High-flame-retardant civil aviation passenger plane interior fabric
Through multi-layer structural design and the application of high-performance materials, the problems of flame retardancy, antibacterial properties, sound insulation, durability and temperature control of traditional civil aircraft interior fabrics have been solved. This has achieved a comprehensive improvement in high flame retardancy, antibacterial properties, sound insulation and durability, meeting the stringent requirements of aviation materials, improving passenger safety and comfort, extending service life and reducing noise transmission, and meeting the requirements of environmental protection and sustainable development.
Patent Information
- Application Number
- CN202422948398.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-30
- Publication Date
- 2025-12-02
- Estimated Expiration
- 2034-11-30
AI Technical Summary
Traditional civil aircraft interior fabrics have insufficient flame retardant properties, limited antibacterial properties, poor sound insulation, poor durability, and lack temperature control functions, failing to meet the safety, comfort, and durability requirements of high-altitude flight environments.
It adopts a multi-layer structure design, including an anti-static outermost layer, a core layer, and a back support layer. Each layer is responsible for flame retardancy, antibacterial properties, sound insulation, temperature control, and UV protection. The core layer contains a flame retardant layer, an antibacterial layer, and a sound insulation layer. The back support layer contains a support lining, a reinforced tear-resistant layer, a temperature control layer, and a UV protection layer. It uses a combination of materials such as high flame retardant polyester fiber, antiviral fiber, polyurethane foam, phase change materials, and UV absorbers.
It achieves comprehensive improvements in high flame retardancy, antibacterial properties, sound insulation, durability, and temperature control, meeting the stringent requirements of aviation materials, enhancing passenger safety and comfort, extending service life, and reducing noise transmission, thus complying with environmental protection and sustainable development requirements.
Smart Images

Figure CN223618405U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of civil aviation passenger aircraft interior fabric technology, and in particular to a high flame-retardant civil aviation passenger aircraft interior fabric. Background Technology
[0002] With the rapid development of the air transport industry, the performance requirements for passenger aircraft interior materials are increasing. As an important component of civil aircraft, interior fabrics not only serve a decorative function but also need to meet stringent requirements for safety, comfort, and durability. Especially in the high-altitude flight environment, the performance of materials directly affects the safety and comfort experience of passengers.
[0003] Traditional interior fabrics for commercial airliners are typically made of ordinary fibers or composite materials. While these fabrics offer some decorative appeal, they exhibit significant drawbacks under high-intensity use and in complex environments:
[0004] Insufficient flame retardancy: Ordinary fabrics are easily flammable in high-temperature or open-flame environments, failing to meet the stringent flame retardancy standards of the international aviation industry, which may lead to the rapid spread of fire.
[0005] Limited antibacterial properties: As a high-density, enclosed space, the cabin is highly susceptible to the growth of bacteria and viruses. Traditional fabrics lack effective antibacterial properties and cannot meet the high standards of hygiene required.
[0006] Poor sound insulation: There are many noise sources inside and outside the aircraft cabin, such as engine noise and aerodynamic noise. Traditional interior fabrics are not good at noise reduction, which affects the passenger's riding experience.
[0007] Poor durability: With long-term use, traditional fabrics are prone to aging, tearing, or losing strength due to ultraviolet radiation, affecting their service life.
[0008] Lack of temperature control: The temperature in the cabin environment varies greatly, and ordinary fabrics are difficult to adapt to these changes, which may cause discomfort to passengers.
[0009] Therefore, it is essential to invent a highly flame-retardant interior fabric for civil aircraft. Utility Model Content
[0010] To address the aforementioned technical problems, this utility model provides a high flame-retardant civil aircraft interior fabric, solving the issues of insufficient flame-retardant performance, limited antibacterial properties, poor sound insulation, poor durability, and lack of temperature control in existing civil aircraft interior fabrics. The high flame-retardant civil aircraft interior fabric includes an antistatic outer layer, a core layer, an inner middle layer, a back support layer, and a protective edge seal. The core layer is sewn below the antistatic outer layer, and the inner middle layer is sewn below the core layer. The back support layer is sewn below the inner middle layer. The protective edge seal is sewn onto the outermost sides of the antistatic outer layer, core layer, inner middle layer, and back support layer.
