Study on Influencing Factors and Critical Conditions of Gouging Wear on Rocket Sled

YANG Jingwei; CHEN Keru; SUN Kun; CHEN Cheng

doi:10.7652/xjtuxb202311011

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Study on Influencing Factors and Critical Conditions of Gouging Wear on Rocket Sled

更新时间：2025-12-08

- Study on Influencing Factors and Critical Conditions of Gouging Wear on Rocket Sled
- Vol. 57, Issue 11, Pages: 110-117(2023)
- 作者机构：
  
  1. 西安交通大学金属材料强度国家重点实验室,西安,710049
  2. 中国兵器工业试验测试研究院, 714200, 陕西华阴)
- 作者简介：
- 基金信息：
- DOI：10.7652/xjtuxb202311011
  CLC： TG141
- Online First：10 November 2023，
  
  Published：2023
- 稿件说明：
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YANG Jingwei, CHEN Keru, SUN Kun, et al. Study on Influencing Factors and Critical Conditions of Gouging Wear on Rocket Sled[J]. 2023, 57(11): 110-117.
DOI：

YANG Jingwei, CHEN Keru, SUN Kun, et al. Study on Influencing Factors and Critical Conditions of Gouging Wear on Rocket Sled[J]. 2023, 57(11): 110-117. DOI： 10.7652/xjtuxb202311011.

摘要

针对火箭橇试验凿削磨损现象影响因素作用机制尚不明确、临界条件难以界定的难题

基于有限元法建立了特有的三维凿削磨损模型

在热力耦合场下对该过程进行了模拟。模拟结果表明:在初始航向速度和温度条件下

竖向速度达到1.75 m·s

-1

以上时凿削磨损发生; 在初始航向速度和竖向速度条件下

温度达到673 K以上时凿削磨损发生。初始航向速度条件下

凿削磨损率随着竖向速度和温度的上升而增大。当航向速度由1 200 m·s

-1

增加到1 800 m·s

-1

时

临界竖向速度由1.65 m·s

-1

上升至3.00 m·s

-1

临界温度由673 K上升至873 K

临界夹角由0.079°上升至0.096°。通过降低滑靴竖向速度和温度能够有效避免凿削磨损的发生。该研究可为进一步阐明火箭橇试验中的凿削磨损机制提供理论支撑

并为避免凿削磨损发生、提高试验安全性提供思路。

Abstract

The mechanism of the influencing factors on the gouging wear phenomenon in rocket sled tests is unclear

and the critical conditions are difficult to define. Based on the finite element method

a unique three-dimensional gouging wear model is established to simulate this process in a thermally coupled field. The simulation results show that under the initial heading speed and temperature conditions

gouging wear occurs when the vertical speed reaches 1.75 m·s

-1

or above; Under the initial heading speed and vertical speed conditions

gouging wear occurs w

hen the temperature reaches 673 K or above. Under the initial heading speed condition

the gouging wear rate increases with the increase of vertical speed and temperature. When the heading speed increases from 1 200 m·s

-1

to 1 800 m·s

-1

the critical vertical speed increases from 1.65 m·s

-1

to 3.00 m·s

-1

the critical temperature increases from 673 K to 873 K

and the critical angle increases from 0.079 ° to 0.096 °. By reducing the vertical velocity and temperature of the slippers

it is effective to avoid gouging wear. The research congtributes to theoretical understanding of the gouging wear mechanism in rocket sled tests

and offers insights for avoiding gouging wear and improving the safety of the test.

关键词

Keywords

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