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Light helicopter control mechanism and using method thereof

A control mechanism and helicopter technology, applied to rotorcraft, motor vehicles, aircraft, etc., can solve the problem of inconvenient adjustment of the control mechanism, and achieve the effect of avoiding excessive adjustment

Pending Publication Date: 2020-07-14
江西通航科技协同创新有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to overcome the deficiencies in the prior art, provide a light helicopter control mechanism, and solve the problem of inconvenient adjustment of the current helicopter direction control mechanism

Method used

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  • Light helicopter control mechanism and using method thereof
  • Light helicopter control mechanism and using method thereof
  • Light helicopter control mechanism and using method thereof

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Embodiment Construction

[0024] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0025] Such as Figure 1-8 A light helicopter control mechanism shown includes a mounting bracket 1, the mounting bracket 1 is mainly used to install the installation structure of the turntable 2, the wing mounting bracket 3, the connecting shaft 11, the front and rear adjustment system 4 and the left and right adjustment system 5, and the installation The bracket 1 is fixedly sleeved with a connecting shaft 11, and the two sides of the mounting bracket 1 are also symmetrically fixedly installed with a cylinder 12, and the telescopic rod 13 of the cylinder 12 is fixedly sleeved with a collar 14. By designing the cylinder 12, the front and rear adjustment system can be adjusted. 4 and the left and right adjustment system 5 facilitate the support and adjustment of components during adjustment. A turntable 2 is arranged above the mounting bracket 1, and the edge...

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Abstract

The invention discloses a light helicopter control mechanism. The light helicopter control mechanism is characterized by comprising a mounting support, a connecting shaft is fixedly connected with themounting support in a sleeving manner, air cylinders are symmetrically and fixedly mounted on two sides of the mounting support respectively, telescopic rods of the air cylinders are fixedly sleevedwith lantern rings, a rotary disc is arranged above the mounting support, a first connecting rod, a second connecting rod, a third connecting rod and a fourth connecting rod are evenly distributed onan edge of the rotary disc in the radial direction, the second connecting rod and the fourth connecting rod are connected with the lantern rings in a sleeving mode, the connecting shaft is movably sleeved with the rotary disc, the rotary disc is fixedly connected with a wing installation support, the connecting shaft is movably sleeved with the wing installation support through a hinge system, a front-back adjusting system is installed on the first connecting rod, and a left-right adjusting system is installed on the second connecting rod and the fourth connecting rod respectively. The light helicopter control mechanism is advantaged in that a problem that an existing helicopter direction control mechanism is inconvenient to adjust is solved.

Description

technical field [0001] The invention relates to the technical field of helicopter adjustment systems, in particular to a light helicopter control mechanism. Background technique [0002] Compared with other means of transportation, the advantage of a light helicopter is that it can take off and land vertically and hover in the air, which makes it unnecessary for specific roads (relative to cars), airports (relative to fixed-wing aircraft), docks (relative to ships), tracks ( Compared with auxiliary facilities such as trains), it only needs a flat land slightly larger than the size of the fuselage to realize take-off and landing. That is to say, geographical terrain basically does not constitute any restrictions on the use of light helicopters, so light helicopters are sometimes a comparison Ideal means of transportation. However, the market has certain requirements for the flexibility of direction adjustment of light helicopters. However, the structure of the control system ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/52
CPCB64C27/52
Inventor 王佳萍李新平仵宝峰鲁文邹全
Owner 江西通航科技协同创新有限公司
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