ImageVerifierCode 换一换
格式:PDF , 页数:4 ,大小:97.34KB ,
资源ID:1022864      下载积分:10000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
如填写123,账号就是123,密码也是123。
特别说明:
请自助下载,系统不会自动发送文件的哦; 如果您已付费,想二次下载,请登录后访问:我的下载记录
支付方式: 支付宝扫码支付 微信扫码支付   
注意:如需开发票,请勿充值!
验证码:   换一换

加入VIP,免费下载
 

温馨提示:由于个人手机设置不同,如果发现不能下载,请复制以下地址【http://www.mydoc123.com/d-1022864.html】到电脑端继续下载(重复下载不扣费)。

已注册用户请登录:
账号:
密码:
验证码:   换一换
  忘记密码?
三方登录: 微信登录  

下载须知

1: 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。
2: 试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。
3: 文件的所有权益归上传用户所有。
4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
5. 本站仅提供交流平台,并不能对任何下载内容负责。
6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

版权提示 | 免责声明

本文(SAE ARP 388-1947 UNIVERSAL JOINTS - DESIGN CRITERIA FOR.pdf)为本站会员(appealoxygen216)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

SAE ARP 388-1947 UNIVERSAL JOINTS - DESIGN CRITERIA FOR.pdf

1、 E u =E$a ;o = _ o ., P o, Y Y e ; ,._ c oF - Eu; E :n c y V Y dE o E c V V 0 P _o oo n= voau O c O t O u r bWg. nNO. O C V Y aO l Or u w P O u c a s u c u c o P j g O O YOnQ -a O V V L Y C L Y . u O O v V C U n r O ._ ;oo o u . pwu y b O - E o : gt a v .= a C U Y -9 vn ,o N O U P o E or 0 0 - k 0 3

2、 o= x= , Society of Automotive n, cn. AERONAUTICAL 388 N w Yo k Cityt MMENDED PRACTICE Issued 2-1_g7 UNIVERSAL JOI:VTS - DESIGN CHITIA FOR Revised Page i of 4 A. INTRODUCTION This data sheet is intended for general use by aircraf“t manufacturers contemplating the use of universal joints in their des

3、igns. Although this sheet was prepared primarily to aesiet in the eelection of universal ,jointe for helicapter rotor drivee, it is recommended that it be used for other universal oint applicationa ae Well. The purpose of the data aheet is to provide a atandardized form for providing the uniereal oi

4、nt manufacturer Mith all pertinent information regarding the factors whih determine h3s recommendation of aoint for a particular application. It ehould be kept in mind that the more completely this form is filled out. the greater will be the assurance that the univereal oint recommended will adequa,

5、tely perform it intended Punetion. I. TYPE OF YEHICI,E: Airlane (), Helicopter () Autogyro ( ), Other . II. PURYOS for which joint ia to be used (Main Helicotter inre ca, Inc. Q Issued 2-1-47 v Revised IY&$SAS+ JOINTS - 1SI(N CEITERIA FOH - 2 - $. Power and Speed Batinge: (1) TAIi-OFF . . . . . . .

6、. . _p. at RPM (2)MAICIMUM CONTINUUS ., hp. at RPM (3)NOEMAL CEUISING. . . . . . _ hp. at BPM C. Number of Cylinders . . . . . . . . . . . . _ D. Eine (ea Batio . . . . . . . . . . . . . _ T Total Ratio of Engine BPM to Joint RPM (If 2ranemission, Acceeeory, or other gear ratios are involved) . . .

7、. . . . . . _ F. Type of Vibration Damper (iP ay) E. Coefficient of Speed Fluatuation (if aveilable) c=v v o O, OPERATINf# CONDITIOASs A. (1) Condition III(A)(1) oP expeeted life. . . . . . . . . _ period spplied conLinuously . . . ss. min. Cotdition III(A)(2) bf expected life . . . . . . . . . . pe

8、riod applid continuougYy . . . hre._,in. Conditioa III(A)(3) of ezpeced liPe. . . . . . . . . _ period applied continuonsly . . . _,re._ia. , (2) Condition III(H)(1) of ezpected life. . . . . . . . . _, period applied continuously . . . lre._Jnin. Condition III(B)(2) . of erpected life. . . . . . .

9、. . , period applied continuoualy . . . _re.,_ia. B. Number of atarta during ezpected life . C. Shock loading conditions (severity and Prequency such ae during starting, etc.). . . . . . . . . D. Ezpected life (houre) . . . . . . . . . . . . . Isaued 2-1-47 A UNIYERSAL JOINTS -, ESIGN CfiITE&IA F08

10、Revised - 3 - E. Desired Dieasaembly Inspection Period (hours) F. Desired Servicfng Period (I,ubrication, etc.) (hours) Q. A,aial Loading (if any) . . . . . . . . . . . lbe. Reeulting ror VI. INSTALIATION INFQRt4ATI0N: A. Permanent (fixed) angle (1)Angularity . . . . . . . . . . . . . . . _,_degreee

11、 (2)Fluctua.tion (due to flexible mountings, vibration etc.) . . . . . . . . . . degrees B. Pariable angle l M87C111L1II1 BIllA. . . degreea i of expected life . . . . . . . . . . . _ period applied continuously. . . . irr. min. (2) Normal e.ngle . . . . . . . . . . . . . . degreee of expected life

12、. . . . . . . . . . . _,_, period applied continuouely. . . , hre. min. (3) Minimwn angle. . . . . . . . . . . . , degrees of expected life . . . . . . . . . . . _, period ,pnlied continuoualy. . hre. i min. C. A,xial movement. Give axial movement reqnired due to: (1) Operating conditione . . . . .

13、. . . . . inchea (2)Manufacturing tolersnces . . . . . . , inches D. Dimensional Limitations (Interference Limitations, Diametral Clearance Permissible Length, etc.) (Eaplain wher3 necesse.ry): E. Deaired Wefght Limita,tion. . . . . . . . . . _ts. Q R“ -1-47 IyLy JOINTS - DESI(N CHITIA F a19 -4- F.

14、Diagranmatio Sketch of Inetallation (ShoMing Location of Driving and Dria )lmbere inoiae. Univerasl Joiat Tranomiseion, Clntch, etc.) (I+absl and plain rhsro aecasear) : d. Mieaellaneous iaforaaticn on ilange or pline conaectioae and eise, or as other data to be ooneidsred ia sslaotion of IInitersal Jeint:

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