作者: Theron L. Cutler , Benjamin P. Van Kampen , Mark A. Shelly , James A. Carns
DOI:
关键词: Structural engineering 、 Spar 、 Fuselage 、 Marine engineering 、 Electrical conduit 、 Engineering 、 Fuel tank 、 Wing
摘要: Systems and methods for distributing loads from fluid conduits, including aircraft fuel are disclosed. An configured in accordance with one embodiment of the invention includes a fuselage portion, wing tank carried by least portion portion. The also spar at first rib second spaced apart rib. further conduit proximate to operably coupled tank. A support member carrying is spar. can be positioned transfer approximately all axial