ASME B1 15-1995 Unified Inch Screw Threads (UNJ Thread Form)《统一标准的英制螺纹(UNJ 螺纹形状)》.pdf
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1、I AN ASME STANDARD Unified Inch Screw Threads (UNJ Thread Form) The American Society of I I Mechanical Engineers L I I 345 East 47th Street, New York, N.Y. - Date of Issuance: August 15, 1995 This Standard will be revised when the Society approves the issuance of a new edition. There will be no adde
2、nda or written interpretations of the requirements of this Standard issued to this Edition. ASME is the registered trademark of The American Society of Mechanical Engineers. This code or standard was developed under procedures accredited as meeting the criteria for American National Standards. The C
3、onsensus Committee that approved the code or standard was balanced to assure that individuals from competent and concerned interests have had an opportunity to participate. The proposed code or standard was made available for public review and comment which provides an opportunity for additional pub
4、lic input from industry, academia, regulatory agen- cies, and the public-at-large. ASME does not “approve,“ “rate,“ or “endorse“ any item, construction, proprietary device, or activity. ASME does not take any position with respect to the validity of any patent rights asserted in connection with any
5、items mentioned in this document, and does not undertake to insure anyone utilizing a standard against liability for infringement of any applicable Letters Patent, nor assume any such liability. Users of a code or standard are expressly advised that determination of the validity of any such patent r
6、ights, and the risk of infringement of such rights, isentirely their own responsibility. Participation by federal agency representative(s) or person(s) affiliated with industry is not to be interpreted as government or industry endorsement of this code or standard. ASME accepts responsibility for on
7、ly those interpretations issued in accordance with governing ASME procedures and policies which preclude the issuance of interpretations by individual volun- teers. No part of this document may be reproduced in any form, in an electronic retrieval system or otherwise, without the prior written permi
8、ssion of the publisher. Copyright O 1995 by THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS All Rights Resewed Printed in U.S.A. FOREWORD (This Foreword is not part of ASME 81.15-1995.) This Standard is similar to Military Specification MIL-S-8879 and equivalent to ISO- 3161-1977 for thread Classes 3A
9、and 3B. British Standard BS 4084: 1978 including Amend- ment 1 is technically identical to ISO-3161-1977 except for Appendix A which provides information for a 20 UNJ constant pitch series for diameters through 3 inches. The UNJ thread form, having the enlarged root radius in the external thread, wa
10、s introduced for applications requiring high fatigue strength where working stress levels are high, in order to minimize size and weight in parts, as in aerospace applications and also for other designs in commercial products where stresses are critical. To meet these requirements, the UNJ external
11、thread root radius is designed between 0.1501 1Pto 0.18042P and the minor diameter of the mating internal thread is increased to ensure the necessary clearance. This Standard includes Classes 2A and 2B UNJ screw threads. Either Class 3 or Class 2 UNJ threads are appropriate for commercial applicatio
12、ns commensurate with the fatigue and stress levels required. It is not recommended that Classes 2A and 2B threads be used for aerospace applications. Only UNJ thread Classes 3A and 3B meet the requirements of Military Specification MIL- S-8879. NOTE: In what follows, the symbols Hand h are used. His
13、 defined as the height of the sharp vee thread formed by extending the thread flanks until they meet. H is equal to.0.866025 times the pitch, P. The symbol h is equal to 0.75 times H and represents the theoretical height of the American National thread form. It is still used as the basis for the val
14、ue called percent of thread. The UNJ thread form is the UN thread form modified to 9/1a H or 75% h basic thread depth which allows the 0.18042P maximum root radius in the external thread. The first known U.S. standard of similar thread form was the Society of Automotive Engineers Aeronautical Standa
15、rd AS 82 published in March 1942, which is a modified American National thread form to 75% h basic thread depth and specifying 0.108P-0.180P root radius in the external thread. This thread was symbolized NR, National Round, and was developed for aircraft engine applications. Tension-tension fatigue
16、testing of aircraft fasteners in 1942 demonstrated the importance of the external thread root contour in the fatigue life of a screw thread rolled after heat treatment. Fatigue testing isolated the following elements of good external thread root design: The root should be radiused, not sharp. Theore
17、tically, it should be a continuous circular arc, blending smoothly with the thread flanks. The radius should be as large as possible within the allowable design form. The root contour should be smooth throughout, free of any imperfections, tool marks, or other minor notches. Recognizing the need for
18、 improved 160,000 psi tensile strength bolts, the Military Services published in April 1952, MIL-B-7838A bolt procurement specification for aircraft applications based on the Unified thread form having 83/3% h Unified thread form. Thus, larger external root radius requires a shallower internal threa
19、d depth to clear the flank tangency point. Although the Unified internal thread standards for tap drill sizes permit depths of more than 75,% h, production rarely used these drills because deeper tapping of internal threads is generally not considered economically practical. A few internal threads h
20、ave depths as great as 70% h, but the vast majority lie between 60% and 68% h. Since internal threads are generally less than 75% h basic thread depth, the root radius of the external thread was increased to 0.150P min. and 0.180P max. for the 180,000 psi and higher tensile strength bolts. This exte
21、rnal thread form was developed in 1955 by the aerospace fastener industry and was known as the “Hi R“ thread form. Through the coordinated effort with the Aerospace Engine and Propeller Utility Stan- dards parts Committee E25 of SAE and the AIA National Aerospace Standards Committee NASC, the Air Fo
22、rce and Navy developed and published in September 1960, the thread specification MIL-S-8879 which features the “Hi R“ thread root radius in the external thread and the internal thread modified to 9/6 H basic or 75% h thread depth. With the advent of aircraft gas turbine engines, the high temperature
23、 threaded fasteners developed better elevated temperature performance using MIL-S-8879 UNJ thread root radius, in that the stress-rupture life of bolts was greatly improved. The UNJ thread form has been adopted by the aerospace industry as the all-purpose thread standard, with the exception of elect
24、rical hardware and thread sizes 0.138 and smaller, which may use the UN thread form. Suggestions for improvement of this Standard will be welcome. They should be sent to The American Society of Mechanical Engineers, Att: Secretary, B1 Main Committee, 345 East 47th Street, New York, NY 10017. This St
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