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Double-shaft swinging and rotating mechanism based on driving gear ring structure

A transmission gear and gear shaft technology, which is applied in the field of electric control technology and aerodynamics, can solve the problems of increased servo mechanism volume, reduced system reliability, and increased maintenance costs, so as to improve reliability, work performance, and work Effects of Environmental Improvement, Mass and Inertia Reduction

Active Publication Date: 2017-09-01
郝思阳 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Excessive exposure of the servo mechanism increases the windward area and brings a lot of resistance to flight
Secondly, servo motors are precision equipment, long-term exposure will reduce system reliability and greatly increase maintenance costs, so it is not practical
Moreover, due to structural reasons, most of the existing two-axis swing mechanisms have a swing dead zone, and it is difficult to complete omnidirectional tilting.

Method used

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  • Double-shaft swinging and rotating mechanism based on driving gear ring structure
  • Double-shaft swinging and rotating mechanism based on driving gear ring structure
  • Double-shaft swinging and rotating mechanism based on driving gear ring structure

Examples

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Effect test

Embodiment Construction

[0031] As shown in the figure, the present invention includes a first servo motor 1, a second servo motor, a first cylindrical gear 2, a first bevel gear, a second cylindrical gear 3 and a housing, and a bevel gear ring 8 is arranged in the housing, and the housing A third bevel gear 18 is arranged on it.

[0032] The center of the first spur gear 2 is connected with the rotating shaft of the first servo motor 1 , the central shaft of the second spur gear 3 is fixedly connected with the housing, and the first spur gear 2 meshes with the second spur gear 3 .

[0033] The first bevel gear shaft 6 is connected to the rotating shaft of the second servo motor 4, and the first bevel gear shaft 6 passes through the central axis of the second spur gear 3 and is connected to the center of the first bevel gear on the housing.

[0034] Both the first bevel gear and the third bevel gear mesh with the bevel gear ring 8 , and the third bevel gear shaft is connected with the engine base 7 . ...

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PUM

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Abstract

The invention belongs to the technical field of electric control and aerospace dynamics, and particularly relates to a double-shaft swinging and rotating mechanism based on a driving gear ring structure. The double-shaft swinging and rotating mechanism based on the driving gear ring structure is high in reliability and working performance. The double-shaft swinging and rotating mechanism based on the driving gear ring structure comprises a first servo motor 1, a second servo motor, a first cylindrical gear 2, a first bevel gear, a second cylindrical gear 3 and a shell body. The double-shaft swinging and rotating mechanism based on the driving gear ring structure is structurally characterized in that a bevel gear ring 8 is arranged in the shell body, and a third bevel gear 18 is arranged on the shell body; the center of the first cylindrical gear 2 is connected with a rotating shaft of the first servo motor 1, a center shaft of the second cylindrical gear 3 is fixedly connected with the shell body, and the first cylindrical gear 2 is engaged with the second cylindrical gear 3.

Description

technical field [0001] The invention belongs to the fields of electric control technology and aviation power technology, and in particular relates to a two-axis swing mechanism based on a transmission gear ring structure. Background technique [0002] Thrust vectoring technology allows part of the engine thrust to be turned into a control force, replacing or partially replacing the control surface; no matter how large the angle of attack is and how low the flight speed is, the aircraft can use this part of the control force to control, which increases the controllability of the aircraft sex. Since the control force is directly generated, and the magnitude and direction are variable, the agility of the aircraft is also increased. [0003] In recent years, the drone industry has developed rapidly, especially small and medium-sized drones have been used in more and more fields. Diversified mission requirements also put forward higher and higher requirements for the maneuverab...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C9/00B64C19/00
CPCB64C9/00B64C19/00B64U50/19B64U2201/00
Inventor 郝思阳杨帆唐鹏冯杨李海旺
Owner 郝思阳
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