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...

Full description

Saved in:
Bibliographic Details
Main Authors XIE LIDONG, LONG JINSHENG
Format Patent
LanguageChinese
English
Published 08.03.2017
Subjects
AEROPLANES
AIRCRAFT
AVIATION
CONTROLLING
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRANSPORTING
Online AccessGet full text

Cover

More Information
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
Bibliography:Application Number: CN201611068005