Invention Application
US20160069009A1 Fiber Composite Component, Adhesive Arrangement For Fiber Composite Components, And Method For Manufacturing A Fiber Composite Component And An Adhesive Arrangement 审中-公开
纤维复合材料组分,纤维复合材料组分的粘合剂布置,纤维复合材料制造方法和粘合剂布置

  • Patent Title: Fiber Composite Component, Adhesive Arrangement For Fiber Composite Components, And Method For Manufacturing A Fiber Composite Component And An Adhesive Arrangement
  • Patent Title (中): 纤维复合材料组分,纤维复合材料组分的粘合剂布置,纤维复合材料制造方法和粘合剂布置
  • Application No.: US14845468
    Application Date: 2015-09-04
  • Publication No.: US20160069009A1
    Publication Date: 2016-03-10
  • Inventor: Thomas Meer
  • Applicant: Airbus Defence and Space GmbH
  • Applicant Address: DE Ottobrunn
  • Assignee: Airbus Defence and Space GmbH
  • Current Assignee: Airbus Defence and Space GmbH
  • Current Assignee Address: DE Ottobrunn
  • Priority: DE102014012915.2 20140905
  • Main IPC: D05C15/16
  • IPC: D05C15/16 B32B5/26 D06M17/04 B32B7/12
Fiber Composite Component, Adhesive Arrangement For Fiber Composite Components, And Method For Manufacturing A Fiber Composite Component And An Adhesive Arrangement
Abstract:
A fiber composite component includes a composite including cured matrix material and a fiber material embedded therein. At least one partial area of the fiber composite component is provided with at least one thread, which undulates as it extends along a surface area of the composite, so that sections of the thread alternately run inside of the composite and outside of the composite. An adhesive arrangement for such fiber composite components is also disclosed. Finally, methods for manufacturing such a fiber composite component or for manufacturing such an adhesive arrangement are disclosed.
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