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Assembly of an inner fixed structure of a turbojet engine nacelle and of a thermal protection
Assembly of an inner fixed structure of a turbojet engine nacelle and of a thermal protection
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机译:涡轮喷气发动机机舱内部固定结构的组装和热保护
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摘要
The present disclosure relates to an assembly of an inner fixed structure of a turbojet engine nacelle and of a thermal protection, said structure including an inner face, on which the thermal protection is added, and an outer face constituting a portion of the inner surface of a cold flow path, the assembly including at least one channel put in fluid communication the inner face and the outer face of the structure.
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