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A transport vehicle suitable for turbine rotors of various aeroengines

An aero-engine and turbine rotor technology is applied in the field of transport vehicles, which can solve the problems of transport vehicles occupying a lot of space, large in diameter and length, and inconvenient to transport.

Active Publication Date: 2020-12-08
阳信创棣智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Due to the different types of aircraft and the different types of aero-engines used, when replacing or maintaining an aero-engine, it is necessary to transport the parts of the aero-engine, because the diameter and length of the turbine rotor in the aero-engine are relatively small Large, special transport equipment is required for transportation. Due to the different sizes of turbine rotors of different aero-engines, most of them use one type of transport vehicle for one model, which is very inconvenient for transportation, and the transport vehicle will also take up a lot of space. space

Method used

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  • A transport vehicle suitable for turbine rotors of various aeroengines
  • A transport vehicle suitable for turbine rotors of various aeroengines
  • A transport vehicle suitable for turbine rotors of various aeroengines

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Embodiment Construction

[0021] The present invention is specifically described below in conjunction with accompanying drawing, as Figure 1-5 As shown, a transport vehicle suitable for a variety of aero-engine turbine rotors includes a chassis 1, a transverse groove 2 is formed on the upper surface of the chassis 1, and a load slider 3 is arranged in the transverse groove 2. The front of the load slider 3 is provided with a fixing device 4. The fixing device 4 consists of a fixing groove 5 opened on the upper surface of the chassis 1 and located behind the transverse groove 2, and a fixed groove 5 located in front of the load slider 3 and fixedly connected with the load slider 3. The fixed plate 6, the fixed hole 7 opened in the middle position behind the upper surface of the fixed plate 6, and the fixed bolt 8 set in the fixed hole 7 and the fixed groove 5 are jointly formed, and the load-bearing slider 3 is provided with a load-bearing device. 9. The loading device 9 consists of a connecting piece ...

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Abstract

The invention discloses a transporter suitable for various aero-engine turbine rotors. The transporter comprises a chassis, a transverse groove is formed in the upper surface of the chassis, a load bearing slider is arranged in the transverse groove, a fixing device is arranged in front of the load bearing slider and jointly composed of a fixing groove formed in the upper surface of the chassis and positioned in rear of the transverse groove, a fixing plate positioned in front of the load bearing slider and fixedly connected with the load bearing slider, a fixing hole formed in the middle in rear of the upper surface of the fixing plate and a fixing bolt mounted in the fixing hole and the fixing groove in a sleeved manner, a load bearing device is arranged above the load bearing slider, and a supporting device is arranged on the right side of the supporting plate and positioned between a rotating screw and a vertical sliding rail. The transporter has the advantages of simple structureand high practicability.

Description

technical field [0001] The invention relates to the technical field of aero-engine transport, in particular to a transport vehicle suitable for turbine rotors of various aero-engines. Background technique [0002] Due to the different types of aircraft and the different types of aero-engines used, when replacing or maintaining an aero-engine, it is necessary to transport the parts of the aero-engine, because the diameter and length of the turbine rotor in the aero-engine are relatively small Large, special transport equipment is required for transportation. Due to the different sizes of turbine rotors of different aero-engines, most of them use one type of transport vehicle for one model, which is very inconvenient for transportation, and the transport vehicle will also take up a lot of space. space. Contents of the invention [0003] The object of the present invention is to solve the above-mentioned problems, and a transport vehicle suitable for various aeroengine turbi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B62B3/04
CPCB62B3/04B62B2203/60
Inventor 不公告发明人
Owner 阳信创棣智能科技有限公司