The invention relates to a composite aircraft. The composite aircraft is composed of a primary aircraft and a secondary aircraft, and has two basic statues of being integrated and split; the composite aircraft is composed of a tailless aircraft and a V-shaped empennage aircraft; the secondary aircraft is arranged on the top of the rear body of the primary aircraft; the manned primary aircraft is the main body of the composite aircraft and is of twin-engine tailless aircraft; the unmanned secondary aircraft is used as the V-shaped empennage of the composite aircraft; a connection-separation system is arranged between the primary aircraft and the secondary aircraft to realize reliable connection and separation-status switching between the primary aircraft and the secondary aircraft; the primary aircraft and the secondary aircraft can be separated by use of four methods, namely horizontal flight and longitudinal separation, horizontal flight and normal separation, vertical flight and longitudinal separation and vertical flight and normal separation. The composite aircraft realizes that the primary aircraft, the secondary aircraft and the composite unit of the two formers all have excellent flight performance and fight performance; meanwhile, the primary aircraft and the secondary aircraft can be separated easily; high aerodynamic force and stealth design indices are realized.
Composite aircraft
2015-09-02
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
SAE Technical Papers | 1939
|Engineering Index Backfile | 1935
|TIBKAT | 1984
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