A composite corner and method for making composite corner

Details A composite corner and method for making composite corner A composite corner and method for making composite corner

B - Operations, Transporting

29

C

B29C 70/18 (2006.01)

Patent

CA 2599634

A gas turbine engine component and a method for making a composite gas turbine engine component, the method includes providing a tool (100) having a first and second surface, the first and second surface arranged at an angle to each other. A fibrous segment (302) (302) is applied to the first surface. The fibrous segment (302) has an end terminating adjacent to the angle between the first surface and the second surface. A fibrous preform (301) is positioned on the fibrous segment (302) and on the second surface. A matrix material is then provided on one or more of the fibrous preform (301) or the fibrous segment (302). The fibrous segment (302) and fibrous preform (301) are heated to a temperature sufficient to allow expansion of the end of the fibrous segment (302). The matrix material is then cured to form a composite article having an angular portion having substantially uniform fiber distribution.

Affiliated with

Also associated with

Rating

A composite corner and method for making composite corner does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with A composite corner and method for making composite corner, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and A composite corner and method for making composite corner will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1931973