B - Operations – Transporting – 29 – C
Patent
B - Operations, Transporting
29
C
B29C 70/24 (2006.01) D04B 1/00 (2006.01)
Patent
CA 2689178
According to one aspect, the present invention relates to a method 200 of manufacturing at least one non-uniform thickness composite spar component 152. The method comprises braiding 202 a plurality of fibres 126 over a non- cylindrical mandrel 140 to form a variable thickness shaped fibre preform 150, flattening the shaped fibre preform 150 and cutting the flattened shaped fibre preform 150 to obtain the at least one non-uniform thickness composite spar component 152. Spars 152 made according to various embodiments of the present invention are faster and less expensive to manufacture than conventional composite spar components.
Craig Wilson And Company
Ge Aviation Systems Limited
LandOfFree
Composite spars does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Composite spars, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Composite spars will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1962223