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Aircraft-floor element, and aircraft zone and aircraft having an aircraft-floor element

A technology for aircraft and components, applied in aircraft floors, aircraft parts, aircraft accessories, etc., can solve the problems of time-consuming and long-term aircraft downtime, and achieve the effect of rapid transformation

Pending Publication Date: 2020-01-21
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Such modifications between the passenger compartment and the cargo compartment and vice versa are rather time-consuming, thereby resulting in longer out-of-service periods of the aircraft

Method used

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  • Aircraft-floor element, and aircraft zone and aircraft having an aircraft-floor element
  • Aircraft-floor element, and aircraft zone and aircraft having an aircraft-floor element
  • Aircraft-floor element, and aircraft zone and aircraft having an aircraft-floor element

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Embodiment Construction

[0049] According to the invention, an aircraft floor element, an aircraft region and an aircraft are described having trim elements which enable the transformation of an aircraft region from a passenger compartment to a cargo compartment and vice versa.

[0050] figure 1 A vertical longitudinal section of the aircraft 10 is schematically shown. The aircraft is only shown here as an example. Aircraft 10 has at least one cabin layer 11 , 12 (levels) in which passengers and / or cargo can be accommodated. therefore, figure 1 The aircraft 10 shown in FIG. 1 has an intermediate floor 100 which separates an upper deck 11 from a lower deck 12 . The ladder 60 connects the upper cabin 11 and the lower cabin 12 . Furthermore, the aircraft area 20 in the lower deck 12 has a floor 101 , so that between the intermediate floor 100 and the floor 101 there is an interior space of the aircraft, which is used selectively as a passenger compartment or a cargo compartment.

[0051] The aircraf...

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PUM

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Abstract

An aircraft-floor element comprising a first cladding element configure to be swung from a first position to a second position. In the first position, the first cladding element is arranged parallel to a main plane of the aircraft-floor element and on a side of the aircraft-floor element which is directed towards a passenger cabin. In the second position, the first cladding is arranged at an angleto the main plane of the aircraft-floor element, wherein it forms a cladding for a cargo space. An aircraft zone having an aircraft-floor element and an aircraft having such an aircraft zone are alsodisclosed.

Description

technical field [0001] The invention relates to an aircraft floor element with a reversible trim element, and in particular the invention relates to an aircraft floor element with a reversible trim element, wherein the trim element forms the aircraft in a first position A part of the floor element and facing the passenger compartment constitutes a trim for the cargo compartment in the second deployed position. Background technique [0002] In certain vehicles, especially in mass transportation such as aircraft, trains, buses and boats, an attempt is made to use the available space as variedly as possible. For example, the interior of the aircraft can be converted from a passenger compartment to a cargo compartment and vice versa. To this end, it is necessary to remove the seat rows of the passenger compartment and, if appropriate, to ensure, when forming the cargo compartment, that there is an airtight separation of the cargo compartment in the case of another passenger are...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/18
CPCB64C1/18B64C1/066B64D11/0023B64D2011/0046Y02T50/40
Inventor 克劳斯-皮特·格鲁斯
Owner AIRBUS OPERATIONS GMBH