ANSI ASME Y14.37-2012 Composite Part Drawings《合成零件图》.pdf

《ANSI ASME Y14.37-2012 Composite Part Drawings《合成零件图》.pdf》由会员分享，可在线阅读，更多相关《ANSI ASME Y14.37-2012 Composite Part Drawings《合成零件图》.pdf（36页珍藏版）》请在麦多课文档分享上搜索。

1、AN AMERICAN NATIONAL STANDARD ASME Y14.37-2012Composite Part DrawingsEngineering Drawing and Related Documentation PracticesASME Y14.37ADOPTION NOTICEASME Y14.37, Composite Part Drawings, was adopted on 27 April 2012 for use by the Department of Defense(DoD). Proposed changes by DoD activities must

2、be submitted to the DoD Adopting Activity: Commander,U.S. Army ARDEC, ATTN: RDAR-QES-E, Picatinny Arsenal, NJ 07806-5000. Copies of this document may bepurchased from The American Society of Mechanical Engineers (ASME), 22 Law Drive, PO Box 2900, Fairfield,NJ 07007-2900; http:/www.asme.org.Custodian

3、s: Adopting Activity:Army AR Army ARNavy SAAir Force 16 (Project DRPR-2012-002)Review Activities:Army AV, CR, MI, PT, TE, TMNavy AS, CG, CH, MC, NPAir Force 04, 13, 99OSDSENGAMPNSANSDLA DH, ISNOTE: The activities listed above were interested in this document as of the dateof this document. Since org

4、anizations and responsibilities can change, you shouldverify the currency of the information above using the ASSIST Online databaseat http:/assist.daps.dla.mil.AMSC N/A FSC DRPRDISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.ASME Y14.37-2012Composite PartDrawingsEngi

5、neering Drawing and RelatedDocumentation PracticesAN AMERICAN NATIONAL STANDARDThree Park Avenue New York, NY 10016 USADate of Issuance: June 15, 2012This Standard will be revised when the Society approves the issuance of a new edition.Periodically certain aspects of the ASME Y14 Committee may be pu

6、blished as Cases. Cases arepublished on the ASME Web site under the Committee Pages at http:/cstools.asme.org/ as they arepublished.Errata to codes and standards may be posted on the ASME Web site under the Committee Pages toprovide corrections to incorrectly published items, or to correct typograph

7、ical or grammatical errorsin codes and standards. Such errata shall be used on the date posted.The Committee Pages can be found at http:/cstools.asme.org/. There is an option available toautomatically receive an e-mail notification when errata are posted to a particular code or standard.This option

8、can be found on the appropriate Committee Page after selecting “Errata” in the “PublicationInformation” section.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 Nation

9、alStandards. The Standards Committee that approved the code or standard was balanced to assure that individuals fromcompetent and concerned interests have had an opportunity to participate. The proposed code or standard was madeavailable for public review and comment that provides an opportunity for

10、 additional public input from industry, academia,regulatory agencies, 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

11、 with anyitems mentioned in this document, and does not undertake to insure anyone utilizing a standard against liability forinfringement of any applicable letters patent, nor assumes any such liability. Users of a code or standard are expresslyadvised that determination of the validity of any such

12、patent rights, 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 asgovernment or industry endorsement of this code or standard.ASME accepts responsibility f

13、or only those interpretations of this document issued in accordance with the establishedASME procedures and policies, which precludes the issuance of interpretations by individuals.No part of this document may be reproduced in any form,in an electronic retrieval system or otherwise,without the prior

14、 written permission of the publisher.The American Society of Mechanical EngineersThree Park Avenue, New York, NY 10016-5990Copyright 2012 byTHE AMERICAN SOCIETY OF MECHANICAL ENGINEERSAll rights reservedPrinted in U.S.A.CONTENTSForeword ivCommittee Roster . vCorrespondence With the Y14 Committee vi1

15、 Scope . 12 References 23 Definitions 24 Part Identification 35 Parts List Requirements 76 Composite Part Definition Requirements. 77 Ply Definition Requirements 78 Ply Stackup Views . 79 Ply Table 710 Opposite Parts. 1211 Revisions 1212 Manufacturing Process Requirements 12Figures3-1 Ply Definition

16、 43-2 Composite Part Process . 67-1 Ply Orientation Symbols 87-2 Multiple Ply Orientation Symbol 99-1 Typical Ply Table . 109-2 Ply Table Multiple Orientation Symbol . 1110-1 Same Ply Orientation Symbol . 1310-2 Opposite Ply Orientation Symbol . 1310-3 Opposite Shape With Identical Ply Orientation i

17、n Same View 1410-4 Opposite Shape With Opposite Ply Orientation in Same View 1512-1 Filament Winding Part 1612-2 Multistage Bonding Precured Method 1712-3 Multistage Bonding Precured With Additional Layup Method 1812-4 Multistage Bonding Layup Method 2012-5 Pultruded Part . 2112-6 Pultrusion Materia

