Abstract: Forming a cured composite structure may include assembling pre-cure members about a variable volume support member to form a pre-cure assembly, applying an internal pressure from within the pre-cure assembly by maintaining the variable volume support member at an expanded volume, and curing the pre-cure members by applying heat while the variable volume support member is in the expanded volume to form a cured composite structure.
Type:
Application
Filed:
January 6, 2017
Publication date:
July 12, 2018
Applicant:
Applied Composite Technology Aerospace, Inc.