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A cabin layout method with stepped bwb layout taking into account aerodynamic shape

An arrangement method and aerodynamic shape technology, which are applied in the directions of ground installations, transportation and packaging, aircraft parts, etc., can solve problems such as the influence of aerodynamic characteristics, and achieve the effect of improving the space utilization rate and the lift-drag ratio of aircraft cruise.

Active Publication Date: 2021-03-12
BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

From the design ideas of Delft University and Boeing, it can be seen that whether it is figure 1 single-layer "bubble" fuselage or figure 2 The double-deck passenger cabin fuselage, the floors of the cylindrical fuselage of each layer are on the same level, which means that in order to meet the height requirements of the passenger and cargo compartments, the central fuselage needs to be modified, which will inevitably affect the aerodynamic characteristics

Method used

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  • A cabin layout method with stepped bwb layout taking into account aerodynamic shape
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  • A cabin layout method with stepped bwb layout taking into account aerodynamic shape

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Embodiment Construction

[0020] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. On the contrary, the invention covers any alternatives, modifications, equivalent methods and schemes within the spirit and scope of the invention as defined by the claims. Further, in order to make the public have a better understanding of the present invention, some specific details are described in detail in the detailed description of the present invention below. The present invention can be fully understood by those skilled in the art without the description of these detailed parts.

[0021] The present invention will be further described below in conjunction with the accompanying drawings and ...

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Abstract

The invention provides a stepped BWB layout passenger and cargo cabin arrangement method. Different from the traditional passenger and cargo cabin arrangement, the passenger and cargo cabin floor in the invention is not on the same horizontal plane, but is distributed in a stepped shape according to different aerodynamic contour height of the section in which the passenger and cargo cabin are located. The goal of the staircase arrangement is to maximize the cruise lift-drag ratio by taking into account the supercritical airfoil shape of the central fuselage as much as possible under the constraints of the cabin and cargo space arrangement.

Description

technical field [0001] The invention belongs to the technical field of overall arrangement in passenger aircraft design, and in particular relates to a method for arranging a passenger cabin with a stepped BWB layout taking into account the aerodynamic shape. Background technique [0002] The basic principle of the traditional BWB layout cabin design is similar to the conventional layout. The passenger and cargo compartments are arranged in a way of multi-channel and multiple cylindrical fuselages side by side. This arrangement is also called "bubble" fuselage design. figure 1 The BWB layout aircraft designed for Delft University in the Netherlands uses this typical multi-cylindrical fuselage design. figure 2 It shows another design method of passenger and cargo compartments, that is, the double-deck passenger and cargo compartment design. The BWB layout in the prior art all adopts horizontal floors for the cabin layout, that is, the cabin floors are basically located on th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/00
CPCB64F5/00
Inventor 夏明罗漫张晓萍周彬白璐李研博
Owner BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC