SAE J 2724-2006 Measurement of Disc Brake Friction Material Underlayer Distribution《轮盘制动摩擦材料衬层分布的测量》.pdf

上传人:tireattitude366 文档编号:1027548 上传时间:2019-03-24 格式:PDF 页数:2 大小:140.53KB
下载 相关 举报
SAE J 2724-2006 Measurement of Disc Brake Friction Material Underlayer Distribution《轮盘制动摩擦材料衬层分布的测量》.pdf_第1页
第1页 / 共2页
SAE J 2724-2006 Measurement of Disc Brake Friction Material Underlayer Distribution《轮盘制动摩擦材料衬层分布的测量》.pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising there

2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2006 SAE International All rights reserved. No part of this publication m

3、ay be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA)

4、 Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org J2724 ISSUED JUN2006 SURFACE VEHICLE RECOMMENDED PRACTICE Issued 2006-06 Measurement of Disc Brake Friction Material Underlayer Distribution RATIONALE Not applicable. 1. SCOPE This procedure describes a method for me

5、asuring the fraction of underlayer (also referred to as backing layer) existing at any given height above the a disc brake friction materials shoe plate. Measuring underlayer distribution is useful for computing useable lining thickness and for friction material quality management. 2. REFERENCES The

6、re are no referenced publications specified herein. 3. INSTRUMENTATION A friction material thickness grinder, a micrometer, and a transparency with a 10 mm grid are required to run this test. A digital camera with image analysis software is a preferred but optional method. All test measurement equip

7、ment must be calibrated and maintained per local standards. All applicable safety guidelines and procedures must be followed. Dust collectors should be used when grinding the friction material. 4. SAMPLE PREPARATION This test can be run on new or used disc brake pads with visually distinguishable ba

8、cking layers. 5. OPERATION 5.1 Visually check the lining for any defects such as: cracks, delaminations, edge lift, un-bonded insulators, or foreign contamination. Record any defects or the absence of defects in the test report. 5.2 Grind the lining to the specified thickness (see Section 6) and mea

9、sure that thickness. The measured pad thickness must be within +/-0.1 mm of target thickness. 5.3 At each thickness specified, overlay a transparent film with 10 mm grid lines. Using the grid, count the number of squares with 50% or more backing layer and the number of squares with 50% or more frict

10、ion material. Add these two numbers together and divide to calculate the ratio (percent) of backing layer and friction material. Alternatively, you may photograph the lining (see Figure 1) and use appropriate image analysis software to compute the percentage of underlayer and friction materials. Cop

11、yright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE J2724 Issued JUN2006 - 2 - 65% lining (35% Backing Material) No Pad Defects Found FIGURE 1 - PAD GROUND TO 2 mm ABOVE BACKING PLATE 5.4 Repeat section

12、s 5.2 and 5.3 at any other specified lining thicknesses (see Section 6). 6. GENERAL INSTRUCTIONS In development, the backing layer thickness is typically assessed at 3, 2.5, 2, 1.5 and 1 mm above the shoeplate. In production the test only needs to be run to evaluate the conditions specified (e.g. 90

13、 minimum friction material when the pad is ground to 1.8 mm over the shoeplate). 7. PRESENTATION OF DATA Summarize the readings and include any photographs in a table. PREPARED BY THE SAE BRAKE LININGS STANDARDS COMMITTEE Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 3747-1994 Aerospace Series O-Rings in Fluorosilicone Rubber (FVMQ) Technical Specification Edition P 1《航空航天系列.氟硅橡胶(FVMQ)O形环 技术规范》.pdf AECMA PREN 3747-1994 Aerospace Series O-Rings in Fluorosilicone Rubber (FVMQ) Technical Specification Edition P 1《航空航天系列.氟硅橡胶(FVMQ)O形环 技术规范》.pdf
  • AECMA PREN 3748-2000 Aerospace Series O-Ring Grooves Dimensions Edition P 1《航空航天系列O形环尺寸.P1版》.pdf AECMA PREN 3748-2000 Aerospace Series O-Ring Grooves Dimensions Edition P 1《航空航天系列O形环尺寸.P1版》.pdf
  • AECMA PREN 3750-1993 Aerospace Series Nuts Anchor Self-Locking Fixed 90 Degree Corner Reduced Series with Counterbore in Heat Resisting Steel MoS2 Lubricated Classification 1 100 M.pdf AECMA PREN 3750-1993 Aerospace Series Nuts Anchor Self-Locking Fixed 90 Degree Corner Reduced Series with Counterbore in Heat Resisting Steel MoS2 Lubricated Classification 1 100 M.pdf
  • AECMA PREN 3751-1996 Aerospace Series Nuts Anchor Self-Locking Fixed Closed Corner Reduced Series with Counterbore in Heat Resisting Steel MoS2 Lubricated Classification  1 100 MPa.pdf AECMA PREN 3751-1996 Aerospace Series Nuts Anchor Self-Locking Fixed Closed Corner Reduced Series with Counterbore in Heat Resisting Steel MoS2 Lubricated Classification 1 100 MPa.pdf
  • AECMA PREN 3752-1994 Aerospace Series Nuts Self-Locking MJ Threads in Heat Resisting Steel FE-PA92HT (A286) MoS2 Coated Classification 1 100 MPa (at Ambient Temperature) 425 Degree.pdf AECMA PREN 3752-1994 Aerospace Series Nuts Self-Locking MJ Threads in Heat Resisting Steel FE-PA92HT (A286) MoS2 Coated Classification 1 100 MPa (at Ambient Temperature) 425 Degree.pdf
  • AECMA PREN 3753-1993 Aerospace Series Nuts Anchor Self-Locking Fixed 60 Degree Corner with Counterbore in Alloy Steel Cadmium Plated MoS2 Lubricated Classification 1 100 MPa (at Am.pdf AECMA PREN 3753-1993 Aerospace Series Nuts Anchor Self-Locking Fixed 60 Degree Corner with Counterbore in Alloy Steel Cadmium Plated MoS2 Lubricated Classification 1 100 MPa (at Am.pdf
  • AECMA PREN 3754-2009 Aerospace series Nuts anchor self-locking fixed 60 degrees corner with counterbore in heat resisting steel MoS2 lubricated Classification  1 100 MPa (at ambien.pdf AECMA PREN 3754-2009 Aerospace series Nuts anchor self-locking fixed 60 degrees corner with counterbore in heat resisting steel MoS2 lubricated Classification 1 100 MPa (at ambien.pdf
  • AECMA PREN 3757-1998 Aerospace Series Nuts Anchor Self-Locking Floating Self-Aligning Two Lug in Heat Resisting Steel MoS2 Lubricated Classification  900 MPa (at Ambient Temperatur.pdf AECMA PREN 3757-1998 Aerospace Series Nuts Anchor Self-Locking Floating Self-Aligning Two Lug in Heat Resisting Steel MoS2 Lubricated Classification 900 MPa (at Ambient Temperatur.pdf
  • AECMA PREN 3758-1997 Aerospace Series Simplex High Speed Data Transmission System Edition P 1《航空航天系列.单通道高速数据传输系统》.pdf AECMA PREN 3758-1997 Aerospace Series Simplex High Speed Data Transmission System Edition P 1《航空航天系列.单通道高速数据传输系统》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1