Heat and sound insulation device for aircraft cockpit structure
An aircraft cockpit and sound insulation technology, which is applied in the direction of fuselage insulation, etc., can solve problems such as decay, heat insulation layer weight gain, and reduction of heat insulation and sound insulation performance, so as to prevent condensation, avoid structural corrosion, and reduce heat insulation. The effect of sound performance
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[0026] In the following detailed description of the embodiments, reference is made to the accompanying drawings that form a part hereof. The drawings show, by way of example, specific embodiments in which the invention may be practiced. The illustrated embodiments are not intended to be exhaustive of all embodiments according to the invention. It is to be understood that other embodiments may be utilized and structural or logical changes may be made without departing from the scope of the present invention. With respect to the drawings, directional terms, such as "below," "upper," "left," "right," etc., are used with reference to the orientation of the drawings being described. Since components of embodiments of the invention can be implemented in a variety of orientations, these directional terms are used for purposes of description, not limitation. Accordingly, the following detailed description is not intended to be limiting, and the scope of the invention is defined by t...
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