Invention Grant
- Patent Title: Composite structural element
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Application No.: US16277297Application Date: 2019-02-15
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Publication No.: US11136108B2Publication Date: 2021-10-05
- Inventor: Sergey Selyugin , Jan-Ronald Balzer
- Applicant: Airbus Operations GmbH
- Applicant Address: DE Hamburg
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE Hamburg
- Agency: Greer, Burns & Crain, Ltd.
- Priority: DE102018104122.5 20180223
- Main IPC: B64C3/18
- IPC: B64C3/18 ; B29C70/20 ; B32B33/00 ; B32B5/26 ; B32B5/02 ; B64F5/10 ; B29K105/10 ; B29L31/30 ; B32B5/12

Abstract:
A composite structural element comprising a substantially planar main section defining a coordinate system with a first axis extending along a longitudinal axis of the structural element and a second axis extending perpendicular to the longitudinal axis within the planar main section. The structural element contains a basic lay-up of single plies, each comprising a fiber-reinforced composite material with a substantially unidirectional fiber orientation. The lay-up comprises N plies arranged from top to bottom in the following form: [[α, β]M; [γ]K; [β, α]M], wherein α, β and γ represent one ply having an angle enclosed between the first axis and the unidirectional fiber orientation of the one ply, respectively, [x]y means y plies each having angle x; [x, y]z means z pairs of plies, K and M are both positive integers equal to or greater than 1: N=4·M+K.
Public/Granted literature
- US20190263499A1 COMPOSITE STRUCTURAL ELEMENT Public/Granted day:2019-08-29
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