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公开(公告)号:US20250121926A1
公开(公告)日:2025-04-17
申请号:US19002889
申请日:2024-12-27
Applicant: Textron Innovations Inc.
Inventor: Charles David Hogue , James Everett Kooiman , Joseph Richard Carpenter, JR. , David G. Carlson , Jonathan Alexander Freeman
Abstract: An aircraft is described and includes a fuselage; wings attached to the fuselage; and a torque box within the fuselage, the torque box including a side panel, the side panel comprising a composite laminate material including a plurality of stiffening beads integrated therewith. The plurality of stiffening beads may be integrated with the side panel and extend parallel to one another.
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公开(公告)号:US20240317382A1
公开(公告)日:2024-09-26
申请号:US18188132
申请日:2023-03-22
Applicant: Textron Innovations Inc.
Inventor: Charles David Hogue , James Everett Kooiman , Joseph Richard Carpenter, JR. , David G. Carlson , Jonathan Alexander Freeman
IPC: B64C1/06
Abstract: An aircraft is described and includes a fuselage; wings attached to the fuselage; and a torque box within the fuselage, the torque box including a side panel, the side panel comprising a composite laminate material including a plurality of stiffening beads integrated therewith.
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