Folding missile lifting lug structure

A lifting ear and missile technology, applied in the field of missile parts, can solve the problems of shortening the missile range, affecting the flight performance of the missile, increasing the resistance, etc., and achieving the effects of reducing aerodynamic resistance, simple structure and flexible use.

Inactive Publication Date: 2014-12-24
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

This technology helps hide any bumps on an object's surface during launching or after being lifted by other means like carts without causing damage. Its technical effect includes reducing air drag while flying at speeds upwards over 100 mph (miles per second), making them more efficient than traditional methods such as ramming into sandbags with weights attached, and allowing people to lift heavy objects safely from their chests when needed.

Problems solved by technology

This patented problem addressed in this patents relates to improving the efficiency or effectiveness of launching missiles with an improved design for their lifters that can resist damage during launches without compromising its ability to perform effectively at longer distances due to increased drag caused by the raised parts attached thereto.

Method used

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  • Folding missile lifting lug structure
  • Folding missile lifting lug structure

Examples

Experimental program
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Embodiment

[0013] Example: see figure 1 , figure 2 .

[0014] A folding missile lifting lug structure, a lifting lug hidden room 12 is opened on the missile body 7, including lifting lug 1, torsion spring 8, rotating shaft 10, bearing 9, leaf spring 5, positioning pin 3, bearing 9 is fixed on the missile body 7, the lifting lug 1 is movably installed in the lifting lug hiding room 12 through the rotating shaft 10 and the bearing 9, the rotating shaft 10 passes through the torsion spring 8, and one arm end of the torsion spring 8 is stuck in the lifting lug 1. The other arm end of the torsion spring 8 is stuck in the elastic body 7, the torsion spring 8 drives the lifting lug 1 to rotate into the lifting lug hidden chamber 12, and the positioning pin 3 is inserted into the elastic body 7 along the lifting lug 1 to prevent the lifting lug 1 from rotating.

[0015] The leaf spring 5 is installed by screws 6 on the edge of the lifting lug hidden chamber 12, the leaf spring 5 just blocks the

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PUM

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Abstract

The invention relates to the field of missile parts, in particular to a folding missile lifting lug structure. A lifting lug hiding room is arranged in a missile body, and comprises a lifting lug, a torsional spring, a rotating shaft, a bearing, a plate spring and a positioning pin, wherein the bearing is fixed in the lifting lug hiding room of the missile body; the lifting lug is movably mounted in the lifting lug hiding room through the rotating shaft and the bearing; the rotating shaft penetrates the torsional spring; one end of the torsional spring is clamped in the lifting lug, and the other end of the torsional spring is clamped in the missile body; the torsional spring drives the lifting lug to be rotated in the lifting lug hiding room; the positioning pin is inserted in the missile body along the side of the lifting lug to prevent the lifting lug from rotating. The folding missile lifting lug structure has the beneficial effects that first, the lifting lug is hidden in the missile body, so that no projections exist on the surface of the missile body, the aerodynamic drag is reduced, and the high speed flight is benefited; second, the folding missile lifting lug structure has a simple structure, and is used flexibly, conveniently and reliably; third, after being unfolded, the lifting lug is suitable for ground hoisting and transporting, and after being folded, the lifting lug is not easy to impact.

Description

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Claims

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Application Information

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Owner JIANGXI HONGDU AVIATION IND GRP
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