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Covering device for a hinge of an aircraft

A technology of hinges and covers, applied in aircraft accessories, aircraft parts, transportation and packaging, etc., can solve problems such as unfavorable aircraft fuel consumption, impact on aircraft flight weight, turbulent flow, etc.

Inactive Publication Date: 2008-12-17
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The disadvantage is that with these technical solutions there is a gap between the door and the skin of the fuselage of the aircraft, which creates turbulence, which is also not conducive to the fuel consumption of the aircraft, and also affects the flight weight of the aircraft

Method used

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  • Covering device for a hinge of an aircraft
  • Covering device for a hinge of an aircraft
  • Covering device for a hinge of an aircraft

Examples

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Embodiment Construction

[0035] in the following to Figures 1 to 12 In the description of , the same or corresponding elements are denoted by the same reference numerals.

[0036] figure 1 A sectional view showing an embodiment of a hinge according to the invention in an open state with a cover device according to an exemplary embodiment of the invention.

[0037] figure 1 The reference number 1 in the figure represents the first hinge part, which is connected to the second hinge part 2 through the hinge axis 3, so that both the first and the second hinge parts 1, 2 or only one of them can be around the hinge axis. 2 Perform a turning motion. In any case, at least one of the first and second hinge parts 1, 2 can rotate around the hinge axis 3, so that figure 1 shown in the open state and figure 2 Move the hinge between the closed states shown. Reference numeral 4 designates a flexible cover. The flexible cover 4 can be, for example, a plastic film or can be made of an elastic material with a ...

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PUM

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Abstract

Hinges, especially those on aircraft doors, have poor aerodynamic properties. According to one embodiment of the invention, a cover device for an aircraft hinge has a flexible cover (4) that stretches over the outer contour of the hinge, for example for a closed hinge. Advantageously, this can cover the opening between the first hinge part (1) and the second hinge part (2), so that improved aerodynamic properties can be obtained.

Description

[0001] This application claims priority to US Provisional Patent Application No. 60 / 589,284, filed July 19, 2004, and German Patent Application No. 102004034903.7, filed July 19, 2004, the entire contents of which are hereby incorporated by reference. technical field [0002] The invention relates to a cover for a hinge such as an aircraft door hinge. In particular, the invention relates to a cover arrangement for aircraft hinges and aircraft door hinges. Background technique [0003] In aircraft construction, aluminum profiles are riveted on both sides parallel to the door hinges in order to protect the hinges from rainwater intrusion into the fuselage and to protect the doors in the outer area of ​​the aircraft. These aluminum profiles guide rainwater away from the hinges. In particular, such devices are used for cargo doors of cargo aircraft. [0004] On the downside, these externally riveted aluminum profiles create air resistance, which leads to additional fuel consum...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/14E05D11/00
CPCB64C1/14B64C7/00E05D7/009E05D11/0054E05Y2900/502
Inventor 马尔科·明德曼托马斯·施维尔
Owner AIRBUS OPERATIONS GMBH
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