Method for manufacturing a thermoacoustic insulation module for an aircraft comprising a bending step
First Claim
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1. A method for manufacturing a thermoacoustic insulation module for an aircraft, comprising:
- providing a mat configured to provide thermoacoustic insulation of an aircraft portion;
followed byattaching a bendable structure to the mat;
followed bybending the bendable structure, along a bending axis parallel to a longitudinal direction of the mat, such that the bendable structure forms a load-bearing structure supporting the mat in a curved shape, the load-bearing structure and the mat together forming said thermoacoustic insulation module.
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Abstract
In order to facilitate the thermoacoustic insulation of an aircraft portion, a method for manufacturing a thermoacoustic insulation module for an aircraft comprises a step of providing a mat configured to provide thermoacoustic insulation of an aircraft portion, followed by a step of attaching a bendable structure to the mat, followed by a step of bending the bendable structure, along a bending axis parallel to a longitudinal direction of the mat, such that the bendable structure forms a load-bearing structure supporting the mat in a curved shape.
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Citations
10 Claims
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1. A method for manufacturing a thermoacoustic insulation module for an aircraft, comprising:
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providing a mat configured to provide thermoacoustic insulation of an aircraft portion;
followed byattaching a bendable structure to the mat;
followed bybending the bendable structure, along a bending axis parallel to a longitudinal direction of the mat, such that the bendable structure forms a load-bearing structure supporting the mat in a curved shape, the load-bearing structure and the mat together forming said thermoacoustic insulation module. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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Specification