Method for realizing flight control of A-wing aircraft
The invention discloses a method for realizing flight control of an A-wing aircraft, and belongs to the technical field of aviation. The A-wing aircraft is provided with a large-area shell-shaped wide-chord wing, a plurality of rows of driving devices are arranged above and below the shell-shaped wi...
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Format | Patent |
Language | Chinese English |
Published |
02.08.2022
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Abstract | The invention discloses a method for realizing flight control of an A-wing aircraft, and belongs to the technical field of aviation. The A-wing aircraft is provided with a large-area shell-shaped wide-chord wing, a plurality of rows of driving devices are arranged above and below the shell-shaped wing, and layered driving airflow is generated on the surface of the wing; the wing and the driving devices are divided into a plurality of subareas by taking the pneumatic center of the large-area shell-shaped wide-chord wing as an original point; by adjusting the power of the upper driving device and/or the power of the lower driving device of the shell-shaped wing in a certain subarea, namely adjusting the pressure intensity of the layered driving airflow on the upper surface and/or the pressure intensity of the layered driving airflow on the lower surface of the shell-shaped wing in the subarea, the stress of the upper wing surface and/or the stress of the lower wing surface of the shell-shaped wing in the subare |
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AbstractList | The invention discloses a method for realizing flight control of an A-wing aircraft, and belongs to the technical field of aviation. The A-wing aircraft is provided with a large-area shell-shaped wide-chord wing, a plurality of rows of driving devices are arranged above and below the shell-shaped wing, and layered driving airflow is generated on the surface of the wing; the wing and the driving devices are divided into a plurality of subareas by taking the pneumatic center of the large-area shell-shaped wide-chord wing as an original point; by adjusting the power of the upper driving device and/or the power of the lower driving device of the shell-shaped wing in a certain subarea, namely adjusting the pressure intensity of the layered driving airflow on the upper surface and/or the pressure intensity of the layered driving airflow on the lower surface of the shell-shaped wing in the subarea, the stress of the upper wing surface and/or the stress of the lower wing surface of the shell-shaped wing in the subare |
Author | YANG WEIHUA |
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Discipline | Medicine Chemistry Sciences |
DocumentTitleAlternate | 一种实现甲翼机飞行控制的方法 |
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Notes | Application Number: CN202210639410 |
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RelatedCompanies | KUNMING QIAOYI TECHNOLOGY CO., LTD |
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Snippet | The invention discloses a method for realizing flight control of an A-wing aircraft, and belongs to the technical field of aviation. The A-wing aircraft is... |
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SubjectTerms | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
Title | Method for realizing flight control of A-wing aircraft |
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