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

Active Publication Date: 2017-07-07
COMAC +1
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

At the same time, it is necessary to separate the heat and sound insulation layer from the aircraft skin, and try to prevent the condensed water generated inside the aircraft skin from entering the heat and s

Method used

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  • Heat and sound insulation device for aircraft cockpit structure
  • Heat and sound insulation device for aircraft cockpit structure
  • Heat and sound insulation device for aircraft cockpit structure

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Embodiment Construction

[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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Abstract

The invention provides a heat and sound insulation device for an aircraft cockpit structure. The heat and sound insulation device for the aircraft cockpit structure comprises a heat and sound insulation layer, the heat and sound insulation layer is arranged between an aircraft skin and an interior trimming panel, and the space between the heat and sound insulation layer and the aircraft skin is filled with airbags. A sound insulation device used for a commercial aircraft to improve sound insulation effects of aircraft cockpits is provided, the heat and sound insulation device for the aircraft cockpit structure can reduce the noise level in the aircraft cockpits, and meanwhile, try to avoid the increase of the weight of the aircraft to improve the service life of the heat and sound insulation layer.

Description

technical field [0001] The invention relates to a heat and sound insulation device for aircraft cockpit structure, in particular to a heat and sound insulation device for reducing the internal noise level of the aircraft cockpit and suppressing the formation and damage of condensed water on the aircraft skin. Background technique [0002] Since the purpose of commercial aircraft is mainly to transport passengers, the comfort of the cabin environment of commercial aircraft is an important indicator reflecting the quality of commercial aircraft. With the continuous advancement of technology, the diversification of human comfort indicators, and the gradual popularization of civil passenger aircraft transportation , the noise level in the cabin has been paid more and more attention in the comfort design index of civil airliner. Because there are external sound sources such as external pneumatics, engines, APUs, landing gear, hydraulic pumps, etc. in civil airliners, there are al...

Claims

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Application Information

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IPC IPC(8): B64C1/40
CPCB64C1/40
Inventor 孙学德郭天鹏刘毓迪汪光文王大伟
Owner COMAC
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