1、NASM 1312-1997 紧固件试验方法_STD.AIA/NAS NASM1322-ENGL 1977 0318743 L150537L1 700 II NASM13 12 29 August 1997 ADOPTION NOTICE NASM1312, “Fastener Test Methods” was adopted on 29 August 1997 for use by the Department of Defnse OD). Proposed changes by DoD activities must be submitted to the DoD Adopting Ac
2、tivity: Commander, Naval Air Warfare Center Aircraft Division, Code 4141OOB120-3 Highway 547, Lakehurst, NJ 08733-5100. DoD activities may obtain copies of this standard hm the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 191 11-5094. The private sector and
3、other Government agencies may purchase copies fiom the Aefospace Industries Association, 1250 Eye Street NW, Washington, DC 20005. NASM13 12 Should be used instead of MIL-STJ” lm, which was cancelled on 29 August 1997. Custodians: Navy - AS AirForce- 11 hy - AV Preparing.activity: Navy - AS (Project
4、 No. 53GPL0285) Review Activities: Navy - AS, SH Army - AV, AR Air FOXW - 11 DLA - IS COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Information Handling ServicesNATIONAL AEROSPACE STANDARD COPYRIGHT 1997 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC ALL RIGHTS R
5、ESERVED NASM1312 STANDARD PRACTICE FASTENER TEST METHODS THE INITIAL RELEASE OF THIS DOCUMENT SUPERSEDES MIL-STD-1312B DESIGNATIONS FOR THESE TEST METHODS REMAIN MIL-STD-13 12 FSC 53GP SHEET 1 OF 45 APPROVAL DATE AUGUST 1997 USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY AEROSPACE STANDARD IS ENTIRELY
6、 VOLUNTARY AIA DOES NOT QUALIFY SUPPLIERS OR CERTIFY CONFORMANCE OF ITEMS PRODUCED UNDER AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABILITY OF ITEMS FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TRADEMARK RIGHTS. CO
7、PYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Information Handling ServicesNATIONAL AEROSPACE STANDARD COPYRIGHT 1997 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, MC ALL RIGHTS RESERVED NASM1312 FOREWORD f 1. Background. The selection of fasteners in the design and c
8、onstruction phase of weapons systems and equipment and the analysis of fasteners used therein for parameters, such as suitability, standardization, and simplification requires the evaluation and correlation of test data and critefia. In evaluating these fbnctions, it has become increasingly evhent t
9、hat the data and criteria received from prime contractors, fastener producers, private laboratories, military documents, and military laboratories cannot be adequately correlated. The chief reason for this is the absence of unified standards prescribing test methods, procedures, fixtures, data analy
10、sis, and data presentation. This disparity encourages and often requires duplication of testing and reduces reliability of weapons systems and equipments, thereby impairing operations involving engineering control, design maintenance, quality assurance, standardization, and logistics simplification.
11、 To correct this situation it was established that a unified set of test methods and procedures is required to serve as a basic engineering tool for obtaining and presenting engineering data. As a result, this document was developed and prepared to satisQ this vital need. This standard delineates st
12、andard test methods, procedures, conditions, fixtures, and methods of recording, analyzing and presenting test data. The purpose of the resulting test data is to determine the capability of fasteners to withstand the various environmental and mechanical conditions encountered when used in military w
13、eapons systems. 2. Benefits. Many benefits are to be expected by unified standard tests for fasteners. The following is a list of benefits that can be expected to accrue from using this standard. a. Availability of testing techniques and criteria qecessary for the design and development of increasin
14、gly superior structural fasteners. In the past, when a new fastener was needed to solve a problem, the necessary test procedures had to be developed and written; also, the necessary fixtures had to be designed. This always imposed delays, additional expenses, variations in test methods and in test r
15、esults. b. Increasing incidences of correlation among fadtener test data and design engineering techniques and design criteria for weapons systems and equipments. As new systems are designed to achieve higher performance for a given volume and mass of material, it is essential that design data for s
16、tructural joints (a large portion of which is obtained by testing fasteners) maintain a i close correlation with engineering techniques and design criteria. Where weight is of importance, such as in aircraft structures, such close correlation will provide a substantial reduction in weight. SHEET 2 A
