To facilitate the thermophonic insulation of an aircraft section, a method comprises engaging first respective parts of flexible structures, respectively connected to two flat mattresses, with a support device, by leaving free respective second parts of the flexible structures arranged at a distance from the first parts, then curving the two mattresses, by virtue of the mutual bringing together of the second parts, then inserting the support device into the aircraft section, and detaching each mattress from the support device and fixing each mattress to an aircraft structure delimiting the aircraft section.

A support bracket for holding interior components of a vehicle includes a base plate and an add-on module, which are engageable with each other to facilitate replacement and maintenance.

An insulation component to be attached to a fuselage structure of an aircraft. The insulation component extends in a planar manner, and at least one peripheral recess, running transversely to the at least one longitudinal recess, is formed in a first surface of the insulation component configured to receive a respective associated peripheral support of the fuselage structure.

Systems and methods are provided for insulation and moisture drainage. One exemplary embodiment is an apparatus comprising a bay blanket configured to insulate an aircraft. The bay blanket includes insulation, and a first waterproof lip that protrudes from the insulation in an outboard direction towards a frame of the aircraft and extends along a length of a leftward side of the bay blanket. The bay blanket also includes a second waterproof lip that protrudes from the insulation in an outboard direction towards the frame of the aircraft along a length of a rightward side of the bay blanket.

A blanket assembly for use in at least one bay and with at least one frame member of an aircraft, the assembly including an insulation blanket. The insulation blanket includes a bay section sized and shaped to fit within the bay and of sufficient thickness to provide insulation to the bay, a return section disposed on a first side of the bay section; and a cap section disposed on a second side of the bay section, opposite the first side. The cap section is sized and shaped to at least partially cover the frame member when the cap section is wrapped around the frame member, the cap section being of sufficient thickness to provide insulation to the frame member. The bay section, the return section, and the cap section are of unitary construction.

An insulation insert comprises a hollow cylinder formed of a closed cell foam, a first adhesive layer on a first face of the hollow cylinder, a flange of the closed cell foam extending from the hollow cylinder, and a second adhesive layer on a second face of the flange.

A noise attenuating device for reducing acoustic resonance in a cavity of an aircraft with an opening in a skin of the aircraft defining a first surface area and an opening peripheral edge includes a connection mechanism for securing the noise attenuating device in proximity to the opening in the skin of the aircraft and an exterior surface. The exterior surface defines a second surface area that is less than the first surface area of the opening and a device peripheral edge, which has a first section having an edge profile complimentary to at least a portion of the opening peripheral edge and a second section having an indented edge profile in relation to the first section such that when the noise attenuating device is secured within the opening, at least one gap is formed between the device peripheral edge and the opening peripheral edge.

An aircraft line or harness fastening system with a clamp attaching the line or harness to the aircraft. A bobbin within the clamp surrounds the line or harness, wherein the bobbin is smaller than the clamp and is circular in shape to enable rotation of the bobbin within the clamp. The bobbin includes two separate complementary parts that fit together around the line or harness. Each of the two separate complementary parts include a tab and a recess, wherein the tab of one of the complementary parts fits into the recess on the other of the complementary parts.

A method for manufacturing a profile rail including a base made of a first material and a top portion to be exposed during use of the profile rail in the floor of a vehicle including a second material that is harder and/or less corrosive as the first material. The method includes the steps of providing the base made of the first material, coating at least the top portion of the base with the second material by a cold spray process, and machining the coating to provide a predefined surface structure of the top portion.

A sealable securing system includes a hook member including a first base, at least one hook group coupled to the first base, and a first seal coupled to the first base. The hook member is configured to be secured to a first component. A loop member includes a second base, at least one loop group coupled to the second base, and a second seal coupled to the second base. The loop member is configured to be secured to a second component. The hook member and the loop member are configured to removably secure to one another.