发明授权
- 专利标题: Aircraft fuselage configurations for avoiding tail strike while allowing long payloads
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申请号: US17403134申请日: 2021-08-16
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公开(公告)号: US11926434B2公开(公告)日: 2024-03-12
- 发明人: Scott David Rewerts , Jason C. Bell , Mark Emil Lundstrom
- 申请人: ZSM HOLDINGS LLC
- 申请人地址: US DE Dover
- 专利权人: ZSM Holdings LLC
- 当前专利权人: ZSM Holdings LLC
- 当前专利权人地址: US DE Dover
- 代理机构: Barnes & Thornburg LLP
- 主分类号: B64D9/00
- IPC分类号: B64D9/00 ; B64C1/06 ; B64C1/14 ; B64C1/20 ; B64C1/22 ; B64C3/32 ; B64C3/34 ; B64C17/08 ; B64D37/04 ; B64F1/32 ; F03D13/40
摘要:
A fixed-wing cargo aircraft having a kinked fuselage to extend the useable length of a continuous interior cargo bay while still meeting a tailstrike requirement is disclosed. The fuselage defines a continuous interior cargo bay along a majority of its length and a pitch axis about which the cargo aircraft rotates during takeoff while still on the ground. The fuselage includes a forward portion defining longitudinal-lateral plane of the cargo aircraft an aft portion extending aft from the pitch axis to the aft end and containing an aft region of the continuous interior cargo bay that extends along a majority of a length of the aft portion. The aft portion has a centerline extending above the forward upper surface of the aircraft.
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