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Lifting platform for assembling light aircraft

A technology for lifting platforms and light aircraft, applied in the direction of lifts, lifting devices, mechanical equipment, etc., can solve the problems of lower work efficiency, poor practicability and reliability, and delivery of accessories or tools, so as to improve work efficiency and output The effect of torque

Inactive Publication Date: 2019-10-18
刘山平
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The defect of the above-mentioned lifting platform is that during assembly, if the workers on the platform need accessories or tools that are not carried, since the platform has been raised to a certain height, it is difficult for people under the platform to send the accessories or tools to the platform. The platform will be lowered, thereby reducing work efficiency; in addition, the lifting motor also has insufficient output torque, and the existing reducer has insufficient internal lubrication performance, resulting in poor practicability and reliability

Method used

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  • Lifting platform for assembling light aircraft
  • Lifting platform for assembling light aircraft
  • Lifting platform for assembling light aircraft

Examples

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Embodiment Construction

[0025] The specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. The following examples are used to illustrate the present invention, but are not intended to limit the scope of the present invention.

[0026] Such as Figure 1 to Figure 3 As shown: this embodiment provides a lifting platform for light aircraft assembly, including a support base plate 1 and a support top plate 2 arranged in parallel up and down, and a folding telescopic frame 3 and a support base plate 2 are respectively arranged between the support base plate 1 and the support top plate 2 Stable telescopic rod, and the folding telescopic frame 3 is arranged between the stable telescopic rods on both sides, the connection between the folding telescopic frame 3 and the support bottom plate 1 and the support top plate 2 is provided with a limit connecting plate 4, and the limit The connecting plate 4 is co...

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PUM

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Abstract

The invention relates to the field of auxiliary devices for light aircrafts, and particularly discloses a lifting platform for assembling a light aircraft. The lifting platform comprises a supportingbottom plate and a supporting top plate; a folding telescopic rack and stable telescopic rods are separately arrange between the supporting bottom plate and the supporting top plate; an adjusting sleeve and a lifting motor used for driving the adjusting sleeve to rotate are separately arranged at the top of the supporting bottom plate; the adjusting sleeve is arranged at the middle part of the supporting bottom plate; a positioning screw rod is in threaded connection with an inner cavity of the adjusting sleeve in a sliding manner; the top of the positioning screw rod is connected with a supporting shaft at the top of the folding telescopic rack; each stable telescopic rod comprises an inner rod and an outer sleeve; the bottom ends of the inner rods are fixedly connected onto the top surface of the supporting bottom plate; the top ends of the outer sleeves are fixedly connected onto the bottom surface of the supporting top plate; and the inner rods coaxially extend into the outer sleeves corresponding to the inner rods and can move axially. An accessory or a tool not to be carried can be sent onto the platform, so that the working efficiency is improved, and meanwhile, the output torque of the lifting motor can be improved.

Description

technical field [0001] The invention relates to the field of light aircraft auxiliary equipment, in particular to a lifting platform used for light aircraft assembly. Background technique [0002] Light aircraft generally refers to aircraft with a maximum take-off weight of less than 5,700 kg. This type of aircraft has the characteristics of lightness, safety, low requirements for use, can take off and land on grass, easy to operate, and low price; light aircraft is small in size and relatively simple in structure. For leisure and business travel; although some light aircraft have jet engines, piston engines are often used to drive propulsion; large, high-speed aircraft have landing gear that allows the wheels to be retracted after takeoff; light aircraft are designed to reduce weight And cost saving, usually equipped with a fixed tripod. As new synthetic materials are developed, lightweight aircraft will become stronger, lighter and fly farther. [0003] Although the auto...

Claims

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Application Information

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IPC IPC(8): B66F7/06B66F7/28F16H57/04
CPCB66F7/0608B66F7/0666B66F7/28F16H57/0402F16H57/0456
Inventor 刘山平方超其他发明人请求不公开姓名
Owner 刘山平
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