Crew rest cabin for aircraft and construction method thereof and aircraft

An aircraft and aviation technology, applied in the field of crew rest cabins, can solve problems such as insufficient use of space, and achieve the effects of improving market competitiveness, expanding space, and improving comfort

Active Publication Date: 2021-01-15
COMAC +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the number of berths is designed to be fixed and the number of resters is insufficient, the space cannot be fully utilized

Method used

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  • Crew rest cabin for aircraft and construction method thereof and aircraft
  • Crew rest cabin for aircraft and construction method thereof and aircraft
  • Crew rest cabin for aircraft and construction method thereof and aircraft

Examples

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Embodiment Construction

[0037] Only according to the preferred embodiment of the present invention, those skilled in the art can think of other ways to realize the present invention on the basis of the preferred embodiment, and the other ways also fall within the scope of the present invention. In the following detailed description, directional terms, such as "left", "right", "upper", "lower", "inner", "outer", etc., are used with reference to the directions described in the drawings, where "longitudinal "Refers to the length direction of the aircraft. Components of embodiments of the present invention may be positioned in a variety of different orientations, and directional terms are used for purposes of illustration and not limitation. Specifically, the "longitudinal axis" mentioned herein refers to the axis longitudinally running through the length direction of the aircraft, "longitudinal" refers to the length direction of the aircraft (crew rest cabin), and "transverse" refers to the "Portrait" ...

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PUM

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Abstract

The invention relates to a crew rest cabin for an aircraft. The crew rest cabin has a longitudinal axis, a first transverse end wall and a second transverse end wall, and comprises a first region, a second region and an intermediate region. The intermediate region has two fixed compartments. The first region and the second region are each provided with two movable division plates parallel to the longitudinal axis, the movable division plates being respectively aligned with the longitudinal walls of the fixed compartments and configured to be longitudinally movable simultaneously from a deployment position to a storage position. In the deployment position, the movable division plates abut against the first transverse end wall or the second transverse end wall of the crew rest cabin, and inthe storage position, the movable division plates are overlapped with the longitudinal walls of the fixed compartments. The invention also relates to an aircraft comprising such crew rest cabin and toa method for arranging the crew rest cabin for the aircraft.

Description

technical field [0001] The present invention relates to a crew rest cabin for an aircraft, and also relates to an aircraft including the crew rest cabin for the aircraft and a construction method for the crew rest cabin for the aircraft. Background technique [0002] The crew rest cabin is a special equipment for long-distance aircraft, which provides a short rest area for the flight attendants. The crew rest cabin is a relatively closed and private space, which should meet the requirements of ergonomic design and visual art design, making people feel warm and comfortable. [0003] The berths in the crew rest cabin take up most of the top luggage rack space, and airlines usually maximize the use of space to accommodate more passengers. Due to the limitation of the top space of the cabin, the rest compartments and berths are designed to be very narrow. The traditional bunk design divides the lounge into a fixed number of bunk areas through fixed partitions, corresponding bun...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D11/00
CPCB64D11/0023B64D2011/0076B64D2011/0046
Inventor 宋宏远庄多多穆玫竹吴佳茜蔡瑞虹
Owner COMAC
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