18、l Roll Cross Section 22iiiFOREWORDThis Standard establishes engineering practices for the definition of Composite Parts andtogether with related documentation practices in the Y14 Series will enable full composite partdefinition.When this Standard is specified as a requirement, its defined requireme

19、nts are assumed to beconsistent with the needs of the user. Therefore, each user provides appropriate applicationconsistent with the environment in which it is applied. Those who use this Standard as a require-ment for contractual purposes should keep the following facts in mind:(a) This Standard sh

20、ould be tailored to meet any specific needs. All users shall take carefulnote of the necessity of tailoring this Standard and the contents. The extent of tailoring will inlarge part be governed by drawing ownership and the logistics intent.(b) It is not the intent of this Standard to prevent individ

21、ual organizations from designingspecific drawing practices that meet their individual needs, but rather to provide common engi-neering delineation standards to aid the increasing interchange of drawing among industry,government, and other users.It is well recognized that individual companies have ma

22、ny detailed requirements for theirspecific method of operation. Consequently, the minimum requirements set forth in this Standardwill provide them flexibility in implementation.The successful creation and release of this Standard is attributed to the subcommittee membersand their respective companie

23、s.Suggestionsfor improvementofthis Standardarewelcome. Theyshouldbe senttothe AmericanSociety of Mechanical Engineers; Attn: Secretary, Y14 Standards Committee; Three Park Avenue;New York, NY 10016-5900.This Standard was approved as an American National Standard on April 10, 2012.ivASME Y14 COMMITTE

24、EEngineering Drawing and Related Documentation Practices(The following is the roster of the Committee at the time of approval of this Standard.)STANDARDS COMMITTEE OFFICERSF. Bakos, Jr., ChairW. A. Kaba, Vice ChairC. J. Gomez, SecretarySTANDARDS COMMITTEE PERSONNELA. R. Anderson, Dimensional Dynamic

25、s, LLCF. Bakos, Jr., ConsultantJ. V. Burleigh, ConsultantD. E. Day, TEC-EASE, Inc.K. Dobert, Siemens PLM Software, Inc.C. J. Gomez, The American Society of Mechanical EngineersB. A. Harding, Purdue UniversityD. H. Honsinger, ConsultantW. A. Kaba, Spirit AeroSystems, Inc.A. Krulikowski, Effective Tra

26、ining, Inc.E. F. McCarthy, Raytheon Missile SystemsSUBCOMMITTEE 37 COMPOSITE PART DRAWINGSW. A. Kaba, Chair, Spirit AeroSystems, Inc.J. D. Bennett, Bell HelicopterD. O. Coon, Bell HelicopterL. G. Davis, ConsultantJ. A. Gagnon, Hamilton Sundstrand Corp.W. S. Gold, The Boeing Co.J. B. Hoskins, The Boe

27、ing Co.vP. J. McCuistion, Ohio UniversityJ. D. Meadows, James D. Meadows Order Department: 22 Law Drive, P.O.Box 2900, Fairfield, NJ 07007-2900 (www.asme.org)2MIL-HDBK-17, Composite Materials HandbookPublisher: Department of Defense Single Stock Point(DODSSP), 700 Robbins Avenue, Building 4D,Philade

28、lphia, PA 19111-5094. Copies are availableon-line at http:/assist.daps.dla.mil/quicksearch/.3 DEFINITIONSThe following terms are defined as their use appliesin this Standard.3.1 Adhesiveadhesive: a substance capable of holding two materialstogether by surface attachment (MIL-HDBK-17).3.2 Annotationa

29、nnotation: dimensions, tolerances, notes, text, or sym-bols visible without any manual or externalmanipulation (ASME Y14.41).3.3 Bandband: the width of the collection of tows or prepreg tapethat a machine can lay down on the work surface.3.4 Bondbond: the adhesion of one surface to another, with orw

30、ithout the use of an adhesive as a bonding agent(MIL-HDBK-17).3.5 Braid Anglebraid angle: the acute angle measured from the axis ofbraiding (MIL-HDBK-17).3.6 Braid, Biaxialbraid, biaxial: braided fabric with two-yarn systems, onerunning in the +0 direction, the other in the 0 directionas measured fr

31、om the axis of braiding (MIL-HDBK-17).3.7 Braid, Triaxialbraid, triaxial: a biaxial braided fabric with laid-in yarnsrunning in the bias of braiding (MIL-HDBK-17).3.8 Braidingbraiding: a textile process where two or more strands,yarns, or tapes are intertwined in the bias direction toform an integra

32、ted structure (MIL-HDBK-17).3.9 Cocuredcocured: simultaneously cured and bonded to anotherprepared surface.3.10 Composite Materialcomposite material: a material made by imbedding loadcarrying fibers within an essentially homogeneous resinmatrix.ASME Y14.37-20123.11 Composite Partcomposite part: an i

33、nseparable assembly of compositematerial(s) that may include noncomposite material(s).See Fig. 3-1, illustrations (a) and (b).3.12 Corecore: an internal item of a sandwich construction towhich the sandwich faces or skins are attached.3.13 Core Ribbon Directioncore ribbon direction: an indicator that

34、 shows the directionof maximum shear strength and rigidity along the con-tinuous webs of material.3.14 Curecure: to change the properties of a thermosetting resinirreversibly by chemical reaction. Cure may be accom-plished by addition of curing agents, with or withoutcatalyst, and with or without he

35、at and pressure(MIL-HDBK-17).3.15 EOPEOP: end of part.3.16 EOPMEOPM: edge of ply material.3.17 Helical (Helix) Plyhelical (helix) ply: two windings, one for each of theplus/minus orientations.3.18 Laminatelaminate: the product resulting from the uncured buildupof two or more ply levels of material.

