FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Structure 1 has zone 4, 4' to receive component of pipeline system 2. Said zone 4, 4' has access in several sections outside of aircraft or spacecraft sections 3 for mounting and/or maintenance of pipeline system 2. Structure 1 comprises sealing separator 11, 12 for tight separation of receiving zone 4, 4' from inner space 9, 10 of fuselage 3. Said zone is designed for internal pressure corresponding to external pressure of fuselage 3 and is located outside of the zone of impact 17 of fuselage 3. Invention covers also aircraft or spacecraft with appropriate structure.
EFFECT: reduced labor input in servicing.
11 cl, 4 dwg
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|
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