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Automatic tilting device of electric helicopter

A technology of tilting device and helicopter, applied in the field of aircraft, can solve the problems of complex structure, unfavorable installation and debugging, etc., and achieve the effects of low manufacturing cost, small occupied space, and easy maintenance.

Active Publication Date: 2021-12-03
重庆航天工业有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problems of complex structure and unfavorable installation and debugging of current electric unmanned helicopters, the present invention provides an electric helicopter automatic tilting device with small footprint, simple structure, high reliability and easy maintenance

Method used

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  • Automatic tilting device of electric helicopter
  • Automatic tilting device of electric helicopter
  • Automatic tilting device of electric helicopter

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Embodiment Construction

[0022] The present invention will be described in detail below in combination with test examples and specific implementation methods. However, it should not be understood that the scope of the above subject matter of the present invention is limited to the following embodiments, and all technologies realized based on the content of the present invention belong to the scope of the present invention.

[0023] An electric helicopter automatic tilting device, comprising a motor support 1, a tilting shaft 3, a tilting ball head 4, a fixed bracket 6 and a push-pull assembly, the upper part of the tilting shaft 3 is connected to the motor support 1; the middle part of the tilting shaft 3 passes through the tilting ball The head 4 is connected with the fixed bracket 6; the tilt ball head 4 is sleeved on the outer surface of the tilt shaft 3, and the lower part of the tilt shaft 3 is connected with a push-pull assembly, which is used to control the tilt angle and direction of the tilt s...

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PUM

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Abstract

The invention relates to the technical field of aircraft, in particular to an automatic tilting device of an electric helicopter. The automatic tilting device comprises a motor support (1), a tilting shaft (3), a tilting ball head (4), a fixed bracket (6) and a push-pull assembly. The upper part of the tilting shaft (3) is connected with the motor support (1); the middle part of the tilting shaft (3) is connected with the fixed bracket (6) through the tilting ball head (4); the tilting ball head (4) is connected to the outer surface of the tilting shaft (3) in a sleeving mode, and the lower part of the tilting shaft (3) is connected with the push-pull assembly. The device is small in occupied space, simple in structure, high in reliability, easy to disassemble and convenient to maintain; and a driving part of the whole device is installed in a helicopter body and is not interfered by the outside, only two telescopic push rod motors are needed for work, the manufacturing cost is low, the device is very matched with current mainstream pure electric large-scale, small-scale and miniature unmanned helicopters, and the device can be widely applied to the fields of surveying and mapping, transportation, routing inspection and the like, is simple in structure and is worthy of popularization.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an electric helicopter automatic tilting device. Background technique [0002] With the advancement of technology, pure electric large, small and micro unmanned helicopters have developed rapidly and are widely used in surveying and mapping, transportation, inspection and other fields. During the working process of the helicopter aircraft, the helicopter automatic tilter responds to the control commands of the autopilot or the driver, adjusts the rotor tilt angle, changes the magnitude and direction of the lift force, and then controls the movement direction of the helicopter. The traditional tilting device needs three to four steering gears to control the tilting of the rotor disc. The steering gear drives the fixed ring of the automatic tilting device to tilt, and then drives the moving ring of the tilting device to tilt. The moving ring of the tilting device passes through th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/52B64C27/68
CPCB64C27/52B64C27/68B64U10/10
Inventor 王小平田圣尧谭左红杨季川廖长清凌勇万小博樊勇彭鸿云杜学海
Owner 重庆航天工业有限公司
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