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Rapid capable of being assembled and disassembled cardboard spacing support rod and spacing adjustment method thereof

A support rod and card board technology, which is applied in the field of aircraft wall panel product assembly, can solve the problems of difficult on-site operation and the inability to disassemble the card board support rod, and achieves the effects of strong structural versatility, light weight and accurate monitoring.

Pending Publication Date: 2019-06-21
XIAN AIRCRAFT IND GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The traditional pallet support rod is a fixed structure. After the adjustment is completed, the pallet support rod cannot be disassembled. When the pallet is disassembled, several pallets connected to the pallet support rod must be disassembled at the same time, which is difficult to operate on site.

Method used

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  • Rapid capable of being assembled and disassembled cardboard spacing support rod and spacing adjustment method thereof
  • Rapid capable of being assembled and disassembled cardboard spacing support rod and spacing adjustment method thereof
  • Rapid capable of being assembled and disassembled cardboard spacing support rod and spacing adjustment method thereof

Examples

Experimental program
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Embodiment Construction

[0019] see Figure 1 ~ Figure 3 , The fast disassembled support rod for the distance between the clamps, including the support rod 1, the corner seat 2, the connecting seat 3, and the adjusting screw. The corner seat 2 is fixed on the card board, and the connecting seat 3 is fixed on the corresponding adjacent card board. The connecting seat 3 is provided with a scale 9 and a card slot 10 matched with the adjusting screw. The support rod 1 is a Z-shaped structure, and one end thereof It is fixed on the corner seat 2, and the other end with the pointer 8 is fixed above the scale 9. The adjusting screw includes a forward screw 4, a reverse screw 5, a handle nut 6, a limit block 7, and the reverse screw 5 is provided with The chute matched with the limit block 7, the forward screw 4 and the reverse screw 5 are connected as a whole through the handle nut 6, one end of the forward screw 4 is fixed on the strut 1, and one end of the reverse screw 5 is installed on the connecting sea...

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PUM

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Abstract

The invention provides a rapid capable of being assembled and disassembled cardboard spacing support rod and a spacing adjustment method thereof. The support rod comprises a Z-shaped structural strutand an adjustment screw rod, wherein one end of the Z-shaped structural strut is fixed on an angle seat, and the other end, with a pointer, is fixed on a scaleplate, and is used for measuring the spacing between adjacent cardboards. The adjustment screw rod comprises a forward screw rod and a reverse screw rod, and the forward screw rod and the reverse screw rod are driven by rotating a handle nut, so as to adjust the spacing between the adjacent cardboards.

Description

technical field [0001] The present application relates to the technical field of assembly of aircraft panel products, in particular to a quick-detachable pallet spacing support rod and a spacing adjustment method thereof. Background technique [0002] Aircraft siding assembly tooling is used for assembling parts and components of riveted aircraft siding. Panel assembly tooling usually includes multiple sets of inner and outer clamps for positioning and pressing the product. Due to the large length and width of the panel product, the length and width of the panel product for large aircraft can reach 3m, or even more Large, the length of the wallboard tooling pallet is longer than that of the product. Considering that the wallboard product needs an open upper and lower shelf space, one side of the pallet must be a detachable structure. Usually, the two ends of the pallet are connected to the tooling frame. The structural form of the card board cannot be fixed and supported in...

Claims

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Application Information

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IPC IPC(8): B64F5/10
CPCY02E30/30
Inventor 赵成张程王琳
Owner XIAN AIRCRAFT IND GROUP