System and methods for distributing loads from fluid conduits, including aircraft fuel conduits
First Claim
1. An aircraft, comprising:
- a fuselage portion;
a wing portion;
a spar carried by at least one of the fuselage portion and the wing portion, the spar including a first spar rib and a second spar rib spaced apart from the first spar rib;
a fuel tank carried by at least one of the fuselage portion and the wing portion;
a fluid conduit proximate to the spar and operably coupled to the fuel tank; and
a support member carrying the fluid conduit, the support member being operably coupled to the spar and positioned to transfer at least approximately all of the axial loads from the fluid conduit to at least one of the first spar rib and the second spar rib.
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Accused Products
Abstract
Systems and methods for distributing loads from fluid conduits, including aircraft fuel conduits, are disclosed. An aircraft configured in accordance with one embodiment of the invention includes a fuselage portion, a wing portion, and a fuel tank carried by least one of the fuselage portion and the wing portion. The aircraft also includes a spar carried by at least one of the fuselage portion and the wing portion. The spar includes a first spar rib and a second spar rib spaced apart from the first spar rib. The aircraft further includes a fluid conduit proximate to the spar and operably coupled to the fuel tank. A support member carrying the fluid conduit is operably coupled to the spar. The support member can be positioned to transfer at least approximately all of the axial loads from the fluid conduit to at least one of the first spar rib and the second spar rib.
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Citations
25 Claims
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1. An aircraft, comprising:
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a fuselage portion;
a wing portion;
a spar carried by at least one of the fuselage portion and the wing portion, the spar including a first spar rib and a second spar rib spaced apart from the first spar rib;
a fuel tank carried by at least one of the fuselage portion and the wing portion;
a fluid conduit proximate to the spar and operably coupled to the fuel tank; and
a support member carrying the fluid conduit, the support member being operably coupled to the spar and positioned to transfer at least approximately all of the axial loads from the fluid conduit to at least one of the first spar rib and the second spar rib. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. A fluid transmission system, comprising:
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a first support member having a web portion, a first rib extending outwardly generally normal to the web portion, and a second rib spaced apart from the first rib and extending outwardly generally normal to the web portion;
a fluid conduit having a first end and a second end spaced apart from the first end, the first end including a first coupling positioned for attachment to the first support member and the second end including a second coupling positioned for engagement with a corresponding coupling of another fluid conduit; and
a second support member carrying the fluid conduit, the second support member being operably coupled to the first support member and positioned to transfer (a) at least approximately all the axial loads from the fluid conduit to at least one of the first rib and the second rib of the first support member, and (b) at least approximately all the shear loads from the first coupling to the web portion of the first support member. - View Dependent Claims (13, 14, 15, 16, 17, 18)
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19. A method for distributing loads from a fluid conduit, the method comprising:
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attaching a support member to a fluid conduit;
attaching the support member and fluid conduit to a spar, the spar including a first spar rib and a second spar rib spaced apart from the first spar rib; and
transferring at least approximately all the axial loads of the fluid conduit from the support member to at least one of the first spar rib and the second spar rib. - View Dependent Claims (20, 21, 22, 23, 24, 25)
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Specification