ASD-STAN PREN 3005-1989 Aerospace Series Nuts Self-Locking in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Classification 1210 MPa 730 Degrees Celsius Technical Specificat.pdf
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1、AECMA PREN3005 87 10L231L 000LLb05 T W - A. E .C .M .A. STAN DARD NORME A.E.C.M.A. A.E.C.M.A. NORM prEN 3006 Issue P 1 April 1989 DITE PAR LASSOCIATION EUROPENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL 88, boulevard Malesherbes. 75008 PARIS - TL. 45-63-82-85 UDC : Key words : ENGLISH VERSION Aerospa
2、ce series Nuts, self-locking, in heat resisting nickel base alloy NI-PI O1 HT (Waspaloy) Classification : I21 O MPa/730 OC Technical specification Srie arospatiale crous, auto-freinants en alliage base nickel rsistant chaud NI-PIO1 HT (Waspaioy) Classification : 121 O MPa/730 OC Spcification techniq
3、ue Luft- und Raumfahrt Muttern, selbstsichernd aus hochwarmfester Nickel basislegierung NI-PT01 HT (Waspaloy) Klasse : 121 O MPa/730 OC Technische Lieferbedngungen This Aerospace Series) pre-standard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matr
4、iel Arospatial). It is published on green paper for the needs of AECMA-Members. it has been technically approved by the experts of the concerned AECMA Commission following comment by the Member countries. Subsequent to the publication of this pre-standard, the technical content shall not be changed
5、to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft E
6、uropean Standard to CEN (European Committee for Standardization) for final vote. Nota - Extra copies can be supplied by B.N.A.E. - 8, rue Moreau-Vauthier - 92100 BOULOGNE-BILLANCOURT Edition approved for publication Comments should be sent within six months C8 Chairman Mr WILLIAMS after the date of
7、publication decision 88, Bd. Malesherbes 25th April 1989 A.E.C.M.A. 75008 PARIS - FRANCE aecrna 1989 Contents. i). Scope and field of application 2). References 3). Definitions 3.1). Production batch. 3.2). Inspection lot. 3.3). Discontinuities. 3.4). Test temperature. 3.5). Simple random sampling.
8、3.6). Critical defect. 3-7)- Major defect. 3.8). Minor defect. 3.9). Sampling plan. 3.10).Limiting quality. 3.ii).Acceptable quality level 3.12).Finished nut. 3.13).Definition document. 3.141.Self locking torque. 3.15).Seating torque. 3.16).Unseating torque. 3.171.Breakaway torque. 3.181.Wrench torq
9、ue. AECMA PREN3005 87 LOL23Ll 0004bOb L 9 I prEN3005 Page 2 4).Certification and quality assurance. 4.1). Qualification. 4.2). Acceptance. 4.3). Quality system certification. 4.4). Responsibility for inspection and tests. 4.5). Inspection and test report. S).Table I : Technical requirement and test
10、methods. 5.1). Materials. 5.2). Dimensions;tolerances of form and position; 5.3). Manufacturing. 5.4). Mechanical properties. 5.5). Metallurgical properties. 5.6). Product identification. 5.7) . Delivery. Table 2.: Summary of tests-Qualification and Table 3.: Qualification testing requasentents for
11、Table 4.: Load values os Axial strength: Wrench threads and quality production acceptance. nut samples. torque; Push out; Torque out and Tight- ening torque for accelerated vibratisn. torque and Assembly torque. Table 5.: Values for Breakaway torque;locking Table 6.: Classification of defects. Table
12、 7.: Sampling plans for visual inspections and Table 8.: Sampling plans for the inspection of dimensional characteristics- mechanical and metallurgical characteristics. Table 9.: Maximum depth of permissible discontinuities. I a O 1.Scope and field of application This standard specifies tRe technica
13、l; quaLifacation and quaity assurance requirements for self lockfng nuts En material NI-PlOi-HT(Waspa1oy) of tensile strength class 1210MPa. at room temperature, maximum test temperature of material 730 C. Primarily for Aerospace applications it is applicable to such self locking nuts when reference
14、d on the product standard or drawing. 2-References IS0 2859-1 Is0 3452 Is0 3453 IS0 3534 IS0 8642 IS0 9002 EN 2002-8 EN 2959 EN 2960 EN 3039 EN 3041 EN 3042 EN 3220 CN/TR 3040 Sampling procedures for inspection by attributes - Part 1: Sampling plans indexed by acceptable quality level(AQL) for lot b
15、y lot inspection. 4)- Non destructive testing - Penetrant inspection - General principles Non destructive testing - Liquid penetrant inspection - Means of verification Statistics - Vocabulary and symbols Aerospce - Fasteners - self locking nuts with maximum operating temperature greater than 425OC -
16、 test methods. Quality systems - Model for quality assurance in production and installation. Aerospace Series - Test methods for metallic materials - Part 8 - Micrographic determination of grain size, i). Aerospace Series - Heat resisting nickel base alloy NL-P101-HT - Solution treated and cold work
17、ed - Bars for hot upset forging for fasteners. 2). Aerospace Series - Heat resisting nickel base alloy NI-PlO1-HT - Cold worked and solution treated - Bars for machining for fasteners. 2). Aerospace series - Quality systems: supplementary requirements to IS09002 applicable to the manufacture/process
18、ing of materiel for propulsion standard parts. 3). Aerospace series - Propulsion standard parts - Manufacturing process - change procedure for qualified parts. 3). Aerospace series - Propulsion standard parts - Qualification procedure. 2). Aerospace Series - Heat resisting nickel base alloy NI-Pli-H
19、T - Cold worked and softened - Ear and wire for continuous cold forging or extrusion of fasteners. 2). : Aerospace series - Propulsion standard parts - Qualification - List of qualified manufacturers. 3). i) published as AEm standard 2) Published as AEW pre-standard 3) in cwrse of preparation 4) At
20、present at the stage of draft.(Revicion, in part of Is0 2859-1974 AECMA PREN3005 87 m LOL23Ll 0004b08 5 m i prEN3005 Page 4 3. ef initions. 3.1 Production batch: Quantity of finished nuts fabricated by the same process from a single material cast(sing1e heat of alloy),having the same basic part numb
21、er and diameter, heat treated together to the same specified condition and produced as one continuous run. 3.2 Inspection lot: Consists of nuts from a single production batch of the same part number which completely defines the nut. 3.3 Discontinuities. 3.3.1 Crack: Rupture in the material which may
22、 extend in any direction and which may be intercrystalline or transcrystalline in character. an unwelded open fold in the material. fins or sharp corners and then rolling or forging them into the surface. the material making process. They may exist as discrete particles or strings of particles exten
23、ding longitudinally. 3.3.2 Seam: Longitudinal surface defect in the form of 3.3.3 Lap: Surface defect caused by folding over metal 3.3.4 Inclusion: Non-metallic particles originating from 3.4 Test temperature: Ambient temperature, unless otherwise specified 3.5 Simple random sampling I): The taking
24、of n items from a population of N items in such a way that all possible combinations of n items have the same probability of being chosen. 3.6 Critical defect i): A defect that according to judgement and experience, is likely to result in hazardous or unsafe conditions for individuals using, maintai
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