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Six-shaft rotating device of aircraft

A technology of a rotating device and an aircraft, which is applied in the field of aircraft, and can solve problems such as the inability to adjust the angle, the easily damaged blades of the aircraft, and the difficulty of protection, etc., and achieve the effects of adjusting the flight angle, facilitating rapid steering, and prolonging the service life

Active Publication Date: 2018-03-23
ANHUI UNIVERSITY OF TECHNOLOGY AND SCIENCE
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

They get the necessary speed into space under the propulsion of the launch vehicle, and then rely on inertia to do orbital motions similar to celestial bodies. With the continuous development of science and technology, the application of aircraft is becoming more and more extensive, especially some small aircraft are now living It plays an important role, but the rotation device of the general aircraft cannot adjust the angle when in use, and the fan blades of the aircraft are easily damaged when not in use, and it is not easy to protect

Method used

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  • Six-shaft rotating device of aircraft
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  • Six-shaft rotating device of aircraft

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Embodiment

[0025] like Figure 1 to Figure 6 As shown, the present invention provides a six-axis rotating device for an aircraft, including a fixed plate 1, a connecting column 2 and a rotating seat 3, the surface of the fixed plate 1 is provided with a wind deflector 101, and the bottom end of the wind deflector 101 is An externally threaded ring 104 is connected, and the externally threaded ring 104 coincides with the internal thread on the surface of the fixed plate 1. The wind deflector 101 is fixed on the surface of the fixed plate 1 by threads, and the side of the fixed plate 1 is connected with six fixed Seat 4, one end of the connecting column 2 is hinged together with the fixed plate 1 through a hinge 401, and several hydraulic rods 402 are connected to the side of the fixed plate 1, and the hydraulic rods 402 are connected to the fixed plate 1, The hydraulic rods 402 are hinged together. After the angles of the connecting columns 2 are adjusted through the hydraulic rods 402, d...

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PUM

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Abstract

The invention discloses a six-shaft rotating device of an aircraft. The six-shaft rotating device comprises a fixing disk, connecting columns and rotating seats, wherein a wind guiding plate is arranged on the surface of the fixing disk; six fixing seats are connected to the side surface of the fixing disk; one end of each connecting column is integrally hinged to the corresponding fixing disk through a corresponding hinge; a plurality of hydraulic rods are connected to the side surface of the fixing disk; each hydraulic rod is integrally hinged to the corresponding fixing disk through a corresponding hinge joint; the other end of the corresponding connecting column is integrally connected with the corresponding rotating seat; a motor seat is arranged in each rotating seat; a micro motor is mounted in each motor seat; a rotating shaft is connected to an output shaft of each micro motor; a clamping disk is mounted on the side surface of the top end of each rotating shaft; rotating blades are arranged in each clamping disk; a plurality of blade grooves are respectively formed in the surfaces of the rotating seats; and an adjusting screw is connected to the bottom end of each motor seat. According to the six-shaft rotating device disclosed by the invention, a relative angle between the rotating seats can be adjusted, so that balance among different flying angles is realized; and when the six-shaft rotating device is not used, the six-shaft rotating device is convenient to retract, not liable to damage, long in service life and worth popularizing.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a six-axis rotating device for an aircraft. Background technique [0002] Aircraft are instruments that fly in or outside the atmosphere. Aircraft are divided into three categories: aircraft, spacecraft, rockets and missiles. Those flying in the atmosphere are called aircraft, such as balloons, airships, airplanes, etc. They rely on the static buoyancy of the air or the aerodynamic force generated by the relative motion of the air to lift into the air. Those flying in space are called spacecraft, such as artificial earth satellites, manned spacecraft, space probes, and space shuttles. They get the necessary speed into space under the propulsion of the launch vehicle, and then rely on inertia to do orbital motions similar to celestial bodies. With the continuous development of science and technology, the application of aircraft is becoming more and more extensive, especially so...

Claims

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Application Information

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IPC IPC(8): B64C27/473B64C27/52B64C27/08
CPCB64C27/08B64C27/473B64C27/52
Inventor 陈玉李祥祥王鹏郝声远李敏
Owner ANHUI UNIVERSITY OF TECHNOLOGY AND SCIENCE
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