The invention discloses a self-unlocking aircraft. The self-unlocking aircraft comprises a cruising section, a switching section and a boosting section, wherein the switching section at least comprises a first butt joint section and a second butt joint section; the first butt joint section comprises a first circular truncated cone section and a first cylinder section, the lower bottom end of the first circular truncated cone section is connected with one end of the cruising section, and the upper bottom end of the first circular truncated cone section is connected with one end of the first cylinder section; the diameter of the first cylinder section is smaller than that of the cruising section and that of the boosting section; the second butt joint section comprises a second circular truncated cone section and a second cylinder section, the lower bottom end of the second circular truncated cone section is connected with one end of the boosting section, and the upper bottom end of the second circular truncated cone section is connected with one end of the second cylinder section; the diameter of the second cylinder section is smaller than that of the cruising section and that of the boosting section; and the second cylinder section is sleeved on the outer side of the first cylinder section. The invention has the technical effects of improving the product reliability and reducing the product cost.
本申请公开了一种自解锁的飞行器,包括:巡航段、转接段和助推段;其中,转接段至少包括:第一对接段和第二对接段;第一对接段包括:第一圆台段和第一圆筒段,第一圆台段的下底端与巡航段的一端连接,第一圆台段的上底端与第一圆筒段的一端连接;第一圆筒段的直径小于巡航段的直径和助推段的直径;第二对接段包括:第二圆台段和第二圆筒段,第二圆台段的下底端与助推段的一端连接,第二圆台段的上底端与第二圆筒段的一端连接;第二圆筒段的直径小于巡航段的直径和助推段的直径;第二圆筒段套接于第一圆筒段的外侧。本申请具有提高产品可靠性和降低产品成本的技术效果。
Self-unlocking aircraft
一种自解锁的飞行器
2023-03-07
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Aircraft steering engine steering lock unlocking control circuit
Europäisches Patentamt | 2023
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