Airplane wing, method for manufacturing an airplane wing and use of a welding process for welding a wing spar
View Patent ↗An airplane wing has a lower wing cover, an upper wing cover and a wing spar. A first end portion of the wing spar is welded to the lower wing cover and/or a second end portion of the wing spar is welded to the upper wing cover.
1. An airplane wing, comprising:
a lower wing cover;
an upper wing cover; and
a wing spar comprising a first end portion and a second end portion, each of the first end portion and the second end portion comprising a front flange and a rear flange, the front flange and the rear flange of the first end portion of the wing spar are butt welded to the lower wing cover and the front flange and the rear flange of the second end portion of the wing spar are butt welded to the upper wing cover, the welded first end portion of the wing spar comprises a part of the lower wing cover and forms a butt welded part of an outside of the airplane wing, and the welded second end portion of the wing spar comprises a part of the upper wing cover and forms a butt welded part of the outside of the airplane wing.
2. The airplane wing according to claim 1 , wherein the wing spar has a double T-shaped cross-section or a C-shaped cross-section.
3. The airplane wing according to claim 1 , further comprising an additional wing spar comprising a first end portion and a second end portion, each of the first end portion and the second end portion comprising a front flange and a rear flange.
4. The airplane wing according to claim 3 , wherein the wing spar is arranged as a front spar of the airplane wing, and the additional wing spar is arranged as a rear spar of the airplane wing, the front flanges of the front spar being connected to a slat junction,
the rear flanges of the rear spar being connected to an end box, and
the rear flanges of the front spar and the front flanges of the rear spar being connected to a center portion of the lower wing cover and the upper wing cover.
5. The airplane wing according to claim 1 , wherein the wing spar is comprised entirely of one metal or metal alloy.
6. The airplane wing according to claim 1 , wherein the wing spar comprises a first section of a first material and a second section of a second material, the first material being different from the second material.
7. The airplane wing according to claim 6 , wherein the wing spar comprises a spar web, and the first section comprises a bottom chord of the wing spar and a portion of the spar web positioned adjacent to the bottom chord, and
wherein the second section comprises a top chord of the wing spar and a portion of the spar web positioned adjacent to the top chord.
8. The airplane wing according to claim 6 , wherein the first section is comprised of a first aluminum alloy, and the second section is comprised of a second aluminum alloy different from the first aluminum alloy.
9. The airplane wing according to claim 6 , wherein the first section is welded to the second section.
10. The airplane wing according to claim 1 , further comprising at least one additional wing spar including a first end portion welded to the lower wing cover and a second end portion welded to the upper wing cover.