17、PPROVAL DATE AUGUST 1997 USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY AEROSPACE STANDARD IS ENTIRELY VOLUNTARY AIA DOES NOT QUALIFY SUPPLIERS OR CERTIFY CONFORMANCE OF ITEMS PRODUCED UNDER AEROSPACE STANDARDS, AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (I) THE SUITABILITY OF ITEMS FOR ANY PARTI
18、CULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY TIIERETO OF PATENT OR TRADEMARK RIGHTS. COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Information Handling ServicesNATIONAL AEROSPACE STANDARD QCOPYRIOHT 1997 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, MC
19、 ALL RIGHTS RESERVED NSM13 12 c. Availability of testing techniques and criteria necessary to maintain consistent quality in the procurement of fasteners. d. Reduction in the time and effort required for the development of procurement specifications for fasteners by having a series of standard tests
20、 available. e. Elimination of duplication in the development of test methods and documents by individual fastener producers, Government contractors, and military activities. f Elimination of duplication of effort in research and evaluation due to lack of unified standard test methods. When test meth
21、ods are not standard, results cannot be correlated; therefore, producers, prime contractors, and military activities will not accept each others results and will duplicate research, development, and evaluation work. g. For logistics simplification, fastener attributes must be reduced to a common den
22、ominator so that variation in type can be compared. Data and the presentation thereof, by means of this standard, will be provided in such form that various types and variations in types of fasteners may be compared to determine their degree of interchangeability, substitutability, and replaceabilit
23、y. h. Time and effort required to reach agreement in regard to specific engineering changes will be reduced by providing unified standard tests for use in evaluating new fasteners. i. This standard will provide a means forestablishing guidelines for evaluating fastener test data and engineering tech
24、niques. j. Industry and Government design personnel will become thoroughly indoctrinated in the use of a single standard prescribing unified standard test methods. ACKNOWLEDGMENT This standard was prepared by the Fastener Testing Development Group (FTDG), consisting of representatives of Government
25、agencies, engineering societies, trade associations, independent testing laboratories, the using industry, and the fastener producing industries. I SHEET 3 APPROVAL. DATE AUGUST 1997 USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY AEROSPACE STANDARD IS ENTIRELY VOLUNTARY AIA DOES NOT QUALIFY SUPPLIERS
26、OR CERTlFY CONFORMANCE OF ITEMS PRODUCED UNDER AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABILITY OF ITEMS FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TRADEMARK RIGHTS. COPYRIGHT Aerospace Industries Association o
27、f America, Inc. (AIA NAS)Licensed by Information Handling ServicesNATIONAL AEROSPACE STANDARD COPYRIGHT 1997 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC ALL RIGHTS RESERVED NASMl3 12 With the increased implementation of the International System of Units (SI) or metric system in military specifi
28、cations and standards, the Department of Defense OD) has approved its usage in this standard. Therefore, this issue, prepared under DoD Project Number 53GP-0142-20 by .the FTDG includes test methods in the SI and inch-pound (I-P) units. I SHEET 4 APPROVAL DATE AUGUST 1997 USE OF OK RELIANCE UPON THI
29、S WCUMENT OR ANY AEROSPACE STANDARD IS ENTIRELY VOLUNTARY AIA WES NOT QUALIFY SUPPLIERS OR CERTIFY CONFORMANCE OF ITEMS PRODUCED UNDER AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (I) THE SUITABILITY OF ITEMS FOR ANY PARTICULAR APPLICATION OR (1) THE EXISTENCE OF OR APPLICABI
30、LITY THERETO OF PATENT OR TRADEMARK RIGHTS. COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Information Handling ServicesNATIONAL AEROSPACE STANDARD COPYRIGHT 1997 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, MC ALL RIGHTS RESERVED NASM1312 TABLE OF CONTENTS f Paragr
31、aph 1. SCOPE 1.1 Applicability 2. REFERENCED DOCUMENTS 2.1 Government documents 2.1.1 Specifications, Standards and Handbooks 3. DEFINITIONS 4. GENERAL REQUIREMENTS 4.1 Test method numbering system 4.2 Document format structure 4.3 Method of revision 4.3.1 Revision to test method number 4.4 Selectio
