Propulsion wing-based cross-medium aircraft capable of vertically taking off and landing and control system of propulsion wing-based cross-medium aircraft
The invention discloses a thrusting wing-based cross-medium aircraft capable of taking off and landing vertically and a control system thereof, the thrusting wing-based cross-medium aircraft comprises a fuselage, a front wing assembly and a rear wing assembly are respectively arranged at the front e...
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Main Authors | , , , , , , , |
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Format | Patent |
Language | Chinese English |
Published |
09.06.2023
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Subjects | |
Online Access | Get full text |
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Summary: | The invention discloses a thrusting wing-based cross-medium aircraft capable of taking off and landing vertically and a control system thereof, the thrusting wing-based cross-medium aircraft comprises a fuselage, a front wing assembly and a rear wing assembly are respectively arranged at the front end and the rear end of the fuselage, and the front wing assembly comprises a front port side rotatable thrusting wing and a front starboard side rotatable thrusting wing; the rear wing assembly comprises a rear port side rotatable propelling wing and a rear starboard side rotatable propelling wing; the rotatable propelling wing is matched with a rotating shaft fixed to the fuselage through a bearing and a shaft support, the wing-shaped rear edge of the propelling wing is embedded into the cross-flow fan, the rotatable propelling wing can independently tilt under the control of a rotating mechanism, and the rotating speed of the cross-flow fan can be independently controlled. The wings of the cross-medium aircraft c |
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Bibliography: | Application Number: CN202310530795 |