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Harmonic deceleration mechanism of an inertial stable tracking platform

A technology of harmonic deceleration and tracking platform, applied in the field of harmonic deceleration mechanism and power transmission drive, can solve the problems of small load/weight ratio, difficult to find, large volume, etc. Effect

Active Publication Date: 2015-12-09
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

These two stable platforms represent the international advanced level of two-frame structure and four-frame two-axis mechanism stable platforms, but these generally show systematic shortcomings in terms of large volume, small load / weight ratio, poor precision, etc., that is, it is difficult to find A product that integrates the advantages of the above aspects

Method used

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  • Harmonic deceleration mechanism of an inertial stable tracking platform
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  • Harmonic deceleration mechanism of an inertial stable tracking platform

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Embodiment Construction

[0027] The structure of the deceleration and vibration reduction system driven by a DC motor of the present invention is suitable for driving the rotational degree of freedom of an inertial stable platform, and has the advantages of large transmission ratio, good transmission rigidity, small size and light weight of the driving unit, and simple structure. The structure can also effectively isolate the angular motion and vibration of the aircraft, improve the platform's carrying capacity and stability accuracy, and is suitable for frame drives in aerial remote sensing and target tracking.

[0028] as attached figure 1 As shown, it is characterized in that it includes motor base 1, code disc tray 2, code disc 3, rotor sleeve 4, drive lower key 5, motor shaft lower bearing 6, rotor sleeve cup 7, electric brush 8, rotor steel ring 9, Harmonic lower bearing 10, harmonic inner sleeve 11, harmonic outer sleeve 12, harmonic upper bearing 13, harmonic rotor 14, driving gear 15, stator ...

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Abstract

Disclosed is a harmonic wave speed reducing mechanism of an inertance stabilizing tracking platform. The harmonic wave speed reducing mechanism of the inertance stabilizing tracking platform comprises a driving structure part, a harmonic wave transmission part and a transmission output structure part, wherein the driving structure part comprises a motor rotor assembly, a motor stator assembly, a motor shaft assembly and a motor installation assembly, the harmonic wave transmission part comprises a harmonic wave generator, a harmonic wave steel wheel and a harmonic wave flexible wheel, and the transmission output structure part comprises a transmission shaft assembly, a transmission shaft sleeve assembly and a lead wire slip ring assembly. Control of the degree of freedom of rotation is achieved through a driving structure, and power support is provided to movement of the platform. A harmonic wave transmission structure is a belt of the driving structure and a transmission structure, and driving of loads of different levels can be achieved through different gear ratios. Speed reduction and twist increase of an output shaft are achieved through a transmission output structure, and servo control of an angle movement of a transmission shaft is achieved according to a programming instruction. The harmonic wave speed reducing mechanism of the inertance stabilizing tracking platform is suitable for control of the inertance stabilizing platform and has the advantages of being large in transmission ratio, good in transmission rigidity, small in size of the driving unit, light in weight, simple in structure and the like. The harmonic wave speed reducing mechanism of the inertance stabilizing tracking platform is capable of improving carrying capacity and stabilization precision of the platform and is suitable for framework driving of aerial remote sensing and target tracking.

Description

technical field [0001] The invention belongs to the technical field of aerial photoelectric imaging, and relates to a harmonic deceleration mechanism of an inertial stable tracking platform, which is suitable for power transmission drive in an aerial photoelectric imaging system using a helicopter or a light and small aircraft as a flight platform. Background technique [0002] The power transmission mechanism of the inertial stable tracking platform is one of the key equipment of the airborne earth observation platform. Its function is to support the imaging load and isolate the attitude angle movement and external disturbance of the flight carrier in three directions, so that the visual axis of the imaging load is in the inertial space. Always track and perpendicular to the local horizon, increasing imaging resolution. However, due to the limitation of the aviation application environment, the power transmission mechanism of the inertial stable tracking platform needs to h...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D47/00
Inventor 周向阳房建成李贝张建斌岳海潇俞瑞霞
Owner BEIHANG UNIV
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