The present application describes a hybrid stratospheric airship (1; 1 ') configured for combined and optimized use of aerostatic and aerodynamic forces; 1 ') comprising: an inflatable central body (10); first and second inflatable wings (20A, 20B) extending from the central body (10) projecting laterally from two opposite sides of the central body (10), each of the wings (20A, 20B) having a portion (21A, 21B) proximal to the central body (10), an end portion (22A, 22B) distal to the central body (10), a leading edge (201A, 201B) and a trailing edge (202A, 202B); an outer shell (11) having a main shell portion (11A-11C) associated with said main body (10) and a first and a second side shell portion (11D, HE) associated with said first and second wing portions (20A, 20B), respectively; at least one main spar (12) extending transversely to the central body (10), structurally supporting the first and second wing portions (20A, 20B) and traversing the central body (10), the at least one main spar (12) being a linear spar, the at least one main spar (12) being a linear spar, the first and second wing portions (20A, 20B) extending transversely to the central body (10), and the first and second wing portions (20A, 20B) extending transversely to the central body (10). And a linear spar interposed between the leading edges (201A, 201B) and the trailing edges (201A, 201B) of the first and second wings and connected to the distal end portions (22A, 22B) of the first and second wings.
本申请描述了一种被配置用于空气静力学力和空气动力学力的组合和优化使用的混合型平流层飞艇(1;1’),包括:·能充气中央主体(10);·第一能充气翼部和第二能充气翼部(20A、20B),从中央主体(10)延伸,从所述中央主体(10的两个相对的侧侧向突出,所述翼部(20A、20B)中的每一个具有靠近中央主体(10)的部分(21A、21B)、在所述中央主体(10)远侧的端部部分(22A、22B)、前缘(201A、201B)以及后缘(202A、202B);·外壳体(11),具有与所述主要主体(10)相关联的主壳体部分(11A‑11C)以及分别与所述第一翼部和第二翼部(20A、20B)相关联的第一侧壳体部分和第二侧壳体部分(11D、HE);·至少一个主翼梁(12),横向于所述中央主体(10)延伸,该主翼梁在结构上支撑所述第一翼部和第二翼部(20A、20B)并且穿越所述中央主体(10),所述至少一个主翼梁(12)是直线翼梁,该直线翼梁插置在所述第一翼部和第二翼部的前缘(201A、201B)和后缘(201A、201B)之间并连接到所述第一翼部和第二翼部的所述远侧端部部分(22A、22B)。
Tactical hybrid stratospheric airship
战术性混合型平流层飞艇
2023-03-28
Patent
Electronic Resource
Chinese
IPC: | B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft |