Support structure for an aircraft
A support structure for an aircraft includes a structural member having a generally planar shape, a longitudinal axis defining a longitudinal direction and a transverse axis orthogonal to the longitudinal axis, and a plurality of rounded holes formed along the longitudinal direction. Each rounded hole has a respective major axis with a major length and a minor axis orthogonal to the major axis with a minor length that is less than the major length. Each rounded hole is oriented with its major axis rotated more than 0 degrees and less than 90 degrees from the longitudinal axis of the structural member. The structural member is configured for bearing external loads acting on the structural member in a principal loading direction that is not parallel with the longitudinal axis or the transverse axis. Each rounded hole may be oriented with its major axis aligned generally parallel with the principal loading direction.
1 . A support structure of an aircraft having a wing, the support structure comprising:
a wingbox rib structurally configured to attach to the wing of the aircraft, the wingbox rib including a structural member having a generally planar shape, a fore-aft length, a vertical height orthogonal to and smaller than the fore-aft length, a longitudinal axis parallel to the fore-aft length, and a transverse axis orthogonal to the longitudinal axis and parallel to the vertical height; and
a plurality of rounded holes formed in the structural member and spaced from each other along the longitudinal axis, wherein the rounded holes are configured to allow one or more of a hydraulic line, an electrical line, or a fuel line to pass therethrough, wherein each of the rounded holes has a respective major axis with a major length therealong and a minor axis orthogonal to the major axis with a minor length therealong that is less than the major length,
wherein each of the rounded holes is oriented with its major axis rotated more than 0 degrees and less than or equal to 45 degrees from the longitudinal axis of the structural member.
2 . The support structure of claim 1 , wherein each of the rounded holes has a shape including a Grodzinski-profiled hole.
3 . The support structure of claim 1 , wherein the generally planar shape of the structural member is flat and the longitudinal axis of the structural member is straight.
4 . The support structure of claim 1 , wherein each of the rounded holes is oriented with its minor axis rotated counterclockwise more than 0 degrees and less than 45 degrees from the transverse axis of the structural member.
5 . The support structure of claim 1 , wherein the wingbox rib is flat.
6 . The support structure of claim 5 , wherein the wingbox rib has curved edges, and wherein each of the rounded holes is an access hole through the wingbox rib.
7 . The support structure of claim 1 , wherein the structural member is configured for bearing one or more external loads acting on the structural member in a principal loading direction that is not parallel with the longitudinal axis or the transverse axis, and wherein each of the rounded holes is oriented with its major axis rotated more than 0 degrees and less than or equal to 45 degrees from the principal loading direction.
8 . The support structure of claim 1 , wherein the structural member is configured for bearing one or more external loads acting on the structural member in a principal loading direction that is not parallel with the longitudinal axis or the transverse axis, and wherein each of the rounded holes is oriented with its major axis aligned parallel with the principal loading direction.
9 . The support structure of claim 8 , wherein the structural member includes a plurality of attachment points configured for interfacing with one or more external members and for receiving the one or more external loads from the external members.
10 . The support structure of claim 1 , wherein the major axis of each of the plurality of rounded holes is aligned and parallel with a principal loading direction, wherein the minor axis of each of the plurality of rounded holes is aligned and parallel with a transverse axis, and perpendicular to the principal loading direction.
11 . A support structure of an aircraft having a wing, the support structure comprising:
a wingbox rib structurally configured to mount inside the wing of the aircraft, the wingbox rib including a structural member having a generally planar shape, a fore-aft length, a vertical height orthogonal to and smaller than the fore-aft length, a longitudinal axis parallel to the fore-aft length, and a transverse axis orthogonal to the longitudinal axis and parallel to the vertical height, wherein the structural member includes a plurality of attachment points configured for interfacing with one or more external members and for receiving one or more external loads from the external members acting on the structural member in a principal loading direction that is not parallel with the longitudinal axis or the transverse axis; and
a plurality of rounded holes formed in the structural member and spaced from each other along the longitudinal axis, wherein the rounded holes are configured to allow one or more of a hydraulic line, an electrical line, or a fuel line to pass therethrough, wherein each of the rounded holes has a respective major axis with a major length therealong and a minor axis orthogonal to the major axis with a minor length therealong that is less than the major length,
wherein each of the rounded holes is oriented with its major axis rotated 45 degrees or less from the longitudinal axis and aligned parallel with the principal loading direction.
12 . The support structure of claim 11 , wherein each of the rounded holes has a shape including an ellipse, a Grodzinski-profiled hole, an oval, a rounded rectangle, a stadium, a rounded rhombus or a rounded trapezoid.
13 . The support structure of claim 11 , wherein the generally planar shape of the structural member is flat and the longitudinal axis of the structural member is straight.
14 . The support structure of claim 11 , wherein each of the rounded holes has an oval or elliptical shape.
15 . The support structure of claim 11 , wherein the wingbox rib is generally flat, and wherein each of the rounded holes is an access hole through the wingbox rib.
16 . The support structure of claim 15 , wherein the wingbox rib has curved edges.
17 . An aircraft, comprising: an
aircraft fuselage;
an aircraft wing attached to the aircraft fuselage;
a wingbox rib attached to the aircraft wing, the wingbox rib including a structural member having a generally planar shape, a fore-aft length, a vertical height orthogonal to and smaller than the fore-aft length, a longitudinal axis parallel to the fore-aft length, and a transverse axis orthogonal to the longitudinal axis and parallel to the vertical height, wherein the structural member includes a plurality of attachment points configured for interfacing with one or more external members and for receiving one or more external loads from the external members acting on the structural member in a principal loading direction that is not parallel with the longitudinal axis or the transverse axis; and
a plurality of elliptical holes formed in the structural member and spaced from each other along the longitudinal axis, wherein the elliptical holes are configured to allow one or more of a hydraulic line, an electrical line, or a fuel line to pass therethrough, wherein each of the elliptical holes has a respective major axis with a major length therealong and a minor axis orthogonal to the major axis with a minor length therealong that is less than the major length,
wherein each of the elliptical holes is oriented with its major axis rotated 45 degrees or less from the longitudinal axis and aligned parallel with the principal loading direction, and
wherein each of the elliptical holes is an access hole through the wingbox rib.
18 . The aircraft of claim 17 , wherein each of the elliptical holes has a respective shape, and each respective shape is an ellipse, a Grodzinski-profiled hole, or an oval.
19 . The aircraft of claim 17 , wherein the generally planar shape of the structural member is flat and the longitudinal axis of the structural member is straight.
20 . The aircraft of claim 17 , wherein each of the elliptical holes is oriented with its major axis rotated more than 0 degrees and less than or equal to 45 degrees from the principal loading direction.
21 . The aircraft of claim 17 , wherein the wingbox rib is generally flat with curved edges.