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A small unmanned helicopter fuselage

A technology for unmanned helicopters and fuselages, which is applied to the fuselage frame, rotorcraft, motor vehicles, etc., can solve the problems of large transmission distance and load, affecting control performance, affecting transmission efficiency, etc., and achieves shortened power transmission distance and better control Strong performance and the effect of improving transmission efficiency

Inactive Publication Date: 2016-03-30
WUXI HANHE AVIATION TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] But in the disclosed this type action helicopter, the fuselage structure is complicated, and the weight is too large, and the engine start needs to be started by means of an external starting device, which affects the handling performance. Because of the structure, the transmission distance between the clutch and the engine and the gearbox The load is too large, which affects the transmission efficiency

Method used

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  • A small unmanned helicopter fuselage
  • A small unmanned helicopter fuselage
  • A small unmanned helicopter fuselage

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Embodiment Construction

[0022] The preferred embodiments of the present invention will be described below in conjunction with the accompanying drawings. It should be understood that the preferred embodiments described here are only used to illustrate and explain the present invention, and are not intended to limit the present invention.

[0023] Such as figure 1 , 2 , Shown in 3, 4, a kind of small-sized unmanned helicopter fuselage, comprises fuselage frame, starting system, transmission system, engine 1 and exhaust pipe 2, transmission system comprises gear speed clutch 3, gearbox power synchronous belt 4, Transmission power gear 5, transmission driven gear 6, driven gear timing belt 7, tail shaft power gear 8 and tailpipe transmission system 9; gears are arranged on the side of the gear speed clutch, and the transmission power is connected with the transmission power through the transmission power timing belt. The gears are connected; the driven gear of the gearbox coaxial with the power gear of ...

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Abstract

The invention provides a small unmanned helicopter fuselage which comprises a fuselage ring, a starting system, a drive system, an engine and an exhaust pipe, wherein the drive system comprises a gear speed clutch, a gear box power synchronous belt, a gear box power gear, a gear box driven gear, a driven gear synchronous belt, a tail shaft power gear and a tail pipe drive system, wherein the side of the gear speed clutch is provided with a gear which is connected with the gear box power gear through the gear box power synchronous belt; the gear box driven gear is connected with the tail shaft power gear through the driven gear synchronous belt; and the tail shaft power gear is connected with the tail pipe drive system. According to the small unmanned helicopter fuselage, the unique fuselage ring structure has high rigidity and small useless space in the fuselage, and the front and rear parts of the fuselage ring have bending to enable two ends of the fuselage to be contracted so as to facilitate manufacturing of the housing of the streamline fuselage; the built-in starting system can control starting remotely; and the improved drive system shortens the power drive distance, has small load and greatly improves the transmission efficiency.

Description

technical field [0001] The invention relates to a small unmanned helicopter fuselage, which belongs to the field of mechanical structures. Background technique [0002] The unmanned helicopter is fully automatically controlled by computers and microprocessors, and can be operated with human hands on the computer, which is convenient and safe. The small unmanned helicopter itself has strong weather adaptability and can fly under conditions that are not suitable for ordinary aircraft. It is small in size and high in precision. More than anything. Small unmanned helicopters have high flight stability, strong positioning, and low environmental site requirements. When used in pesticide spraying, the spraying efficiency is 10 times that of manual spraying; when used in high-altitude vertical aerial photography, the definition is higher In addition, small unmanned helicopters can also perform long-range aerial photography and stunt photography, forming a new aerial photography sy...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/06B64C27/04B64D27/24
Inventor 朱家乐沈建平沈建文
Owner WUXI HANHE AVIATION TECH