[0011] The core layer includes a flame-retardant layer, an antibacterial layer, and a sound-insulating layer, with the antibacterial layer heat-sealed below the flame-retardant layer and the sound-insulating layer heat-sealed below the antibacterial layer; the core layer is sewn between the outermost antistatic layer and the middle inner layer.
[0012] The back support layer includes a support liner, a reinforced tear-resistant layer, a temperature-regulating layer, and a UV-protective layer. The support liner is sewn with yarn below the middle inner layer, and the reinforced tear-resistant layer is sewn with yarn below the support liner. The temperature-regulating layer is sewn with yarn below the reinforced tear-resistant layer, and the UV-protective layer is sewn with yarn below the temperature-regulating layer.
[0013] The flame-retardant layer inside the core layer is a fabric woven from highly flame-retardant polyester fiber yarn; the antibacterial layer is an antiviral fiber made by embedding antiviral silver into a polymer through chemical spinning, and then forming an antibacterial fabric through weaving; the sound insulation layer is a sound insulation material made by heating polyurethane foam to a certain temperature and then applying pressure to form it, and has the following functions: ① Flame retardant function: The flame-retardant layer of the core layer plays a role in inhibiting the spread of fire, which meets the strict flame retardant requirements of civil aviation for aviation materials. This helps to reduce the spread of flames in the event of a fire, improve safety, and the flame-retardant layer can quickly reduce the burning rate when it encounters a fire source, and even self-extinguish to a certain extent, preventing the fire from spreading in the cabin and ensuring passenger safety; ② Antibacterial function: The core layer... The antibacterial layer of the core layer effectively inhibits the growth of bacteria and viruses, ensuring the hygiene of the cabin environment and preventing bacterial growth and cross-infection. Especially in high-traffic public areas, the antibacterial layer provides long-term antibacterial effects through the embedding of silver ions or other antiviral components, effectively inhibiting the growth of common bacteria such as Escherichia coli and Staphylococcus aureus, thereby reducing the spread of diseases; ③ Sound insulation: The sound insulation layer of the core layer helps reduce the transmission of external noise and improve passenger comfort. The sound insulation layer is particularly important for long-haul flights, as it can reduce engine noise, cabin noise, etc., and improve the overall riding experience. This layer uses materials such as polyurethane foam, which can effectively absorb sound and vibration, reduce noise transmission, and create a quieter cabin environment.
[0014] The inner support layer of the back support layer is made of a non-woven fabric; the reinforced tear-resistant layer is made of an aramid fabric; the temperature-controlling layer is formed by embedding or encapsulating phase change materials inside the textile fabric using a phase change material embedding method; the UV-protective layer is formed by coating the textile fabric with a UV absorber to block UV rays, and has the following functions: ① Support function: The support lining provides basic support for the entire fabric, ensuring the stability and durability of the fabric, preventing damage when the fabric is deformed or under pressure, and providing a solid foundation so that the fabric maintains its shape during use, enhancing the overall structural integrity of the fabric; ② Enhanced tear resistance function: The reinforced tear-resistant layer enhances the tear resistance of the fabric, preventing the fabric from breaking under strong tension or external impact, and improving the durability of the fabric. ① **Strength and Durability:** By using high-strength materials such as aramid fabrics, the tensile and tear resistance of the fabric is enhanced, ensuring its stability under extreme conditions and extending its service life. ② **Temperature Control:** The temperature control layer helps regulate temperature, providing a comfortable environment and preventing excessively high or low temperatures, thus improving the passenger experience. By using phase change materials, the temperature control layer can absorb or release heat when the ambient temperature changes, regulating the fabric temperature and maintaining a suitable cabin temperature for increased comfort. ③ **UV Protection:** The UV protection layer blocks ultraviolet rays, protecting the underlying structure from UV damage. By coating with UV absorbers or adding UV-shielding materials, the UV protection layer effectively prevents UV rays from penetrating the fabric, protecting the structure, such as aircraft seats, from UV damage and extending the lifespan of the aircraft.
