一种阻燃型航空座椅套

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By introducing a combined structure of spandex base material, activated carbon fiber odor adsorption layer, and silicon carbide fiber flame retardant layer into the aircraft seat cover, the problems of insufficient thermal stability and flame retardant performance of the seat cover are solved, achieving efficient odor adsorption and gas purification, and improving the comfort and safety of the seat.

CN224511458UActive Publication Date: 2026-07-17JIANGSU CARNATION BUSINESS TRAVEL PROD CO LTD

Patent Information

Authority / Receiving Office: CN · China
Patent Type: Utility models(China)
Current Assignee / Owner: JIANGSU CARNATION BUSINESS TRAVEL PROD CO LTD
Filing Date: 2025-09-18
Publication Date: 2026-07-17

AI Technical Summary

Technical Problem

Existing aircraft seat covers have low thermal stability, poor flame retardant properties, and are not good at absorbing odors, affecting comfort and safety.

Method used

It adopts a combination structure of spandex material base layer, odor absorption layer and flame retardant layer. The odor absorption layer is woven from activated carbon fiber, the flame retardant layer is woven from silicon carbide fiber and coated with organosilicon resin coating, combined with adjustable tightening strap and adjustment buckle for easy fixation.

Benefits of technology

The seat covers have improved thermal stability and flame retardant properties, effectively absorb odors, purify gases, and enhance comfort and safety.

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Abstract

本实用新型涉及航空座椅套技术领域，具体的说是一种阻燃型航空座椅套，包括航空座椅套本体，所述航空座椅套本体由头部套、靠背套和座垫套组成，所述航空座椅套本体的材料组成包括氨纶材料基层，所述氨纶材料基层的顶部表层通过第二粘接层粘接有异味吸附层，所述异味吸附层的顶部表层通过第一粘接层粘接有阻燃层；所述阻燃层的两侧表层均涂覆有有机硅树脂涂层；航空座椅套热稳定性高，阻燃性能显著提高，便于吸附航空座椅套本体表面异味，净化气体。

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Claims

1. A fire-retardant aviation seat cover, characterized by, The aircraft seat cover body (1) is composed of a head cover (2), a back cover (3) and a seat cushion cover (4). The head cover (2) has silicone rubber massage protrusions (11) evenly attached to the middle part of one side. The aircraft seat cover body (1) is made of spandex material base layer (10). The top surface of the spandex material base layer (10) is bonded with an odor adsorption layer (8) through a second adhesive layer (9). The top surface of the odor adsorption layer (8) is bonded with a flame retardant layer (6) through a first adhesive layer (7), and both sides of the flame retardant layer (6) are coated with an organosilicon resin coating (13).

2. The fire-retardant aircraft seat cover according to claim 1, wherein, Both the first adhesive layer (7) and the second adhesive layer (9) are acrylic adhesives.

3. The fire-retardant aircraft seat cover according to claim 1, wherein The odor adsorption layer (8) is specifically woven from activated carbon fibers.

4. The fire-retardant aircraft seat cover of claim 1, wherein, The flame-retardant layer (6) is specifically woven from silicon carbide fibers.

5. The fire-retardant aircraft seat cover of claim 1, wherein, Both ends of the backrest cover (3) and seat cushion cover (4) are sewn with adjustable tightening straps (5), and the adjustable tightening straps (5) are provided with adjustment buckles.