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公开(公告)号：US20240109639A1
公开(公告)日：2024-04-04
申请号：US18532324
申请日：2023-12-07
发明人： John F. GUNDLACH , Jacob S. Allen
CPC分类号： B64C1/061 , B33Y80/00 , B64C3/24 , B64C2001/0054
摘要： An additive manufactured airframe structure includes a first additive manufactured fuselage segment including a first outer wall that extends in a normal direction from a first end to a second end, and also includes a plurality of reinforcement elements extending from the second end of, and away from, the first outer wall in the normal direction. The airframe structure also includes a second additive manufactured fuselage segment formed separately from the first additive manufactured fuselage segment and including a second outer wall that extends in the normal direction from a first end to a second end, and a plurality of receiving channels extending along the second outer wall. The plurality of reinforcement elements are received in the plurality of receiving channels and link together the first and second additive manufactured fuselage segments.
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公开(公告)号：US20230192267A1
公开(公告)日：2023-06-22
申请号：US18103992
申请日：2023-01-31
发明人： John F. GUNDLACH , Jacob S. Allen
CPC分类号： B64C1/061 , B33Y80/00 , B64C3/24 , B64C2001/0054
摘要： Additive manufactured airframe structure having a plurality of additive manufactured airframe segments operable to be linked together in an assembled direction. Each of the plurality of additive manufactured airframe segments are separate from one another in an unassembled configuration. Plurality of reinforcement elements operable to be received in a receiving portion of the plurality of airframe segments and extending through the plurality of airframe segments in a normal direction. Receiving portion is located on the interior of a respective one of the plurality of airframe segments.
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公开(公告)号：US11840323B2
公开(公告)日：2023-12-12
申请号：US18103992
申请日：2023-01-31
发明人： John F. Gundlach , Jacob S. Allen
CPC分类号： B64C1/061 , B33Y80/00 , B64C3/24 , B64C2001/0054
摘要： Additive manufactured airframe structure having a plurality of additive manufactured airframe segments operable to be linked together in an assembled direction. Each of the plurality of additive manufactured airframe segments are separate from one another in an unassembled configuration. Plurality of reinforcement elements operable to be received in a receiving portion of the plurality of airframe segments and extending through the plurality of airframe segments in a normal direction. Receiving portion is located on the interior of a respective one of the plurality of airframe segments.
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公开(公告)号：US11597490B1
公开(公告)日：2023-03-07
申请号：US17559829
申请日：2021-12-22
发明人： John F. Gundlach , Jacob S. Allen
摘要： Additive manufactured airframe structure having a plurality of additive manufactured airframe segments operable to be linked together in an assembled direction. Each of the plurality of additive manufactured airframe segments are separate from one another in an unassembled configuration. Plurality of reinforcement elements operable to be received in a receiving portion of the plurality of airframe segments and extending through the plurality of airframe segments in a normal direction. Receiving portion is located on the interior of a respective one of the plurality of airframe segments.
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