[0015] Compared with the prior art, the present invention has the following beneficial effects:
[0016] 1. The core layer of this utility model has the following functions: ① Flame retardant function: The flame retardant layer of the core layer inhibits the spread of fire, meeting the strict flame retardant requirements of civil aviation for aviation materials. This helps to reduce the spread of flames and improve safety in the event of a fire. The flame retardant layer can quickly reduce the burning rate when it encounters a fire source, and even self-extinguish to a certain extent, preventing the fire from spreading in the cabin and ensuring passenger safety; ② Antibacterial function: The antibacterial layer of the core layer can effectively inhibit the growth of bacteria and viruses, ensuring the hygiene of the cabin environment and avoiding bacterial growth and cross-infection. Especially in high-traffic public places, the antibacterial layer provides long-term antibacterial effect through the embedding of silver ions or other antiviral components, effectively inhibiting the growth of common bacteria such as Escherichia coli and Staphylococcus aureus, thereby reducing the spread of diseases;
[0017] ③ Sound insulation: The sound insulation layer of the core layer helps reduce the transmission of external noise and improve passenger comfort. The sound insulation layer is especially important for long-haul flights, as it can reduce engine noise, cabin noise, etc., and improve the overall riding experience. This layer uses materials such as polyurethane foam, which can effectively absorb sound and vibration, reduce the transmission of noise, and create a quieter cabin environment.
[0018] 2. The back support layer of this utility model has the following functions: ① Support function: The support layer provides basic support for the entire fabric, ensuring the stability and durability of the fabric, preventing damage when the fabric is deformed or under pressure, and providing a solid foundation so that the fabric maintains its shape during use and enhances the overall structural integrity of the fabric; ② Enhanced tear resistance:
[0019] The enhanced tear-resistant layer strengthens the fabric's tear resistance, preventing it from tearing under strong tension or impact, thus improving its durability. By using high-strength materials such as aramid fabrics, the tensile and tear resistance of the fabric is enhanced, ensuring its stability under extreme conditions and extending its service life. ③ Temperature control: The temperature control layer helps regulate temperature, providing a comfortable environment and preventing excessively high or low temperatures, improving the passenger experience. By using phase change materials, the temperature control layer absorbs or releases heat when the ambient temperature changes, regulating the fabric temperature and maintaining a suitable cabin temperature for increased comfort. ④ UV protection: The UV-protective layer blocks ultraviolet rays, protecting the underlying structure from UV damage. By coating with UV absorbers or adding UV-shielding materials, the UV-protective layer effectively prevents UV rays from penetrating the fabric, protecting the structure, such as aircraft seats, from UV damage and extending the structure's lifespan. Attached Figure Description
[0020] Figure 1 This is a schematic diagram of the structure of this utility model.
[0021] Figure 2 This is a schematic diagram of the core layer of this utility model.
[0022] Figure 3 This is a schematic diagram of the back support layer of this utility model.
[0023] In the picture:
[0024] The outermost layer is antistatic, the core layer is core, the flame retardant layer is flame retardant, the antibacterial layer is antibacterial, the sound insulation layer is sound insulation, the middle inner layer is middle, the back support layer is back support, the support lining is support, the reinforced tear-resistant layer is reinforced, the temperature control layer is temperature control, the UV protection layer is UV protection, and the protective edge seal is protective. Detailed Implementation
[0025] To enable those skilled in the art to better understand the present invention, the technical solutions in the embodiments of the present invention will be clearly and completely described below. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort should fall within the protection scope of the present invention.
[0026] As attached Figure 1 To be continued Figure 3 As shown.
[0027] This utility model provides a high flame-retardant civil aircraft interior fabric, comprising an antistatic outermost layer 1, a core layer 2, an inner middle layer 3, a back support layer 4, and a protective edge seal 5. The core layer 2 is sewn below the antistatic outermost layer 1, and the inner middle layer 3 is sewn below the core layer 2. The back support layer 4 is sewn below the inner middle layer 3. The protective edge seal 5 is sewn onto the outermost sides of the antistatic outermost layer 1, core layer 2, inner middle layer 3, and back support layer 4.
