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US 12,319,402 B2Granted
Drive mechanism
AssigneeAirbus Operations S.L.U.
InventorsAlvaro Jara Rodelgo, Miguel Gonzalez Antohi
Life of this patent
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Abstract
A drive mechanism, a drive system and an aerodynamic structure for an aircraft, each including at least one articulated module comprising four links. Each link includes three coupling points distributed forming a triangular geometry. The links are coupled to each other such that an articulation with only one degree of freedom is provided.
Claims17
A drive mechanism comprising at least one articulated module comprising four links,
- wherein each link comprises three coupling points Ai, Bi, Ci, wherein i, with i=1, . . . , 4, denotes the first, second, third and fourth link, respectively;
- wherein in each link the three coupling points are distributed forming a triangular geometry,
- wherein a side Ai-Ci is defined by the coupling points Ai and Ci;
- wherein a side Bi-Ci is defined by the coupling points Bi and Ci;
- and
- wherein a side Ai-Bi is defined by the coupling points Ai and Bi;
- wherein a length of the side B1-C1 of the first link is equal to a length of the side B4-C4 of the fourth link;
- wherein a length of the side A2-B2 of the second link is equal to a length of the side A3-B3 of the third link, and
- wherein the links are coupled to each other according to a relationship wherein:
- the coupling point C1 of the first link is coupled to the coupling point A3 of the third link by means of a pivot joint;
- the coupling point B1 of the first link is coupled to the coupling point B2 of the second link by a pivot joint;
- the coupling point A2 of the second link is coupled to the coupling point C4 of the fourth link by a pivot joint;
- and
- the coupling point B3 of the third link is coupled to coupling point B4 of the fourth link by a pivot joint.
11 more elements
Dependencies are inferred from the claim text.