Rectangular combination ducted aircraft and flight control system and method thereof
The invention relates to a rectangular combination ducted aircraft which comprises a rectangular duct body (1), wherein two rows of ducts (7) of the same number are symmetrically arranged on the rectangular duct body (1); a reactive torque grid rudder (6), a power device and a power device support m...
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Main Authors | , |
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Format | Patent |
Language | Chinese English |
Published |
08.03.2017
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Subjects | |
Online Access | Get full text |
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Summary: | The invention relates to a rectangular combination ducted aircraft which comprises a rectangular duct body (1), wherein two rows of ducts (7) of the same number are symmetrically arranged on the rectangular duct body (1); a reactive torque grid rudder (6), a power device and a power device support member (2) are arranged in the duct (7) sequentially from bottom to top; and the rectangular duct body (1) is positioned between the two rows of ducts (7) and also provided with a flight control equipment box (8). The invention also provides a flight control system and control method of the aircraft. The rectangular combination duct aircraft provided by the invention is simple in structure and convenient to assemble/disassemble, can reduce the air resistance and noise, can realize safe and stable flight and can quickly respond to operations; without a balancing reactive torque device, the reactive torque grid rudder of a brand new structure is adopted to realize reactive torque balancing so as to realize quicker and |
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Bibliography: | Application Number: CN201611068005 |