Co-cured anti-UV glass fiber coated composites for aircraft wing fuel tank components
Co-cured anti-UV glass fiber coated composites for aircraft wing fuel tank components
- Neue Suche nach: ACKERMAN PATRICK K
- Neue Suche nach: MILLER MICHAEL D
- Neue Suche nach: POWERS JAMES A
- Neue Suche nach: ACKERMAN PATRICK K
- Neue Suche nach: MILLER MICHAEL D
- Neue Suche nach: POWERS JAMES A
The invention relates to a co-cured anti-UV glass fiber coated composite material for an aircraft wing fuel tank assembly. UV degradation resistant composites for use in UV/visible light resistant vehicle fuel tank assemblies are disclosed by providing a co-cured composite substrate co-cured with a UV/visible light resistant glass fiber layer to form a co-cured composite, imparting UV/visible light resistant properties exclusively to the co-cured composite substrate.
本发明的标题为“用于飞行器翼燃料箱组件的共固化抗UV玻璃纤维涂覆的复合材料”。通过提供共固化复合材料基材与抗UV/可见光玻璃纤维层共固化以形成共固化复合材料，专有地对共固化复合材料基材赋予抗UV/可见光特性而公开了防UV降解的复合材料，其用于抗UV/可见光运载工具燃料箱组件。
Dokumentinformationen
Co-cured anti-UV glass fiber coated composites for aircraft wing fuel tank components
用于飞行器翼燃料箱组件的共固化抗UV玻璃纤维涂覆的复合材料
2023-10-17
Patent
Elektronische Ressource
Chinesisch
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