ASD-STAN PREN 3152-1989 Aerospace Series Propulsion Standard Parts Nuts Self-Locking in Heat Resisting Steel FE-PA92HT (A286) Classification 1100 MPa 425 Degrees Celsius Technical .pdf
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1、A. E. C. M. A. STAN DARD NORME A.E.C.M.A. A.E.C.M.A. NORM prEN 3152 Issue P 1 April 1989 DIT PAR LASSOCIATION EUROPENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL 88, boulevard Malesherbes, 75008 PARIS -TL. 45-63-82-85 UDC : Key words : ENGLISH VERSION Aerospace series Propulsion standard parts Nuts, s
2、elf-locking, in heat resisting steel Classification : I I O0 MPa/425 OC Technical specification FE-PA92HT (A286) Srie arospatiale Pices normalises pour la propulsion crous, auto-freinants en acier rsistant chaud Classification : 11 O0 MPa/425 OC Spcification technique FE-PA92HT (A286) Luft- und Raum
3、fahrt Genormte Antriebsteile Muttern, selbstsichernd aus hochwarmfestem Stahl Klasse : 1 1 O0 MPa/425 OC Technische Lieferbedingungen FE-PA9SHT (A286) This Aerospace Series pre-standard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matriel Arospatial
4、). It is published on green paper for the needs of AECMA-Members. It has been technically approved b y 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 to an extent
5、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 European Stand
6、ard 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 after the date of publication decision 25th
7、 April 1989 A.E.C.M.A. Mr WILLIAMS 88, Bd. Malesherbes 75008 PARIS - FRANCE 0 aecma 1989 prEN3152 Page2 Contents - i). Scope and field of application 2). References 3). Definitions 3-11. Production batch. 3.2). Inspection lot. 3.3). Discontinuities. 3.4). Test temperature. 3.5). Simple random sampli
8、ng. 3.6). Critical defect- 3.7). Major defect. 3.8). Minor defect. 3.9)- Sampling plan. 3.lO).Lmiting quality. 3.1l).Acceptable quality level. 3.12l.Finished nut. 3.13).Definition document. 3.14).Self locking torque. . 3.151.Seating torque. 3.16)-Unseating torque. 3.17).Breakaway torque. 3.18).Wrenc
9、h torque. 41.Certification and quality assurance. 4.1). Qualification. 4.2). Acceptance. 4.3). Quality system certification. 4.41- Responsibility for inspection and tests. 4.5). Inspection and test report. 5).Table 1 : Technical requirement and test methods. 5.1). Materials. 5.2). Dimensions;toleran
10、ces of form and position; 5.3). Manufacturing. 5.4). Mechanical properties. 5-51. Metallurgical properties. 5.6). Product identification. 5 - 7 . Deliverv. threads and quality Table 2. : Table 3. : Table 4. : Table 5. : Table 6. : Table 7. : Table 8. : Table 9. : Summary of tests-Qualification and p
11、roduction acceptance- Qualification testing requirements for nut samples. Load values for Axial strength: Wrench torque; Push out; Torque out and Tight- ening torque for accelerated vibration. Values for Breakaway torque;locking torque and Assembly torque. Classification of defects. Sampling plans f
12、or visual inspections and dimensional characteristics. Sampling plans for the inspection of mechanical and metallurgical characteristics. Maximum depth of permissible discontinuities. AECMA PREN3152 87 10123L1 0004735 9 W prEN3152 Page3 1.Scope and field of application This standard specifies the te
13、chnical; qualification and quality assurance requirements for self locking nuts in material FE PAgS-HT(A286) of tensile strength class 1100MPa. at room temperature, maxiym test temperature of nuts to this specification 425 C. Primarily for Aerospace applications it is applicable to such self locking
14、 nuts when referenced on the product standard or drawing. 2.References IS0 2859-1 IS0 3452 Is0 3453 IS0 3534 IS0 7481 IS0 9002 EN 2002-8 EN 2398 EN 2399 EN 3039 EN 3041 EN 3042 EN 3638 EN 3639 CN/TR 3040 Sampling procedures for inspection by attributes - Part i : Sampling plans indexed by acceptable
15、 quality level (AQL) for lot by lot inspection. 4). Non destructive testing - Penetrant inspection - General principles Non destructive testing - Liquid penetrant inspection - Means of verification Statistics -Vocabulary and symbols Aerospace - Fasteners - self locking nuts with maximug operating te
16、mperature less than or equal to 425 C - 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). Heat resisting steel FE-PA92HT - Rm equal to or greater t
17、han 900MPa. bars for machined bolts - D equal to or less than 25mm - Aerospace Series. i). Heat resisting steel FE-PA92HT -Rm equal to or greater than 900MPa. bars for forged bolts - D equal to or less than 25mm - Aerospace Series. I). Aerospace series - Quality systems: supplementary requirements t
18、o IS09002 applicable to the manufacture/processing 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 ser
19、ies - Heat resisting alloy FE-PA92HT - solution treated - Sheet and strip. 3). Aerospace series - Heat resisting steel FE-PA92HT - cold worked and softened - Bar and Wire for the continuous forging or extrusion for fasteners. 3). Aerospace series - Propulsion standard parts - Qualification: List of
20、qualified manufacturers. 3). i) Published as AEM standard 2) Published as AEW pre-standard 3) In ccurse of preparation 4) At present at the stage of draft.(Revision, in part of IC0 28594974.) I AECMA PREN3152 89 W 1012311 000493b O prEN3152 Page4 3. De initions. 3.1 Production batch: Quantity of fin
21、ished nuts fabricated by the same process from a single material cast(s2ngle heat of alloy),having the same basic part number 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
22、 the same part number which completely defines the nut. 3.3 Discontinuities. 3.3.1 Crack: Rupture in the material which may 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 forg
23、ing them into the surface. the material making process. They may exist as discrete particles or strings of particles extending 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 origina
24、ting from 3.4 Test temperature: Ambient temperature, unless otherwise specified. 3.5 Simple random sampling i): The taking 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 1): A defect that
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