Windshield protective cover for aircraft windshield glass and installation method
A windshield and protective cover technology, applied in windshields, aircraft accessories, windows, etc., can solve the problems of aircraft surface equipment damage, body surface wear, inconvenient installation, etc., to achieve the effect of protecting the windshield glass.
Active Publication Date: 2018-07-31
COMAC +1
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Problems solved by technology
[0010] In view of this, in order to solve the above-mentioned technical problems, the present invention provides a windshield protective cover for an aircraft windshield and a method for installing the protective cover. Avoid wind and sand pouring into the protective cover; and the installation of the present invention is more convenient, get rid of the traditional way of relying on ropes to fix the windshield glass protective cover, and solve the resulting installation inconvenience, and when the wind and sand are poured into the protective cover or windshield When the protective cover is blown, it is easy to cause wear on the surface of the airframe and damage to the surface equipment of the aircraft
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[0033] In the following detailed description of the preferred embodiments, reference will be made to the attached drawings constituting a part of the present invention. The attached drawings illustrate specific embodiments capable of implementing the present invention by way of example. The illustrated embodiments are not intended to be exhaustive of all embodiments according to the present invention. It should be noted that although the steps of the method of the present invention are described in a specific order in this article, this does not require or imply that these operations must be performed in the specific order, or that all the operations shown must be performed to achieve the desired result. The drawings are not shown to scale. On the contrary, in order to clarify multiple parts and parts, the parts and parts may be enlarged in the drawings. Whenever possible, the same reference numerals will be used in all drawings and the corresponding written description to r...
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The invention discloses a protective cover for an aircraft windshield, which is characterized in that a bonding layer composed of viscous material is arranged inside the windshield protective cover. The aircraft windshield protective cover is firmly adsorbed on the aircraft windshield glass through the sticky bonding layer with strong molecular adsorption force, so that the aircraft windshield protective cover is installed on the aircraft windshield glass to prevent external wind and sand from affecting the aircraft windshield glass. erosion. The invention has the advantages of easy installation, small covering area, no need to use ropes in the traditional method to fix the windshield protective cover, thereby avoiding the damage of the ropes to the parts around the machine head. When the wind and sand are relatively large, the present invention can effectively prevent the wind and sand from pouring into the windshield protective cover.
Description
Technical field [0001] The invention relates to the field of aircraft ground support equipment, and in particular to an aircraft windshield glass protective cover used in aircraft ground support equipment and a quick installation method thereof. When the invention is used for parking outside the airport, it is installed outside the windshield glass of the aircraft to shield the windshield glass, protect the windshield glass of the aircraft and avoid the erosion of the windshield glass of the aircraft by the wind and sand. Background technique [0002] When the aircraft is parked in the open for a long time, it is necessary to install the aircraft windshield protective cover to avoid the erosion of the aircraft windshield glass by wind and sand. To prevent the sand entrained by the wind from scratching the windshield glass of the aircraft. The scratched windshield will seriously affect the pilot's observation effect. [0003] The aircraft windshield protective cover currently used...
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IPC IPC(8): B60J11/08B64C1/14
Inventor 邓英华聂鑫
Owner COMAC