NAVY MS9084 REV A-1961 COLLAR SWIVEL-PILOTED O-RING TUBE CONNECTION 4 BOLT AMS 6322《美军标准6332型含4个螺钉的管道连接试用旋转0型套环》.pdf

上传人:bonesoil321 文档编号:984183 上传时间:2019-03-12 格式:PDF 页数:1 大小:70.33KB
下载 相关 举报
NAVY MS9084 REV A-1961 COLLAR SWIVEL-PILOTED O-RING TUBE CONNECTION 4 BOLT AMS 6322《美军标准6332型含4个螺钉的管道连接试用旋转0型套环》.pdf_第1页
第1页 / 共1页
亲,该文档总共1页,全部预览完了,如果喜欢就下载吧!
资源描述

1、MSSOBLI REV A LI7 797l,2 OOLOL35 LI - 1 FED. SUP CLASS c. 8 4 Y I r;-#-.- I .$J C DIA-4 HOLES EQUALLY SPACZD AND LOCATED WITH11.: .O05 OF TRUE POSITION IN RELATION TO F DIA - SEE NOTE 1 PCRi!4E?ER SURFACES HARK PABT NIMBER PER AS 475 CLASS C MFO ICBXT REQD m v SECTION AT S ENLAROOD o Q 1.874 2.652 ,

2、281 .281 2.096 2.964 .344 ,344 SECTIOH R-R 2.248 2.498 1.2.0 2.288 8 I I FIR 1. 2. 3: HIR31IESSr RSCWELL C26-32, 5, PIKSHI CADIIW PLATB AH9 2400. DINSION3 SPECIFIED ARE AFTER PLkTINO. 6. SVXBACB RC)binHNZSSi AS 291. UNLESS OTHEBdISZ SPECIFIED1 SURFACES TO 125 MICROINCES. I: PIRIMTER LIMITS MAY BE EX

3、CEEDED BY POROINO DRAFI ANOLE OF 7 MAX. CKNER PNJ$US MAY VARY BEWEEN 0 AND E. UATERIbLi GYEIL AM9 6322. ?AaTJ SUaIECT M WONETIC PARTICLE INSPICTICN PEfI LYS 264.0. 9R9AK SHARP EDOES -003 - .O15 UNmS OTHERWISE SPECIFIED. DO H3T V3E UNASSIONED PART H?4ERS. 9. DIHWSIOXY 24 IKCHES. WILES3 OTHPRUISS SPZIIFIED; TOLERANCES; LINEAR DIMENSIONS t.010. 10. -. P /- . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • NASA-TN-D-4719-1968 Supersonic aerodynamics of large-angle cones《大角度圆锥的超音速空气动力学》.pdf NASA-TN-D-4719-1968 Supersonic aerodynamics of large-angle cones《大角度圆锥的超音速空气动力学》.pdf
  • NASA-TN-D-4759-1968 Noncavitating and cavitating performance of two low-area-ratio water jet pumps with throat lengths of 5 66 diameters《带有5 66直径咽喉区长度的两个低面积比的喷水泵不成穴和成穴性能》.pdf NASA-TN-D-4759-1968 Noncavitating and cavitating performance of two low-area-ratio water jet pumps with throat lengths of 5 66 diameters《带有5 66直径咽喉区长度的两个低面积比的喷水泵不成穴和成穴性能》.pdf
  • NASA-TN-D-4821-1968 Effect on base drag of recessing the bases of conical afterbodies at subsonic and transonic speeds《在亚音速和跨音速下 圆锥后体基底凹槽底部阻力的影响》.pdf NASA-TN-D-4821-1968 Effect on base drag of recessing the bases of conical afterbodies at subsonic and transonic speeds《在亚音速和跨音速下 圆锥后体基底凹槽底部阻力的影响》.pdf
  • NASA-TN-D-4856-1968 Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail《在反向V尾翼上带有边界层控制的双螺旋浆偏转滑流短距离.pdf NASA-TN-D-4856-1968 Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail《在反向V尾翼上带有边界层控制的双螺旋浆偏转滑流短距离.pdf
  • NASA-TN-D-4891-1968 Prediction of lift and drag for slender sharp-edge delta wings in ground proximity《在近地时 细长锐边三角形机翼升力和阻力的预测》.pdf NASA-TN-D-4891-1968 Prediction of lift and drag for slender sharp-edge delta wings in ground proximity《在近地时 细长锐边三角形机翼升力和阻力的预测》.pdf
  • NASA-TN-D-4929-1968 Theory for computing span loads and stability derivatives due to sideslip yawing and rolling for wings in subsonic compressible flow《在亚音速可压缩流下机翼的侧滑 偏航和旋转引起的翼展荷载.pdf NASA-TN-D-4929-1968 Theory for computing span loads and stability derivatives due to sideslip yawing and rolling for wings in subsonic compressible flow《在亚音速可压缩流下机翼的侧滑 偏航和旋转引起的翼展荷载.pdf
  • NASA-TN-D-4983-1969 Full-scale wind-tunnel investigation of static longtudinal and lateral characteristics of a light twin-engine airplane《轻型双发动机飞机静态纵向和横向特性的全比例风洞研究》.pdf NASA-TN-D-4983-1969 Full-scale wind-tunnel investigation of static longtudinal and lateral characteristics of a light twin-engine airplane《轻型双发动机飞机静态纵向和横向特性的全比例风洞研究》.pdf
  • NASA-TN-D-5054-1969 Experimental pressure distributions on a 120 degrees cone at Mach numbers from 2 96 to 4 63 and angles of attack from 0 degrees to 20 degrees《当马赫数为2 96至4 63且攻角为.pdf NASA-TN-D-5054-1969 Experimental pressure distributions on a 120 degrees cone at Mach numbers from 2 96 to 4 63 and angles of attack from 0 degrees to 20 degrees《当马赫数为2 96至4 63且攻角为.pdf
  • NASA-TN-D-5095-1969 Noncavitating and cavitating performance of several low area ratio water jet pumps having throat lengths of 3 54 diameters《带有3 54直径咽喉区长度的若干低面积比的喷水泵不成穴和成穴性能》.pdf NASA-TN-D-5095-1969 Noncavitating and cavitating performance of several low area ratio water jet pumps having throat lengths of 3 54 diameters《带有3 54直径咽喉区长度的若干低面积比的喷水泵不成穴和成穴性能》.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