Additive manufactured airframe structure having a plurality of reinforcement elements
Additive manufactured airframe structure having a plurality of additive manufactured airframe segments operable to be linked together in an assembled direction. Each of the plurality of additive manufactured airframe segments are separate from one another in an unassembled configuration. Plurality of reinforcement elements operable to be received in a receiving portion of the plurality of airframe segments and extending through the plurality of airframe segments in a normal direction. Receiving portion is located on the interior of a respective one of the plurality of airframe segments.
1. An additive manufactured airframe structure comprising:
a plurality of additive manufactured wing segments operable to be linked together in a spanwise direction, wherein each of the plurality of additive manufactured wing segments are separate from one another in an unassembled configuration, and wherein each of the plurality of additive manufactured wing segments comprises:
an outer wall that defines an airfoil cross-section and encloses an interior section therewithin, the interior section extending in the spanwise direction and bounded in a chordwise direction by a first end and an opposite second end;
a plurality of tabs additively manufactured with and extending interiorly from the outer wall, wherein the plurality of tabs include a first tab formed at the first end of the interior section and a second tab formed at the second end of the interior section; and
a plurality of receiving channels extending within the plurality of tabs along the spanwise direction, wherein the plurality of receiving channels is configured to align with the plurality of receiving channels of others of the plurality of additive manufactured wing segments when the plurality of additive manufactured wing segments are oriented for linking; and
a plurality of reinforcement elements operable to be received in the aligned plurality of receiving channels of the plurality of additive manufactured wing segments, wherein the received plurality of reinforcing elements links together the plurality of additive manufactured wing segments.
2. The additive manufactured airframe structure as recited in claim 1 , wherein the plurality of reinforcement elements are tubes.
3. The additive manufactured airframe structure as recited in claim 1 , wherein the plurality of tabs includes a third tab positioned between the first tab and the second tab.
4. The additive manufactured airframe structure as recited in claim 1 , wherein the receiving channels are adjacent to the interior section of the outer wall.
5. The additive manufactured airframe structure as recited in claim 4 , wherein the receiving channels form a substantially hollow portion corresponding in size to one of the plurality of reinforcement elements.
6. The additive manufactured airframe structure as recited in claim 1 , wherein the plurality of reinforcement elements are rods.
7. The additive manufactured airframe structure as recited in claim 6 , wherein the rods are carbon fiber rods.
8. The additive manufactured airframe structure as recited in claim 6 , wherein the rods are pultruded rods.
9. The additive manufactured airframe structure as recited in claim 6 , wherein the rods are bonded to at least a section of respective receiving channels through adhesion, whereby the plurality of additive manufactured wing segments form an assembled airframe component.
10. The additive manufactured airframe structure as recited in claim 9 , wherein the assembled airframe component is a wing.
11. The additive manufactured airframe structure as recited in claim 10 , further comprising:
a plurality of additive manufactured fuselage segments operable to be linked together in an assembled direction, wherein each of the plurality of additive manufactured fuselage segments are separate from one another in an unassembled configuration;
a plurality of fuselage reinforcement elements operable to be received in a fuselage receiving portion of the plurality of fuselage segments and extending through the plurality of fuselage segments in a normal direction;
wherein the fuselage receiving portion is located on the interior of the respective one of the plurality of fuselage segments.
12. An additive manufactured airframe structure, comprising:
a plurality of additive manufactured fuselage segments operable to be linked together in an assembled direction to form an aircraft fuselage, wherein each of the plurality of additive manufactured fuselage segments are separate from one another in an unassembled configuration, and wherein each of the plurality of additive manufactured fuselage segments comprises:
an outer wall that extends circumferentially and encloses a hollow interior therewithin, the hollow interior extending in a normal direction; and
a plurality of receiving channels extending along the outer wall, wherein the plurality of receiving channels is configured to align with the plurality of receiving channels of others of the plurality of additive manufactured fuselage segments when the plurality of additive manufactured fuselage segments are oriented for linking; and
a plurality of reinforcement elements operable to be received in the aligned plurality of receiving channels of the plurality of additive manufactured fuselage segments, wherein the received plurality of reinforcing elements links together the plurality of additive manufactured fuselage segments.
13. An additive manufactured airframe structure, comprising:
a plurality of additive manufactured wing segments each comprising:
a wing outer wall that defines an airfoil cross-section and encloses a wing interior therewithin, the wing interior extending in a wing-normal direction; and
a plurality of wing receiving channels extending along the wing outer wall and aligned with the plurality of wing receiving channels of others of the plurality of additive manufactured wing segments;
a plurality of additive manufactured fuselage segments each comprising:
a fuselage outer wall that extends circumferentially and encloses a fuselage interior therewithin, the fuselage interior extending in a fuselage-normal direction; and
a plurality of fuselage receiving channels extending along the fuselage outer wall and aligned with the plurality of fuselage receiving channels of others of the plurality of additive manufactured fuselage segments;
a plurality of wing reinforcement elements received in the aligned plurality of wing receiving channels of the plurality of additive manufactured wing segments, wherein the received plurality of wing reinforcing elements links together the plurality of additive manufactured wing segments; and
a plurality of fuselage reinforcement elements received in the aligned plurality of fuselage receiving channels of the plurality of additive manufactured fuselage segments, wherein the received plurality of fuselage reinforcing elements links together the plurality of additive manufactured fuselage segments, wherein a wing formed by the plurality of additive manufactured wing segments is coupled to a fuselage formed by the plurality of additive manufactured fuselage segments.