32、n of tests 4.5 Method of reference 5. DETAIL REQUIREMENTS APPENDICES Appendix 6 6 6 6 6 7 9 A List of available Test Methods in I-P system of measurement 10 B List of available Test Methods in SI system of measurement 11 C Alignment and load verification of axial-load fatigue testing machines 12 SHE
33、ETS APPROVAL DATE AUGUST 1997 USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY AEROSPACE STANDARD IS ENTIRELY VOLUNTARY AIA DOES NOT QUALIFY SUPPLIERS OR CERTIFY CONFORMANCE OF ITEMS PRODUCED UNDER AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABILITY OF ITEMS FOR ANY
34、PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TRADEMARK RIGHTS. COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Information Handling ServicesNATIONAL AEROSPACE STANDARD COPYRIGHT 1997 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA,
35、 INC ALL RIGHTS RESERVED NASM13 12 1. SCOPE 1: 1.1 Applicability. This standard establishes methods for testing fasteners, covering both the SI and I-P units, to determine their physical and mechanical properties. These standard test methods will yield reproducible data for use in research, developm
36、ent, procurement or product application. These test methods shall be observed when specifically referenced in the applicable documents. In case of conflict between the provisions of these methods and the individual test procedure in the specification for a particular item, the latter shall take prec
37、edence. This document exists as a dynamic standard subject to addition and change as reflected by the state- of-the-art. 2. REFERENCED DOCUMENTS 2.1. Government documents. 2.1.1 Specifications. standards and handbooks. Unless otherwise specified, the following specifications, standards and handbooks
38、 of the issue listed in the current Department of Defense Index of Specifications and Standards (DoDISS) and the supplement thereto (if applicable), form a part of this standard to the extent specified herein. STANDARDS MILITARY MIL-STD-962 Outline of Forms and Instructions for the Preparation of Mi
39、litary Standards and Military Handbooks i 2.1.2 Documents applicable to a particular test method bookform standard part or section shall be listed therein. (Copies of specifications, standards, handbooks, drawings, and publications required .by contractors in connection with specific acquisition fbn
40、ctions should be obtained fiom the contracting activity or as directed by the contracting officer.) ! SHEET 6 APPROVAL DATE AUGUST 1997 USE OF OR RELIANCE UPON THlS DOCUMENT OR ANY AEROSPACE STANDARD IS ENTIRELY VOLUNTARY AIA DOES NOT QUALlFY SUPPLIERS OR CERTIFY CONFORMANCE OF lTEMS PRODUCED UNDER
41、AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTINO (1) THE SUITABILITY OF ITEMS FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TRADEMARK RIGHTS. COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Informatio
42、n Handling ServicesNATIONAL AEROSPACE STANDARD COPYRIGHT 1997 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, MC ALL RIGHTS RESERVED NASM1312 3. DEFINITIONS 4 3.1 SI - The International System of Units (from the French Le Systeme International dUnites), as modified for use in the United States by the S
43、ecretary of Coinmerce. 3.2 Inch-pound units - Units based upon the yard and the pound commonly used in the United States of America and defined by the National Bureau of Standards. Note-that units having the same names in other countries may differ in magnitude. 3.3 Definitions applicable to a parti
44、cular test method bookform standard part or section shall be listed therein. 4. GENERAL REQUIREMENTS 4.1 Test method numbering svstem. This standard consists of a general basic document and supporting parts or sections. Each part addresses a specific test method which is designated by a dash number
45、commencing with number 1 for the I-P system of measurement and number 101 for the SI system of measurement. A different dash number is assigned to each test method. 4.2 Document format structure. Each test method is prepared as an individual document in the format of a bookform standard in accordanc
46、e with the guidelines of MIL-STD-962. The individual bookform standard part is identified by the basic document identifier, MIL-STD-13 12 for the I-P system of measurement and DOD-STD-13 12 for the SI system of measurement, followed by a sequential dash number. The dash number is identical to the nu
47、mber of the test method. Examples: I-P System 7-Dash number Test Method No. l, Salt Spray, MIL-STD-13 12-1 -T- I Document identifier assigned to the basic standard SI Svstem ! DOD-STD- 1 3 12- 1 O 1 Dash number Test Method No. 101, Salt Spray , I Document identifier assigned to the basic standard SHEET 7 APPROV
