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Armrest structure and aircraft seat group thereof

A technology of aircraft seats and armrests, which is applied to the layout of seats and other directions, can solve the problems of hands touching each other and the distance between armrests being close to each other, and achieve the effect of solving troubles and improving the appearance

Inactive Publication Date: 2017-01-04
AIRCOM PACIFIC INC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the setting mode of this seat, the passengers on the adjacent two seats need to share the armrest between the adjacent seats mostly, or the distance between the armrests of the two seats is close, thus causing the hands of the two passengers to The parts may have the problem of touching each other
This problem has always been a big problem for passengers.

Method used

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  • Armrest structure and aircraft seat group thereof
  • Armrest structure and aircraft seat group thereof
  • Armrest structure and aircraft seat group thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0044] refer to figure 1 , 2 As shown, it is the first schematic diagram and the second schematic diagram of Embodiment 1 of the aircraft seat group of the present invention. Wherein, the aircraft seat group 100 is provided with the armrest structure 10 of the present invention for passengers to properly place their hands.

[0045] As shown in the figure, the aircraft seat set 100 includes an armrest structure 10 and an aircraft seat 20 . Wherein the number of aircraft seats 20 can be two, three or more, and the armrest structure 10 is correspondingly one, two or more. In this embodiment, two aircraft seats 20 and one armrest structure 10 are taken as an example for illustration, but it is not limited thereto.

[0046] Two aircraft seats 20 are arranged adjacently. The armrest structure 10 includes an armrest body 101 and two supporting plates 102 . The armrest body 101 is disposed between two aircraft seats 20 . The shape of the two supporting plates 102 is correspondin...

Embodiment 2

[0053] refer to Figure 4 , 5 , which are respectively the first schematic diagram and the second schematic diagram of Embodiment 2 of the aircraft seat group of the present invention. In this embodiment, the configuration of each component is similar to that of Embodiment 1, and the similarities will not be repeated here. The main difference between the present embodiment and the first embodiment lies in the transformation manner of the supporting plate 102 from the first position A to the second position B.

[0054] Furthermore, in this embodiment, the width of the supporting plate 102 can be smaller than the width of the armrest body 101 . In addition, one end of each supporting plate 102 and the other side close to the supporting plate 102 are pivotally disposed in the concave portion 1011 . Wherein, the other side of the support plate 102 refers to the side away from the seat cushion 201 of the aircraft seat 20 .

[0055] Therefore, the passenger on the aircraft seat ...

Embodiment 3

[0057] refer to Figure 6 , which is a schematic diagram of Embodiment 3 of the aircraft seat group of the present invention. In this embodiment, the configuration of each component is similar to that of the foregoing embodiments, and the similarities will not be repeated here. The main difference between this embodiment and Embodiment 1 is that the supporting plate 102 is converted from the first position A to the second position B, and the main difference from the second embodiment is that the supporting plate 102 is changed from the first position A to the second position B. After the transformation from the first position A to the second position B, the space between the two supporting plates 102 and the armrest body 101 forms an inverted T shape.

[0058] In this embodiment, the width of the supporting plate 102 may correspond to (for example be equal to) the width of the armrest body 101 . In addition, as in the previous embodiment, one end of each supporting plate 102...

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PUM

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Abstract

The invention discloses an armrest structure and an aircraft seat group thereof. The armrest structure comprises an armrest body and two bearing plates, wherein the armrest body is arranged between two adjacent aircraft seats; the shapes of the two bearing plates correspond to the armrest body, and the two bearing plates are respectively arranged on two sides of the armrest body in a pivot manner; each of the two bearing plates is provided with a first position and a second position; when the two bearing plates are located at the first positions, the two bearing plates are combined with the armrest body, so that an armrest is formed; and when the two bearing plates are located at the second positions, the two bearing plates and the armrest body are in a vertical condition, so that hands of passengers sitting on the two aircraft seats can be borne on the two bearing plates.

Description

technical field [0001] The invention relates to a seat, in particular to an armrest structure applied to transportation tools such as airplanes and an airplane seat set thereof. Background technique [0002] Usually, the seat configuration on an airplane is mostly a plurality of seats adjacent to each other, for example, two or three seats are adjacently arranged in a group near the window, and four or five seats are arranged in the middle area. or more seats are adjacently arranged as a group. In the setting mode of this seat, the passengers on the adjacent two seats need to share the armrest between the adjacent seats mostly, or the distance between the armrests of the two seats is close, thus causing the hands of the two passengers to The parts may have the problem of touching each other. This problem has always been a big problem for passengers. [0003] In view of this, the inventor of the present invention conceived and designed an armrest structure and an aircraft ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D11/06
Inventor 施允泽
Owner AIRCOM PACIFIC INC
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