The thermal insulation blanket assembly of claim 16 wherein the thermal insulation blanket assembly will have an installed weight of approximately 1.953 kilograms per square meter or less.