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A roll control mechanism suitable for small vertical take-off and landing fixed-wing aircraft

A vertical take-off and landing, control mechanism technology, applied in the direction of flight control, aircraft control, aircraft parts, etc., can solve the problems of difficult maintenance, heavy weight, complex structure, etc., and achieve simple and exquisite structure, easy installation and disassembly, maintenance highly accessible effect

Active Publication Date: 2022-08-05
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the rolling nozzles of large vertical take-off and landing aircraft generally adopt double-door nozzle nozzles, and the opening and closing of the two doors are controlled by two actuators, and the aircraft is controlled by adjusting the flow and speed of the airflow. Its structure is complex, heavy, difficult to maintain, and not suitable for small vertical take-off and landing fixed-wing aircraft

Method used

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  • A roll control mechanism suitable for small vertical take-off and landing fixed-wing aircraft
  • A roll control mechanism suitable for small vertical take-off and landing fixed-wing aircraft
  • A roll control mechanism suitable for small vertical take-off and landing fixed-wing aircraft

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Embodiment Construction

[0027] The present invention will be further described below in conjunction with the examples.

[0028] like Figure 1-2 As shown in the figure, a roll control mechanism suitable for a small vertical take-off and landing fixed-wing aircraft includes a rolling nozzle 3 and a rolling control adjusting mechanism 4. The throat of the engine barrel of the small vertical take-off and landing fixed-wing aircraft is tapered. A rolling nozzle 3 is installed symmetrically to the left and right along the radial direction of the engine barrel 2, and the rolling control and adjustment mechanism 4 includes a driving device installed on the outer wall of the engine barrel 2 and a rolling nozzle 3 and a The blocking device inside the connection of the engine barrel 2 is driven by the driving device to adjust the size of the airflow inlet 15 of the rolling nozzle 3 . In essence, the driving device includes a steering gear 8, and the blocking device includes a baffle 12. The steering gear 8 is...

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Abstract

The invention discloses a rolling control mechanism suitable for a small vertical take-off and landing fixed-wing aircraft, comprising a rolling nozzle and a rolling control adjusting mechanism. , a rolling nozzle is installed symmetrically to the left and right along the radial direction of the engine barrel, and the rolling control and adjustment mechanism includes a driving device installed on the outer wall of the engine barrel and a rolling nozzle installed inside the connection between the rolling nozzle and the engine barrel. The blocking device, the driving device drives the blocking device to adjust the size of the airflow inlet of the rolling nozzle; the invention has a simple and delicate structure, light weight, the rolling nozzle can be quickly installed and unloaded, and the rolling control and adjustment mechanism has high maintenance accessibility. , By controlling the steering gear, it can provide partial lift for the aircraft in the horizontal flight state and the vertical take-off and landing state, and realize the roll control of the acceleration transition from the vertical take-off and landing state to the horizontal flight state.

Description

technical field [0001] The invention belongs to the technical field of aeronautical aircraft design, in particular to a roll control mechanism suitable for small vertical take-off and landing fixed-wing aircraft. Background technique [0002] The vertical take-off and landing fixed-wing aircraft not only has the ability of the rotorcraft to take off and land vertically and control the hovering, but also has the advantages of fast speed and long range of the fixed-wing aircraft. It is a research hotspot in recent years. The rolling nozzle is an important part of the VTOL fixed-wing aircraft. It can provide partial lift for the aircraft in level flight and VTOL state, and provide rolling torque for the aircraft during the acceleration transition from the VTOL state to the level flight state. Play the role of adjusting posture. At present, the rolling nozzles of large vertical take-off and landing aircraft generally use double-door nozzle nozzles. The opening and closing degre...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C15/14
CPCB64C15/14
Inventor 王子安王欣艺刘朋辉吕慧涛龚正
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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