Invention Application
US20160082696A1 METHOD FOR LIMITING INTERLAMINAR FATIGUE IN COMPOSITE LAMINATE AND A COMPONENT INCORPORATING THE SAME
审中-公开
用于限制复合层压板中的层间疲劳的方法和包含它们的组分
- Patent Title: METHOD FOR LIMITING INTERLAMINAR FATIGUE IN COMPOSITE LAMINATE AND A COMPONENT INCORPORATING THE SAME
- Patent Title (中): 用于限制复合层压板中的层间疲劳的方法和包含它们的组分
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Application No.: US14798658Application Date: 2015-07-14
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Publication No.: US20160082696A1Publication Date: 2016-03-24
- Inventor: Bogdan Roman Krasnowski , Robert Arnold Brack , Xiaoming Li , Robert Wardlaw
- Applicant: Bell Helicopter Textron Inc.
- Main IPC: B32B7/02
- IPC: B32B7/02 ; B32B27/08 ; B32B37/14 ; B32B27/38

Abstract:
In some embodiments, a rotor system for a rotorcraft includes a yoke, a blade, and a grip that is configured to couple the blade to the yoke. The grip has a plurality of baseline layers and a compliant layer. The baseline layers each have a plurality of fibers disposed in a first polymeric matrix. The compliant layer has a plurality of fibers disposed in a second polymeric matrix. The compliant layer is stronger than the baseline layer and the first polymeric matrix has a different chemical composition than the second polymeric matrix.
Public/Granted literature
- US10792896B2 Method for limiting interlaminar fatigue in composite laminate and a component incorporating the same Public/Granted day:2020-10-06
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