Mounting device for an aircraft
First Claim
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1. A method of installing a mounting device in a structural member of an aircraft, comprising the steps of:
- assembling a metal securement member by;
holding unassembled metal sheets together in a constrained position so that the unassembled metal sheets do not move relative to one another;
welding the unassembled metal sheets together with the metal sheets fixedly held in the constrained position so that the metal sheets do not move relative to one another during the welding; and
annealing the welded together metal sheets while fixedly maintaining the welded metal sheets in the constrained position so that the welded metal sheets to not move relative to one another during the annealing;
positioning a mounting device within a channel formed in the structural member, wherein the mounting device comprises the assembled metal securement member and a composite member attached to the metal securement member; and
attaching the composite member to the structural member within the channel.
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Abstract
The invention relates to a mounting device in an aircraft. In one aspect of the invention, a method is disclosed for assembling a metal securement member of the mounting device. In another aspect of the invention, a mounting device is disclosed. In another aspect of the invention, a method is disclosed for installing and using a mounting device in an aircraft.
42 Citations
27 Claims
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1. A method of installing a mounting device in a structural member of an aircraft, comprising the steps of:
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assembling a metal securement member by;
holding unassembled metal sheets together in a constrained position so that the unassembled metal sheets do not move relative to one another;
welding the unassembled metal sheets together with the metal sheets fixedly held in the constrained position so that the metal sheets do not move relative to one another during the welding; and
annealing the welded together metal sheets while fixedly maintaining the welded metal sheets in the constrained position so that the welded metal sheets to not move relative to one another during the annealing;positioning a mounting device within a channel formed in the structural member, wherein the mounting device comprises the assembled metal securement member and a composite member attached to the metal securement member; and attaching the composite member to the structural member within the channel. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26)
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27. A method of installing a mounting device in a structural member of an aircraft, comprising the steps of:
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positioning a mounting device within a channel formed in the structural member, wherein the mounting device comprises a metal securement member, comprising a cap member and two spaced apart arms connected to and extending from a first surface of the cap member, and a composite member attached to a second surface of the cap member opposite the first surface; attaching the composite member to the structural member within the channel; and bonding a spar to and between the two spaced apart arms with an adhesive so that excess of the adhesive seeps out holes, disposed along lengths of the two spaced apart arms, from between the two spaced apart arms to outside of the two spaced apart arms.
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Specification