Shrouded fluid-conducting apparatus
AssigneeThe Boeing Company
InventorsJames A. Carns, Theron L. Cutler, Mark A. Shelly
Life of this patent
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AssigneeThe Boeing Company
InventorsJames A. Carns, Theron L. Cutler, Mark A. Shelly
Estimating the term…
A shrouded fluid-conducting apparatus is provided that includes at least one outer conduit and at least one inner conduit disposed within the outer conduit. Preferably, the shrouded fluid-conducting apparatus further includes at least one shrouded end fitting disposed at an end of the shrouded fluid-conducting apparatus and at least one support member engaged with the inner and outer conduits. The shrouded end fitting allows the shrouded fluid-conducting apparatus to be engaged with an additional shrouded fluid-conducting apparatus. The support member allows for the transfer of loads from the inner and/or outer conduits to one or more components external to the shrouded fluid-conducting apparatus. Accordingly, the shrouded-fluid conducting apparatus may be used to transport fuel through an aircraft “ignition zone” in an FAA-compliant manner.
A shrouded fluid-conducting apparatus, comprising:
A shrouded fluid-conducting apparatus, comprising:
A shrouded fluid-conducting apparatus, comprising:
A shrouded fluid-conducting apparatus, comprising:
A shrouded end fitting, comprising:
A method of making a shrouded fluid-conducting apparatus, the method comprising:
A method of conducting fluid, the method comprising:
A method of conducting fluid, the method comprising:
Dependencies are inferred from the claim text.