Integral transportation support for rear half section of gas compressor

An integral transport, compressor technology

Pending Publication Date: 2022-07-15
HARBIN TURBINE +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention solves the problem that in the existing shipping method, the compressor shakes left and right inside the wooden box due to the bumping of the vehicle, and the compressor cannot be positioned inside the wooden box, which in turn leads to the problem that the compressor is damaged during transportation. , and propose a whole transport bracket for the second half of the compressor

Method used

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  • Integral transportation support for rear half section of gas compressor
  • Integral transportation support for rear half section of gas compressor
  • Integral transportation support for rear half section of gas compressor

Examples

Experimental program
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specific Embodiment approach 1

[0022] Embodiment 1: Combining figure 1 and figure 2 Describing this embodiment, an integral transport bracket for the second half of the compressor described in this embodiment includes a base 1 , a strut 2 , a stopper 3 , a gland 4 , a No. 1 baffle 5 , a pull rod 6 , and a No. 2 baffle 7 , extension shaft 8, No. 1 positioning plate 9, adjusting block 10, No. 1 arc baffle 11, No. 2 arc baffle 12, spring 14, No. 2 positioning plate 15, nut 16 and screw 17;

[0023] One end and two sides of the upper surface of the base 1 are respectively provided with a pillar 2, and the top of each pillar 2 is processed with an arc-shaped through hole. A gland 4 is provided, and one end of the gland 4 is fixedly connected with the stopper 3 on the top side of the pillar 2 through bolts, and the other end of the gland 4 is fixedly connected with the stopper 3 on the other side of the top of the pillar 2 through bolts The middle of the upper surface of the base 1 is provided with a No. 2 arc...

specific Embodiment approach 2

[0025] Specific implementation mode 2: Combining image 3This embodiment is described. This embodiment is a further limitation of the transport bracket described in Embodiment 1. In the overall transport bracket for the second half of the compressor described in this embodiment, the No. 2 baffle 7 includes: The upper semicircular baffle 7-3, the lower semicircular baffle 7-2 and the shock-absorbing rubber plate 7-1;

[0026] A connecting baffle is respectively provided on both sides of the upper surface of the upper semicircular baffle 7-3 and the lower semicircular baffle 7-2, and the upper semicircular baffle 7-3 is connected to the lower semicircular baffle through bolts. The plate 7-2 is fixedly connected, and a shock-absorbing rubber plate 7-1 is respectively provided on the end surfaces of the upper semicircular baffle 7-3 and the lower semicircular baffle 7-2;

[0027] In this specific embodiment, the upper semicircular baffle 7-3 and the end surface of the lower semic...

specific Embodiment approach 3

[0028] Specific implementation three: combination figure 2 This embodiment is described. This embodiment is a further limitation of the transport bracket described in the first embodiment. In the overall transport bracket for the second half of the compressor described in this embodiment, the four corners of the upper surface of the base 1 A lifting lug 13 is respectively provided;

[0029] In this specific embodiment, a lifting lug 13 is respectively provided at the four corners of the upper surface of the base 1 to facilitate the lifting of the transport bracket.

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PUM

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Abstract

The invention discloses a gas compressor rear half section integral transportation support and relates to the technical field of gas turbine transportation. In order to solve the problems that according to an existing loading and transporting mode, due to vehicle jolting, an air compressor shakes left and right in a wooden box, the air compressor cannot be positioned in the wooden box, and then the air compressor is damaged in the transporting process. Shipping is carried out in a three-point supporting mode, and a damping rubber layer is arranged on the inner wall of an arc-shaped through hole in the top of a supporting column; and the damping rubber layer is arranged on the inner wall of the gland, so that the safety of the test piece in the transportation process can be ensured. Axial and radial positioning structures are designed on the transport support to realize radial and axial locking and limiting of the rotor, and the transport support has a horizontal adjusting function so as to ensure that the test piece is in a horizontal state. The transportation support has good rigidity, strength and supporting stability, and meanwhile has a damping function, so that damage to internal parts of the test piece due to vibration in the transportation process is avoided. The invention is suitable for gas turbine transportation.

Description

technical field [0001] The invention relates to the technical field of gas turbine transportation, in particular to an integral transportation support for the second half of a compressor. Background technique [0002] At present, the transportation of compressors on the market is completed by special transport vehicles or special transport brackets. After the parts are transported to the assembly unit, they participate in the assembly. There is no mature transport tool for the second half of the non-standard compressor used for testing. The existing means of transportation is to use wooden boxes for shipment. During the packing process, a large number of anti-collision sponges are placed inside the wooden boxes, so as to realize the shipment of the compressor. The inside of the wooden box swayed from side to side, and the compressor could not be positioned inside the wooden box, resulting in damage to the compressor during transportation; [0003] To sum up, in the existing...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B65D25/10B65D81/07B65D85/68
CPCB65D25/10B65D81/07B65D2585/6875
Inventor 丁莹王铮刘国松潘文娟梁毅超张子盈邱占成白杨杜志强
Owner HARBIN TURBINE
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