LOWER JOINTS BETWEEN OUTBOARD WING BOXES AND CENTER WING SECTIONS OF AIRCRAFT WING ASSEMBLIES
First Claim
1. A wing assembly for an aircraft, the wing assembly comprising:
- a left wing box;
a right wing box;
a wing center section;
a left lower joint assembly that defines a left lower joint with the left wing box and the wing center section; and
a right lower joint assembly that defines a right lower joint between the right wing box and the wing center section;
wherein the left wing box and the right wing box are constructed substantially of a first material having a first coefficient of thermal expansion, wherein the wing center section is constructed substantially of a second material that is different from the first material and that has a second coefficient of thermal expansion that is greater than the first coefficient of thermal expansion, and wherein the left lower joint assembly and the right lower joint assembly are constructed substantially of a third material that is different from the first material and the second material and that has a third coefficient of thermal expansion that is greater than the first coefficient of thermal expansion and less than the second coefficient of thermal expansion.
1 Assignment
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Accused Products
Abstract
Lower joints of aircraft wing assemblies are disclosed. In some embodiments, a lower joint includes an outboard lower wing panel, a center lower wing panel, a rib, and a lower joint assembly that includes two outboard flanges operatively coupled to the outboard lower wing panel, an inboard flange operatively coupled to the center lower wing panel, and an upper flange operatively coupled to the rib. In some embodiments, a lower joint assembly includes one or more splice plates, an upper T-fitting, and one or more intermediate plates. In some embodiments, the outboard lower wing panel, the center lower wing panel, and the lower joint assembly are constructed substantially of different materials.
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Citations
21 Claims
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1. A wing assembly for an aircraft, the wing assembly comprising:
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a left wing box; a right wing box; a wing center section; a left lower joint assembly that defines a left lower joint with the left wing box and the wing center section; and a right lower joint assembly that defines a right lower joint between the right wing box and the wing center section; wherein the left wing box and the right wing box are constructed substantially of a first material having a first coefficient of thermal expansion, wherein the wing center section is constructed substantially of a second material that is different from the first material and that has a second coefficient of thermal expansion that is greater than the first coefficient of thermal expansion, and wherein the left lower joint assembly and the right lower joint assembly are constructed substantially of a third material that is different from the first material and the second material and that has a third coefficient of thermal expansion that is greater than the first coefficient of thermal expansion and less than the second coefficient of thermal expansion. - View Dependent Claims (2, 3, 4, 5, 6)
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7. A lower joint for a wing assembly of an aircraft, the lower joint comprising:
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an outboard lower wing panel of an outboard wing box; a center lower wing panel of a wing center section; a rib that defines an interface between the outboard wing box and the center wing section; and a lower joint assembly operatively interconnecting the outboard lower wing panel, the center lower wing panel, and the rib, wherein the joint assembly includes; two outboard flanges, wherein the outboard lower wing panel extends between the two outboard flanges in a double shear arrangement; an inboard flange operatively coupled to the center lower wing panel; and an upper flange operatively coupled to the rib. - View Dependent Claims (8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
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20. A kit for forming a lower joint assembly operable to join an outboard lower wing panel of an outboard wing box, a center lower wing panel of a wing center section, and a rib of an aircraft wing assembly, the kit comprising:
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one or more lower splice plates that defines a lower of two outboard flanges for operatively receiving the outboard lower wing panel between the two outboard flanges; an upper T-fitting that defines an upper of the two outboard flanges and an upper flange for operatively being coupled to the rib; and one or more intermediate plates for positioning between the one or more lower splice plates and the upper T-fitting, wherein the one or more intermediate plates defines an inboard flange for being coupled operatively to the center lower wing panel. - View Dependent Claims (21)
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Specification