High-speed helicopter transmission system

A transmission system and helicopter technology, which is applied in the field of aerospace, can solve the problems of large radial size, heavy weight, and low life, and achieve the effects of reducing the number of transmission stages, improving stability, and smooth transmission

Inactive Publication Date: 2020-03-27
CHONGQING UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In view of this, the purpose of the present invention is to provide a power transmission system of a high-speed helicopter, to solve the problem that the transmission system has a large radial dimension and an excessive weight under the functional requirements of the main rotor vertical power output and the propeller horizontal power output. , low strength, low service life and other issues to ensure compact structure, high transmission efficiency and high reliability

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  • High-speed helicopter transmission system
  • High-speed helicopter transmission system

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Embodiment Construction

[0023] Embodiments of the present invention are described below through specific examples, and those skilled in the art can easily understand other advantages and effects of the present invention from the content disclosed in this specification. The present invention can also be implemented or applied through other different specific implementation modes, and various modifications or changes can be made to the details in this specification based on different viewpoints and applications without departing from the spirit of the present invention. It should be noted that the diagrams provided in the following embodiments are only schematically illustrating the basic concept of the present invention, and the following embodiments and the features in the embodiments can be combined with each other in the case of no conflict.

[0024] Depend on figure 1 It can be seen that the high-speed helicopter transmission system in this embodiment includes: the main rotor transmission subsyste...

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Abstract

The invention relates to a high-speed helicopter transmission system, which belongs to the field of space flight and aviation, comprises a main rotor transmission subsystem and a propeller transmission subsystem, adopts a pure bevel gear train in structure, and consists of a propeller horizontal reversing bevel gear pair, a main rotor vertical reversing bevel gear pair and a two-wing horizontal reversing bevel gear pair. Power is input through a helicopter main reduction shaft. Power is transmitted through two paths to drive the main rotor and the two-wing propellers respectively, wherein onepath is transmitted from the main reduction shaft to the propeller horizontal reversing bevel gear pair and the two-wing propeller bevel gear pair and then horizontally reverses through the two-wing propeller bevel gear pair to drive the propeller, and the other path is transmitted from the main reduction shaft to the main rotor vertical reversing bevel gear pair and then drives the main rotor torealize power output. While two functions of driving the main rotor wing by vertical reversing of power and driving the propeller by horizontal reversing are realized, the structure is compact, the weight is light, the transmission efficiency is high, the stability is good, the stable driving capability is realized, and the medium-high speed transmission is realized.

Description

technical field [0001] The invention belongs to the field of aerospace and aviation, and relates to a transmission system for transmitting and distributing engine power to main rotors and propellers. Background technique [0002] The transmission system is one of the three key moving parts of the high-speed helicopter. Its main function is to drive the engine accessories and aircraft accessories to work, and transmit the power and speed of the engine to the main rotor, propeller and other accessories of the high-speed helicopter according to a certain transmission ratio. It is an indispensable power transmission component for the power output of the helicopter engine. The performance of the transmission system largely determines the working performance and reliability of the entire helicopter. Because of the special work requirements of the helicopter, there are stricter requirements on its transmission system. Under the premise of realizing the functional requirements of h...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D35/00
CPCB64D35/00
Inventor 宋朝省闫国帅李帅朱才朝汪言
Owner CHONGQING UNIV
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