Acoustic structure with internal thermal regulators
View Patent ↗Thermally insulating septums are located internally within the cells of an acoustic honeycomb to regulate heat flow into the acoustic structure. The internally located insulating septums protect the honeycomb and acoustic septums located within the honeycomb cells from heat damage that might otherwise be caused by a heat source, such as the hot section of a jet engine. The internal thermal regulators are useful in combination with heat blankets or other thermal insulating structures to provide a reduction in size and/or weight of the insulating structure while still providing the same overall degree of thermal insulation for the acoustic honeycomb.
1. An acoustic structure having an internal thermal regulator, said acoustic structure comprising:
a honeycomb comprising a first edge that is to be located closest to a high temperature area and a second edge, said honeycomb comprising a cell defined by a plurality of walls that extend between said first and second edges;
a thermally insulating septum located within said cell adjacent to the first edge of said honeycomb to provide said internal thermal regulator, said thermally insulating septum comprising sides which are attached to the walls of said cell;
an acoustic damping material located within said cell between said thermally insulating septum and said second edge; and
a perforated acoustic panel attached to the second edge of said honeycomb wherein sound waves can enter said cell through said perforated acoustic panel.
2. An acoustic structure according to claim 1 which further comprises a solid protective sheet which is attached to the first edge of said honeycomb.
3. An acoustic structure according to claim 1 wherein said acoustic damping material is an acoustic septum.
4. An acoustic structure according to claim 1 wherein said acoustic damping material is difunctional filler material that provides both thermal insulation and sound attenuation within said cell.
5. An acoustic structure according to claim 1 which further includes a thermal insulation structure located between the first edge of said honeycomb and said high temperature area.
6. An acoustic structure according to claim 5 wherein an air gap is located between said thermal insulation structure and the first edge of said honeycomb.
7. An acoustic structure according to claim 1 wherein said honeycomb walls comprise fibers and a cured resin.
8. A jet engine that comprises an acoustic structure according to claim 1 .
9. A jet engine that comprises an acoustic structure according to claim 5 and wherein said jet engine comprises a high temperature area having a temperature of between 750° F. and 900° F.
10. A method for making an acoustic structure having an internal thermal regulator, said method comprising the steps of:
providing a honeycomb comprising a first edge that is to be located closest to a high temperature area and a second edge, said honeycomb comprising a cell defined by a plurality of walls that extend between said first and second edges;
locating a thermally insulating septum within said cell adjacent to the first edge of said honeycomb to provide said internal thermal regulator, said thermally insulating septum comprising sides which are attached to the walls of said cell;
locating an acoustic damping material within said cell between said thermally insulating septum and said second edge; and
attaching a perforated acoustic panel to the second edge of said honeycomb wherein sound waves can enter said cell through said perforated acoustic panel.
11. A method for making an acoustic structure according to claim 10 which includes the additional step of attaching a solid protective sheet to the first edge of said honeycomb.
12. A method for making an acoustic structure according to claim 10 wherein said acoustic damping material is an acoustic septum.
13. A method for making an acoustic structure according to claim 10 wherein said acoustic damping material is a difunctional filler material that provides both thermal insulation and sound attenuation within said cell.
14. A method for making an acoustic structure according to claim 10 which further includes the additional step of locating a thermal insulation structure adjacent to the first edge of said honeycomb.
15. A method for making an acoustic structure according to claim 14 wherein said thermal insulation structure is located adjacent to the first edge of said honeycomb such that an air gap is located between said thermal insulation structure and the first edge of said honeycomb.
16. A method for making an acoustic structure according to claim 10 wherein said honeycomb walls comprise fibers and a cured resin.
17. A method for providing thermal insulating and sound dampening for a jet engine that comprises a high temperature area, said method comprising the step of locating an acoustic structure having an internal thermal regulator according to claim 1 adjacent to said high temperature area.
18. A method for providing thermal insulating and sound dampening for a jet engine that comprises a high temperature area, said method comprising the step of locating an acoustic structure having an internal thermal regulator according to claim 5 adjacent to said high temperature area.
19. An acoustic structure according to claim 1 wherein said thermally insulating septum comprises hollow microspheres and a matrix of resin.
20. An acoustic structure according to claim 19 wherein said matrix of resin comprises polyimide resin.