COCKPIT WINDOW OF AIRCRAFT HAVING ELECTROMAGNETIC SHIELD, AND AIRCRAFT

• US 20130026296A1
• Filed: 01/24/2011
• Published: 01/31/2013
• Est. Priority Date: 04/19/2010
• Status: Active Grant

• Current Assignee: Msj Asset Management Co.
• Original Assignee: Mitsubishi Aircraft Corporation (Mitsubishi Heavy Industries, Ltd.)
• Inventors: Yokoi, Takashi
• Granted Patent: US 8,714,487 B2
• Time in Patent Office: Days
• US Class Current: 244/129.3
• CPC Class Codes: B32B 17/10045 with at least one intermediate layer consisting of a glass sheet
• CPC Class Codes: B32B 17/10174 Coatings of a metallic or dielectric material on a constituent layer of glass or polymer
• CPC Class Codes: B32B 17/10293 Edge features, e.g. inserts or holes
• CPC Class Codes: B32B 17/10761 containing vinyl acetal
• CPC Class Codes: B32B 17/1077 containing polyurethane
• CPC Class Codes: B32B 2250/02 2 layers
• CPC Class Codes: B32B 27/308 comprising acrylic (co)polymers
• CPC Class Codes: B64C 1/1476 Canopies; Windscreens or similar transparent elements
• CPC Class Codes: B64C 1/1492 Structure and mounting of the transparent elements in the window or windscreen

Abstract

There is provided a cockpit window of an aircraft and the aircraft in which an electromagnetic shield film for preventing electromagnetic noise can be reliably and easily provided at low cost. An electromagnetic shield film is provided to a window part, and a conductive film is provided between the electromagnetic shield film and an outer retainer made of a conductive material. The conductive film is connected to the electromagnetic shield film via a connecting member is provided so as to be led to an outer perimeter side of the window part along an outer perimeter part of the window part, and is electrically connected to the outer retainer. With this configuration, a film made of a conductive material is formed without a gap at a joint portion between the window part and the outer retainer. Also, the conductive film is assumed to have flexibility.

Claims

1. A cockpit window of an aircraft having an electromagnetic shield comprising:

a plurality of laminated transparent widow panels;

an inner-side inner retainer and an outer-side outer retainer provided to an outer perimeter part of the window panels, the retainers interposing the window panels and made of a conductive material;

a coupling member coupling the inner retainer and the outer retainer to each other;

a weather seal provided between the outer retainer and the window panels;

an electromagnetic shield film provided between two of the window panels that are opposed to each other and made of a conductive material; and

a connecting film made of a conductive material and electrically connecting an outer perimeter part of the electromagnetic shield film and the outer retainer.

2. The cockpit window of the aircraft having the electromagnetic shield according to claim 1, wherein the connecting film has one end interposed between two of the window panels that are opposed to each other to be electrically connected to the electromagnetic shield film and has another end connected to the outer retainer outside the window panels, and an intermediate part between the one end and the other end is along an outer perimeter surface of the window panels and is provided so as to fill a space between the outer perimeter part of the electromagnetic shield film and the outer retainer.

3. The cockpit window of the aircraft having the electromagnetic shield according to claim 2, wherein the connecting film and the electromagnetic shield film are connected via a band-shaped connecting member provided so as to surround the outer perimeter part of the electromagnetic shield film, the connecting member being made of a conductive material.

4. The cockpit window of the aircraft having the electromagnetic shield according to claim 1, wherein the electromagnetic shield film is provided on an inner perimeter side from a portion fastened by the inner retainer and the outer retainer and the connecting film is inserted in the portion.

5. The cockpit window of the aircraft having the electromagnetic shield according to claim 1, wherein a heater layer for anti-icing or de-fogging is further provided between the plurality of window panels.

6. An aircraft comprising the cockpit window having the electromagnetic shield according to any one of claims 1 to 5.