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Flexible support and to receiving device

A flexible support and containment device technology, used in transportation and packaging, aircraft parts, sleepers, etc., to solve problems such as not very strong, completely broken, and crib matching

Active Publication Date: 2021-07-23
苏州华瑞腾航空设备有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Existing cribs, in this case, are not inherently very strong, so through mishandling or excessive force, the brackets can quickly wear out, bend, snap off completely
The cot is then no longer suitable for further use, resulting in obstruction of the corresponding occupant
Also, in this case, the airline has to order a replacement part, but the aviation industry is already known to have enormous cost pressures
[0004] Also, with possible tolerance deviations in the mounting joints, existing cribs do not fit exactly to the outside or have to be adjusted with the aid of tools

Method used

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  • Flexible support and to receiving device
  • Flexible support and to receiving device
  • Flexible support and to receiving device

Examples

Experimental program
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Embodiment Construction

[0065] refer to figure 1 A first embodiment of the containment device is shown, comprising flexible supports 3, 3a and 4 for securing it inside the passenger transport.

[0066] The receiving device 10 has a horizontal surrounding section 1 , which in this example has a fastening section 11 and further supporting frame sections 12 , 13 and 14 . The vertical section 2 is pivotably fixed to the support frame sections 21 , 22 and 23 at swivel joints 5 , 5 a. The flexible support 3 , 3 a is arranged on the fixed section 11 and the flexible support 4 is arranged on the vertical section 2 .

[0067] figure 1 The example of FIG. 10 shows a receiving device 10 with a flexible support 6 having three support shells 3 , 3 a and 4 . The receptacle 10 can also be designed in such a way that it only has the support housing 3 , 3 a and the vertical section 2 is supported only against the corresponding section of the interior. Support feet (not shown) can be provided for this purpose. It...

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PUM

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Abstract

The invention relates to a flexible support and to a receiving device for securing the receiving device in an interior of a passenger vehicle. The flexible support comprises at least one first securing pin, which is configured for coupling with a first mounting opening arranged in the interior, and a position compensation element is further comprised; a first fastening pin is supported by the position compensation element, the position compensation element is configured to bear a transverse force component acting on the fastening pin, and the first fastening pin is configured to be movably and / or tiltably mounted on the accommodating device; therefore, a positioning error or the dimensional tolerance between the mounting openings during the mounting of the fixed accommodating device can be compensated.

Description

technical field [0001] The present invention relates to a flexible support and a containment device, in particular a flexible support and a containment device for use in a passenger vehicle such as an aircraft. Background technique [0002] In the prior art, a baby cot can be fixed in a predetermined position in an aircraft cabin so that a baby can rest therein during the flight. Such cots usually need to be stowed during the take-off and landing phases in order to avoid injury to the passengers or crew, and during this phase of flight the child must be seated in the passenger seat. Therefore, such a crib needs to perform assembly and / or disassembly and storage steps several times in only one flight, especially when the aircraft cabin is in motion. [0003] Existing cribs, in this case, are not inherently very strong, so that through improper handling or excessive force, the brackets can quickly wear out, bend, and snap off completely. The baby cot is then no longer suitab...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A47D9/00B64D11/00
CPCA47D9/005B64D11/00B64D2011/0084
Inventor 谢明星
Owner 苏州华瑞腾航空设备有限公司