Aircraft seat backs with non-tubular peripheral flanges
A technology of seat back and flange, applied in the field of seat back, can solve the problems of weight, safety, size, cost change, conflict with each other, etc.
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Examples
example 1
[0098] Example 1. A seat back for a passenger seat, the seat back comprising: a unitary structural core formed as a single piece, the unitary structural core comprising: (A) a body comprising a carbon fiber composite material, the body further comprising a front lateral and rearward sides; and (B) a non-tubular flange comprising a carbon fiber composite material, the non-tubular flange being integrally formed with the main body and comprising a rearward side of the main body along the integral The portion of the left, top, and right edges of the structural core that extends.
example 2
[0099] Example 2. The seat back of example 1 or any preceding or following example, wherein the non-tubular flange comprises: (A) a depth extending rearwardly from a rearwardly side of the body; and (B) ) thickness transverse to the depth and corresponding to the distance between the inward side of the non-tubular flange and the outer side of the non-tubular flange, wherein the non-tubular flange spans the thickness including a solid Material.
example 3
[0100] Example 3. The seat back of Example 2 or any preceding or following example, wherein the thickness of the non-tubular flange is varied such that the thickness of the non-tubular flange is greater near the bottom of the unitary structural core than at the near the top of the one-piece structural core.
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Abstract
Description
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Application Information
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