Tilting propeller unmanned aerial vehicle
The invention provides a tilting propeller unmanned aerial vehicle. The tilting propeller unmanned aerial vehicle comprises a fuselage, main wings, main wing propeller thrust unit, a propeller tilting mechanism and a tail propeller thrust unit; the main wings are arranged on the two sides of the fus...
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Main Authors | , |
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Format | Patent |
Language | Chinese English |
Published |
14.09.2021
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Subjects | |
Online Access | Get full text |
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Abstract | The invention provides a tilting propeller unmanned aerial vehicle. The tilting propeller unmanned aerial vehicle comprises a fuselage, main wings, main wing propeller thrust unit, a propeller tilting mechanism and a tail propeller thrust unit; the main wings are arranged on the two sides of the fuselage, the propeller tilting mechanism is connected to the main wings, the main wing propeller thrust unit is connected to the propeller tilting mechanism, and the tail propeller thrust unit is connected to the position, located at the tail of the fuselage, of the fuselage; and the propeller tilting mechanism comprises a shell, a driving part, a first swing arm, a connecting rod and a second swing arm, the main wing propeller thrust unit is hinged to the shell, the driving part is connected to one end of the first swing arm, the other end of the first swing arm is hinged to one end of the connecting rod, the other end of the connecting rod is hinged to the second swing arm, and the second swing arm is connected to |
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AbstractList | The invention provides a tilting propeller unmanned aerial vehicle. The tilting propeller unmanned aerial vehicle comprises a fuselage, main wings, main wing propeller thrust unit, a propeller tilting mechanism and a tail propeller thrust unit; the main wings are arranged on the two sides of the fuselage, the propeller tilting mechanism is connected to the main wings, the main wing propeller thrust unit is connected to the propeller tilting mechanism, and the tail propeller thrust unit is connected to the position, located at the tail of the fuselage, of the fuselage; and the propeller tilting mechanism comprises a shell, a driving part, a first swing arm, a connecting rod and a second swing arm, the main wing propeller thrust unit is hinged to the shell, the driving part is connected to one end of the first swing arm, the other end of the first swing arm is hinged to one end of the connecting rod, the other end of the connecting rod is hinged to the second swing arm, and the second swing arm is connected to |
Author | WANG CHAOSONG ZHANG LIHUI |
Author_xml | – fullname: WANG CHAOSONG – fullname: ZHANG LIHUI |
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DocumentTitleAlternate | 倾转螺旋桨无人机 |
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Notes | Application Number: CN202110621884 |
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RelatedCompanies | SICHUAN YAOLEI TECHNOLOGY CO., LTD |
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Snippet | The invention provides a tilting propeller unmanned aerial vehicle. The tilting propeller unmanned aerial vehicle comprises a fuselage, main wings, main wing... |
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SubjectTerms | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
Title | Tilting propeller unmanned aerial vehicle |
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