A vehicle body includes a primary vehicle structure and interior vehicle fittings as well as a coupling device for fastening the interior vehicle fittings to the primary vehicle structure. The coupling device is configured to generate a magnetic field, so as to fasten the interior vehicle fittings to the primary vehicle structure without contact. Methods for assembling a vehicle body as well as an edifice are also described.

A vehicle body includes a primary vehicle structure and interior vehicle fittings as well as a coupling device for fastening the interior vehicle fittings to the primary vehicle structure. The coupling device is configured to generate a magnetic field, so as to fasten the interior vehicle fittings to the primary vehicle structure without contact. Methods for assembling a vehicle body as well as an edifice are also described.

A composite insulation is included between the skin of an aircraft and interior trim panels. The composite insulation includes multiple layers of micro-perforate material interspersed with layers of semi-rigid material. For a given thickness, the composite insulation provides superior transmission loss over a wide range of frequencies, including low frequencies, compared to conventional homogeneous insulation having the same thickness. Thus, the composite insulation reduces broadband noise within the cabin of an aircraft more effectively compared to conventional insulation.

A composite insulation is included between the skin of an aircraft and interior trim panels. The composite insulation includes multiple layers of micro-perforate material interspersed with layers of semi-rigid material. For a given thickness, the composite insulation provides superior transmission loss over a wide range of frequencies, including low frequencies, compared to conventional homogeneous insulation having the same thickness. Thus, the composite insulation reduces broadband noise within the cabin of an aircraft more effectively compared to conventional insulation.

A thermal insulation support includes a body including a first edge portion and a second edge portion extending generally along a longitudinal axis of the body. A first flange extending a first distance from the first edge portion of the body is coupled to a first wall. A second flange extending a second distance from the second edge portion of the body is coupled to a second wall.

A thermal insulation support includes a body including a first edge portion and a second edge portion extending generally along a longitudinal axis of the body. A first flange extending a first distance from the first edge portion of the body is coupled to a first wall. A second flange extending a second distance from the second edge portion of the body is coupled to a second wall.

Methods and apparatus for forming and installing insulation blankets in a vehicle compartment are disclosed. An example apparatus includes an insulation blanket that includes an outer layer, an insulation layer disposed in the outer layer, and a first fastener disposed in the insulation layer. The outer layer and the insulation layer are to form to a first channel. The first fastener is to receive, via the first channel, a first portion of a vehicle compartment frame to sealingly couple the insulation layer and the outer layer of the insulation blanket to the vehicle compartment frame.

Methods and apparatus for forming and installing insulation blankets in a vehicle compartment are disclosed. An example apparatus includes an insulation blanket that includes an outer layer, an insulation layer disposed in the outer layer, and a first fastener disposed in the insulation layer. The outer layer and the insulation layer are to form to a first channel. The first fastener is to receive, via the first channel, a first portion of a vehicle compartment frame to sealingly couple the insulation layer and the outer layer of the insulation blanket to the vehicle compartment frame.

An existing acoustic honeycomb panel having a radius of curvature is cut into segments that have longitudinal and lateral sides that extend between the edges of the honeycomb. The segments are bonded together along their longitudinal or lateral sides to form a segmented acoustic honeycomb in which the radius of curvature is different from the radius of curvature of the original acoustic honeycomb panel. The shape of the longitudinal or lateral sides of the segments and the thickness of the adhesive bond can be controlled to provide segmented acoustic honeycomb panels that are tightly curved and which are suitable for use in demanding noise damping applications, such as jet engine nacelles.

An existing acoustic honeycomb panel having a radius of curvature is cut into segments that have longitudinal and lateral sides that extend between the edges of the honeycomb. The segments are bonded together along their longitudinal or lateral sides to form a segmented acoustic honeycomb in which the radius of curvature is different from the radius of curvature of the original acoustic honeycomb panel. The shape of the longitudinal or lateral sides of the segments and the thickness of the adhesive bond can be controlled to provide segmented acoustic honeycomb panels that are tightly curved and which are suitable for use in demanding noise damping applications, such as jet engine nacelles.