Methods for reducing stress on composite structures

Details Methods for reducing stress on composite structures Methods for reducing stress on composite structures

B - Operations, Transporting

32

B

B32B 7/04 (2006.01) F01D 25/24 (2006.01)

Patent

CA 2610094

Methods for reducing stress on composite structures involving providing a primary composite structure (38) having a circumference, providing at least one mounting flange (46) operably connected to the primary composite structure (38) about the circumference to form a joint, and providing a secondary structure (48) operably connected to the primary composite structure (38) at the mounting flange (46) such that when stresses on the primary composite structure (38) exceed a maximum capacity level delamination or separation of the mounting flange (46) from the primary structure (38) occurs at the joint, and the secondary structure (48) remains operably connected to the mounting flange (46).

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