Fuselage variant type vertical take off and landing aircraft
A technology for vertical take-off and landing aircraft and fuselage, applied in the field of aircraft, can solve the problems of strict design requirements of vertical take-off and landing aircraft, disregarding the actual technical level, harsh internal and external environment, etc. The effect of military combat effectiveness, avoiding devastating assaults
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[0040] The scheme of the present invention has many kinds of specific embodiments, and the best implementation should be determined according to the body weight and speed requirements. For example, a medium-sized "body-variable vertical take-off and landing aircraft" is best to use Figure 1~4 The scheme of the first embodiment adopts a single large turboprop engine, and the propellers counter-rotate up and down (back and forth) to improve efficiency and eliminate the reaction force of the rotating propellers. The rear part of the fuselage is composed of 2 turnable load-bearing structures. These turnable load-bearing structures have a certain length and do not carry cargo, personnel or heavy weapons. The structure is as simple and lightweight as possible. It is best to install the tail on these 2 The tail of a load-bearing structure is used to lengthen the longitudinal moment and improve the efficiency of manipulation; it is best to use an X-shaped tail, which has the advantag...
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