An aircraft (10) is disclosed. An aircraft (10) is provided with a fuselage (12), wings (rear wings (16)) disposed above the fuselage (12), a pylon (32), and a plurality of internal combustion engines (58). The wings are connected to the fuselage (12) through the hanging frames (32); the plurality of internal combustion engines (58) are housed in the body (12). The hanger (32) vertically penetrates the fuselage (12) and is fixed to the upper portion and the lower portion of the fuselage (12), and a first internal combustion engine (a first engine (58L)) and a second internal combustion engine (a second engine (58R)) among the internal combustion engines (58) are arranged in bilateral symmetry about the hanger (32) and are fixed to the hanger (32). Accordingly, the internal combustion engine can be stabilized by being arranged in the fuselage in a balanced manner.
本发明公开一种航空器(10)。航空器(10)具有机身(12)、机翼(后翼(16))、挂架(32)和多个内燃机(58),其中,所述机翼被配置在比机身(12)靠上方的位置;所述挂架(32)将机翼连接于机身(12);多个所述内燃机(58)被收装于机身(12)。挂架(32)纵穿机身(12)且被固定于机身(12)的上部和下部,多个内燃机(58)中的第1内燃机(第1发动机(58L))和第2内燃机(第2发动机(58R))以挂架(32)为中心左右对称配置,且被固定于所述挂架(32)。据此,能够在机身的内部通过平衡配置内燃机而使其稳定。
Aircraft
航空器
2022-09-30
Patent
Elektronische Ressource
Chinesisch
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