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Seat fastening system, seat or seat set and fastening method thereof, aircraft cockpit

一种航空器、紧固元件的技术,应用在座椅的布置、飞机配件、飞机零件等方向,能够解决结构繁复、组装费时、燃油损耗增加等问题,达到简单迅速安装、提高便利性、便于维修的效果

Active Publication Date: 2018-11-27
AIRBUS DEFENCE & SPACE GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This in turn creates weight gain and leads to increased fuel consumption
Due to the top of the holes, the fastening elements are skewed in the crosspieces, which leads to complex construction and time-consuming assembly
Furthermore, the flexibility in the aircraft cockpit is limited due to the rungs

Method used

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  • Seat fastening system, seat or seat set and fastening method thereof, aircraft cockpit
  • Seat fastening system, seat or seat set and fastening method thereof, aircraft cockpit
  • Seat fastening system, seat or seat set and fastening method thereof, aircraft cockpit

Examples

Experimental program
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Embodiment Construction

[0046] exist figure 1 , figure 2 and Figure 10 The middle figure shows a seat fastening system 10 for fastening a seat or seat set 12 of an aircraft, in particular an airplane, to an aircraft component, in particular an aircraft cabin.

[0047] The seat fastening system 10 has a plurality of rectangular mounting plates 14 adjoining at their long sides and fastening modules 16 for securing seat packages 12 to the mounting plates 14, in particular two per seat or seat package 12. A fastening module 16.

[0048] Especially as figure 1 , figure 2 and Figure 7-10 As shown, each mounting plate 14 has a plurality of connection points 18 for securing fastening modules 16 . The connection points 18 form two parallel rows of holes 20 on each mounting plate, wherein each hole row 20 is formed by three connection points 18 . The mounting plate 14 is made of fiber-reinforced plastic.

[0049] Each connection point 18 is constituted by a connection piece 22 (also known as an inser...

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PUM

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Abstract

The invention relates to a seat fastening system, a seat or a seat set, an aircraft cabin and a method for fastening a seat or a seat set. In order to reduce weight, simplify the assembly of seats or seat sets and increase the flexibility of the cockpit, the present invention provides a seat fastening system (10) for an aircraft seat or seat set (12) with There is at least one mounting plate (14) for attaching the seat or seat package (12) to an aircraft component of the aircraft and at least one mounting plate (14) for securing the seat or seat package (12) to the mounting plate (14) Fasten the module (16).

Description

technical field [0001] The invention relates to a seat fastening system for an aircraft seat or seat kit, in particular an aircraft. Furthermore, the invention relates to a seat or a seat set for an aircraft with at least one such seat fastening system. Furthermore, the invention also relates to an aircraft cabin of an aircraft, in particular an aircraft cabin. Finally, the invention also relates to a method for fastening a seat or a seat set of an aircraft, in particular an airplane, to an aircraft component by means of such a seat fastening system. Background technique [0002] Seats or seat sets (also called benches) of an aircraft, in particular an airplane, are fastened in the aircraft cabin by means of seat rails installed in the floor of the aircraft cabin. The seat rail is equipped with a perforated top that includes equally spaced perforations along the top. The positioning of the seat or the seat package inside the aircraft cabin is effected by means of the slot...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D11/06
CPCB64C1/18B64F5/10B64D11/0696Y02T50/40
Inventor 亚武兹·托克塔斯帕特里克·罗尔芬克
Owner AIRBUS DEFENCE & SPACE GMBH
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