36、See Fig. 3-2.3.19 Plyply: one discrete piece of manufactured material suchas fabric, tape, adhesive film, etc. See Fig. 3-2.3.20 Ply Drop-Offply drop-off: when the edge of ply material (EOPM) doesnot correspond with the end of part (EOP) and endsinside the EOP.3.21 Ply Identificationply identificati

37、on: a temporary identification that is nota part or identifying number in accordance withASME Y14.100.3.22 Ply Levelply level: the relative position from the tool surface ofone or more discrete materials or plies in a laminate.See Fig. 3-2.3.23 Ply Orientationply orientation: the direction of the re

38、inforcing fiberwithin a laminate that may be at any angle but are3normally 0 deg, 90 deg, +45 deg, or 45 deg relative toa fixed reference direction on the part as indicated bya ply orientation symbol.3.24 Ply Stackup Viewply stackup view: a view representing the ply level rela-tionship of each ply a

39、nd other items within the laminate.3.25 Ply Tableply table: a table annotating the plies and items that areapplicable to a composite part. See Fig. 9-1.3.26 Preformpreform: an assembly of dry fabric and fibers that hasbeen prepared for one of several different wet resin injec-tion processes. A prefo

40、rm may be stitched or stabilizedin some other way to hold its shape. A commingledpreform may contain thermoplastic fibers and may beconsolidated by elevated temperature and pressurewithout resin injection.3.27 Rovingroving: a number of strands, tows, or ends collected intoa parallel bundle with litt

41、le or no twist. In spun yarnproduction, an intermediate state between sliver andyarn.3.28 Sequencesequence: denotes a sub-bond configuration (groupingof plies) for design definition/clarity. It may also beused, when specified, to define the manufacturing pro-cess (i.e., to tie groups of plies to spe

42、cific tooling orprocess methodologies).3.29 Tool Sidetool side: the surface of the item adjacent to the toolsurface.3.30 Tool Side Viewtool side view: a viewing direction looking through thepart towards the tool surface.3.31 Towtow: an untwisted bundle of continuous filaments. Com-monly used in refe

43、rringto man-made fibers, particularlycarbon and graphite fibers, in the composites industry(MIL-HDBK-17).4 PART IDENTIFICATIONAssign a Part or Identifying Number (PIN) in accor-dance with ASME Y14.100. A PIN is not required forindividual plies. For ply identification, see para. 7.1.ASME Y14.37-2012F

44、ig. 3-1 Ply Definition4ASME Y14.37-2012Fig. 3-1 Ply Definition (Contd)5ASME Y14.37-2012Fig. 3-2 Composite Part Process6ASME Y14.37-20125 PARTS LIST REQUIREMENTSPrepare parts list in accordance with ASME Y14.34.Material for each ply of the part may be specified in theNOTES column by reference to the

45、ply table such asSEE PLY TABLE.6 COMPOSITE PART DEFINITION REQUIREMENTSComposite part definition shall contain all datarequired to define a part as follows:(a) Provide a tool side view.(b) Complete surface definition(s).(c) Show the part in the finished condition includingvariations due to ply drop-

46、off, core shape, etc. SeeFig. 3-1.(d) Ply orientation symbol(s). See para. 7.3.(e) Dimensioning and tolerancing in accordance withASME Y14.5 and ASME Y14.41.(f) Complete ply definition including internal cutoutsand perimeters of each ply. See Fig. 3-1.(g) Supplementary views and ply stackup views as

47、required.(h) Annotations.(i) Ply table.(j) Identify tool side(s) on each part.(k) Where used, identify the honeycomb core ribbondirection on the tool side view. See Fig. 3-1.(l) Manufacturing process specification.NOTE: Composite parts are highly dependent on the manufac-turing process utilized. Pro

48、cess parameters such as cure and postcure cycles, splices and darts, orientation deviation, temperatureramp rate, thermal soak cycles, vacuum, pressure, material condi-tioning, and manufacturing environment can all have significantimpact on the end product performance. Because verification ofendprod

49、uctscanyieldincompleteinformationastoproperfabrica-tion, a process specification should be used to define and controlthe manufacturing variables.7 PLY DEFINITION REQUIREMENTS7.1 Ply IdentificationEach ply shall be identified with a separate ply identi-fier regardless of configuration or orientation. Seepara. 3.21.7.2 Ply Size and LocationThe definition of each ply shape shall include clearindications of the edges of each ply within the laminate.Ply location within the laminate shall be shown. SeeFig. 3-1. Developed ply flat patterns are optional forde