[0028] The core layer 2 includes a flame-retardant layer 21, an antibacterial layer 22, and a sound-insulating layer 23, with the antibacterial layer 22 heat-sealed below the flame-retardant layer 21 and the sound-insulating layer 23 heat-sealed below the antibacterial layer 22; the core layer 2 is sewn between the outermost antistatic layer 1 and the middle inner layer 3.
[0029] The back support layer 4 includes a support liner 41, a reinforced tear-resistant layer 42, a temperature control layer 43, and a UV protection layer 44. The support liner 41 is sewn with yarn below the middle inner layer 3, and the reinforced tear-resistant layer 42 is sewn with yarn below the support liner 41. The temperature control layer 43 is sewn with yarn below the reinforced tear-resistant layer 42, and the UV protection layer 44 is sewn with yarn below the temperature control layer 43.
[0030] The flame-retardant layer 21 inside the core layer 2 is a layer of fabric woven from high flame-retardant polyester fiber yarn; the antibacterial layer 22 is an antiviral fiber made by embedding silver, an antiviral component, into a polymer through chemical spinning process, and is woven into an antibacterial fabric; the sound insulation layer 23 is a sound insulation material made by heating polyurethane foam to a certain temperature and then applying pressure to form it.
[0031] The support lining 41 inside the back support layer 4 is made of a non-woven fabric; the reinforced tear-resistant layer 42 is made of an aramid fabric; the temperature control layer 43 is formed by embedding or encapsulating phase change material inside the textile fabric using a phase change material embedding method; and the UV protection layer 44 is formed by coating a UV absorber onto the textile fabric to form a UV-blocking fabric.
[0032] A new type of high flame-retardant interior fabric for civil aircraft has the following significant advantages over existing technologies:
[0033] 1. Multi-layered structural design, comprehensive functions
[0034] The fabric adopts a multi-layer structure consisting of an anti-static outermost layer 1, a core layer 2, an inner middle layer 3, a back support layer 4, and a protective edge sealing layer 5. Each layer has been optimized for civil aviation needs and performs different functions to ensure the improvement of the overall performance of the fabric.
[0035] Advantages: Compared to traditional single-function fabrics, this multi-layer structure can simultaneously meet multiple requirements such as flame retardancy, antibacterial properties, sound insulation, temperature control, and UV protection, providing all-round protection for the cabin.
[0036] 2. Superior flame retardant properties
[0037] The flame-retardant layer 21 of the core layer 2 is made of high flame-retardant polyester fiber, which has a high ignition point and does not produce toxic gases when burning, meeting strict aviation flame-retardant standards.
[0038] Advantages: Compared to ordinary flame-retardant materials, high flame-retardant polyester fiber materials are more environmentally friendly, safer, and have stable performance, and can maintain their integrity even in high-temperature environments.
[0039] 3. Innovative antibacterial function
[0040] The antibacterial layer 22 of the core layer 2 is embedded with antiviral components such as silver through chemical spinning process, which has a long-lasting antibacterial effect and a highly effective inhibitory effect on a variety of bacteria and viruses.
[0041] Advantages: Compared to existing antibacterial technologies, this antibacterial layer is more durable and can maintain its antibacterial effect for a long time without the need for additional coatings, improving cabin hygiene and making it especially suitable for high-traffic civil aviation environments.
[0042] 4. Excellent sound insulation
[0043] The sound insulation layer 23 of the core layer 2 is made of polyurethane foam material, which is formed by heating and pressing, and has excellent sound absorption and noise reduction capabilities.
[0044] Advantages: Compared with traditional sound insulation materials, the sound insulation layer 23 is lighter and has stronger sound insulation performance, which can effectively reduce engine noise and cabin noise, and improve passenger comfort.
[0045] 5. Enhanced back support and improved durability
[0046] The back support layer 4 adopts a combination design of support liner 41, reinforced tear-resistant layer 42, temperature control layer 43 and UV protection layer 44, which respectively provide structural support, tear resistance, temperature change protection and UV protection functions.
[0047] Advantages: This design significantly improves the durability and protective capabilities of the fabric, especially in extreme environments such as strong ultraviolet radiation and high-frequency use, where it can still maintain good performance.
