Invention Publication
- Patent Title: AIRCRAFT COMPOSITE WINGBOX INTEGRATION
- Patent Title (中): 飞机综合展示架集成
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Application No.: EP17185973.9Application Date: 2017-08-11
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Publication No.: EP3287360A1Publication Date: 2018-02-28
- Inventor: KISMARTON, Max U , MUNK, Clayton L
- Applicant: The Boeing Company
- Applicant Address: 100 North Riverside Plaza Chicago, IL 60606-2016 US
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: 100 North Riverside Plaza Chicago, IL 60606-2016 US
- Agency: Boult Wade Tennant
- Priority: US201615238250 20160816
- Main IPC: B64C3/18
- IPC: B64C3/18 ; B64C1/26 ; B64C3/26
Abstract:
Systems and methods are provided for integrating structural components of a wing box. One embodiment is a system that includes outboard planked stringers within an outboard section of a wing box and are co-cured with composite skin at the outboard section. Each outboard planked stringer of the outboard section includes planar layers of Carbon Fiber Reinforced Polymer (CFRP) that are parallel with the composite skin at the outboard section, have fiber orientations aligned to bear tension and compression applied to the wing box, and each extend a different distance along the composite skin at the outboard section. The system also includes center planked stringers within the center section and are co-cured with composite skin at the center section. Each center planked stringer of the center section includes planar layers of CFRP that are parallel with the composite skin at the center section, have fiber orientations aligned to bear tension and compression applied to the wing box, and each extend a different distance along the skin at the center section.
Public/Granted literature
- EP3287360B1 AIRCRAFT COMPOSITE WINGBOX INTEGRATION Public/Granted day:2021-06-16
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