[0048] 6. Temperature control function
[0049] The temperature control layer 43 of the back support layer 4 uses phase change material embedding technology to absorb or release heat according to changes in ambient temperature, thus maintaining the temperature comfort of the fabric.
[0050] Advantages: Compared to traditional materials that passively regulate temperature, this temperature-regulating layer can actively regulate temperature, improving passenger comfort.
[0051] 7. Enhanced UV protection
[0052] The UV protection layer 44 of the back support layer 4 is coated with a UV absorber, which can block UV penetration and protect the body structure under the fabric, such as an airplane seat, from UV damage.
[0053] Advantages: Compared to traditional fabrics, this UV-protective layer effectively extends the lifespan of both the fabric and the machine's structure.
[0054] 8. Lightweight overall design
[0055] Each layer of material achieves lightweight design while ensuring functionality.
[0056] Advantages: Compared to traditional interior materials, this fabric is lighter, which helps reduce the overall weight of the aircraft, thereby improving fuel efficiency and operating economy.
[0057] 9. Environmental Protection and Sustainability
[0058] Most of the materials used are recyclable, and the production process reduces the emission of harmful substances.
[0059] Advantages: It meets the current high requirements of the civil aviation industry for green environmental protection and sustainable development.
[0060] Comprehensive comparison:
[0061] This highly flame-retardant civil aircraft interior fabric, through multi-layered innovative design and the application of high-performance materials, significantly improves flame retardancy, comfort, and durability, while also taking into account environmental friendliness and economic benefits, and has obvious comprehensive advantages compared to existing technologies.
[0062] Any technical solution that achieves the above-mentioned technical effects by utilizing the technical solution described in this utility model, or by designing a similar technical solution inspired by the technical solution described in this utility model, falls within the protection scope of this utility model.
Claims
1. A high flame-retardant interior fabric for civil aircraft, characterized in that: The structure includes an outermost antistatic layer (1), a core layer (2), an inner middle layer (3), a back support layer (4), and a protective edge seal (5). The core layer (2) is sewn with yarn below the outermost antistatic layer (1), and the inner middle layer (3) is sewn with yarn below the core layer (2). The back support layer (4) is sewn with yarn below the inner middle layer (3). The protective edge seal (5) is sewn with yarn on the outermost sides of the outermost antistatic layer (1), the core layer (2), the inner middle layer (3), and the back support layer (4). The core layer (2) includes a flame-retardant layer (21), an antibacterial layer (22), and a sound-insulating layer (23). The antibacterial layer (22) is heat-sealed below the flame-retardant layer (21), and the sound-insulating layer (23) is heat-sealed below the antibacterial layer (22). The core layer (2) is sewn between the outermost antistatic layer (1) and the inner middle layer (3).
2. The high flame-retardant civil aircraft interior fabric as described in claim 1, characterized in that: The back support layer (4) includes a support liner (41), a reinforced tear-resistant layer (42), a temperature control layer (43), and a UV protection layer (44). The support liner (41) is sewn with yarn below the middle inner layer (3), and the reinforced tear-resistant layer (42) is sewn with yarn below the support liner (41). The temperature control layer (43) is sewn with yarn below the reinforced tear-resistant layer (42), and the UV protection layer (44) is sewn with yarn below the temperature control layer (43).
3. The high flame-retardant civil aircraft interior fabric as described in claim 1, characterized in that: The flame-retardant layer (21) inside the core layer (2) is a layer of fabric woven from high flame-retardant polyester fiber yarn; the antibacterial layer (22) is an antiviral fiber made by embedding silver, an antiviral component, into a polymer through chemical spinning process, and is woven into an antibacterial fabric; the sound insulation layer (23) is a sound insulation material made by heating polyurethane foam to a certain temperature and then applying pressure to form it.
4. The high flame-retardant civil aircraft interior fabric as described in claim 2, characterized in that: The support lining (41) inside the back support layer (4) is made of a non-woven fabric; the reinforced tear-resistant layer (42) is made of an aramid fabric; the temperature control layer (43) is formed by embedding or encapsulating phase change material inside the textile fabric using a phase change material embedding method; the UV protection layer (44) is formed by coating a UV absorber onto the textile fabric to form a UV-blocking fabric.