AECMA PREN 6110-2000 Aerospace Series Bolts Blind 100 Degree Flush Head Stainless Steel Edition P 1《航空航天系列.螺钉100度埋头钉不锈钢.P1版》.pdf

1、STD-AECMA PREN bLI,U-EMGI- 2OD M ZOL23Ll OUL7Tb LL AECMA STANDARD prEN 61 IO NORME AECMA Edition P I AECMA NORM February 2000 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (+32) 2 775 81 11 Edition approved for

2、 publication ICs: Descriptors: Comments should be sent within six months AIBITF3 Chairman after the date of publication to ENGLISH VERSION Aerospace series Bolts, blind 100“ flush head Stainless steel Srie arospatiale Boulons aveugles, tte fraise IOO“, en acier inoxydable Luft- und Raumfahrt Bolzen,

3、 blind 100“ Senkkopf Rostfreier Stahl This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs of AECMA- Members. It has been technically approved by the experts of the con

4、cerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Presfandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examinati

5、on and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it wil/ be submiffed as a draft European Standard to CEN (European Committee for Standardization) for formal vote. Mr Luck 2000-02-29 AECMA Gulledelle 94 6-1200 BRUXELLE

6、S I I O aecrna 2000 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-S1D-AF:CMA PREN LLZO-.ENGL 2000 m LOL233tL 0037907 057 m Page 2 prEN 61 1 O: 2000 C

7、ontents list Scope . 3 . Normative references 3 Requirements 3 Designation . 6 . . 6 6 Technical specification,., Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license fr

8、om IHS-,-,-Page 3 prEN 61 1 O: 2000 Fe: and Stem 1 Scope A-286 CRES per AMs5737 This standard specifies the configuration, dimensions, tolerances and mass of a stainless steel blind bolt with 100“ flush head for aerospace application. CRES Inconel 600 2 Normative references Passivated per AMS-QQ-P-3

9、5 None This European Standard incorporates by dated or undated reference, provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of th

10、ese publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN2424 Aerospace series - Marking of aerospace products AMs5687 Nickel Alloy, Corrosion and Heat Resistant, Wire,

11、74Ni-l5,5Cr-8,OFe Annealed 1) AMs5737 Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, and Tubing, 15Cr-25,5Ni- I ,2Mo-2, ITi-0,006B-O,30V Consumable Electrode Melted, 1650 “F (899 OC) Solution and Precipitation Heat Treated 1) AMS-QQ-P-35 Passivation Treatments for Corrosion Resisting Ste

12、el 1) MI L-F-8975 Fasteners, Blind, High Strength, Installation Formed, Corrosion Resistant and Heat Resistant Steel and Titanium, General specification for 2) 3 Requirements 3.1 Configuration, Dimensions, Tolerances, Mass The configuration, dimensions, tolerances and mass shall conform to figure 1

13、and tables I and 2 3.2 Material A-286 CRES per AMs5737 or 1 Locking Collar 1 Inconel 600 per AMS5687 3.3 Surface treatment 3.4 Static values (shear tension) See Table I. 3.5 See Table 3. Fatigue values (tension-tension fatigue; for qualification only) 1) Published by: Society of Automotive Engineers

14、 (SAE), 400 Commonwealth drive, Warrendale, PA 15096-0001, USA. 2) Published by: Department of Defense (DoD), the Pentagon, Washington, D.C. 20301. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or netwo

15、rking permitted without license from IHS-,-,-Shifting Anvil shear min. N 8807 13011 22241 I) Diameter of serrated pin head shall not exceed “0 D” max. and may be 0,051 mm below “0 D” min. in area P only. 2) This type of bolt is supplied with a shifting anvil and installed with a single action tool F

16、igure 1: Configuration - Dimensions Table I Dimensions in millimetres Diameter code 05 06 08 OA Theor. * 0,102 7,264 8,966 12,090 B Ref. 1,321 1,651 2,311 Hole limits Z min. min. max. 21,438 I 4, 1664,242 I * This length of 0 D may be 0,051 mm undersize. Retention min. min. 6672 I 3336 11565 I 5782

17、Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Table 2 Dimensions in millimetres a Minimum grip length for diameter code 05 is 2,388 mm and for diamet

18、er code 06 is 3,048 mm. Diameter Tensile Preload code min. Table 3: Fatigue values High load Low load Duration cycles a Duration cycles a average min. min. min. I Tension-Tension Fatigue N I I N I N I 05 467 06 667 08 1157 21 04 209 3002 302 15.000 30.000 5204 520 30 O00 Copyright Association Europe

19、ene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-4 Designation EXAMPLE : Description block Identity block I Number of this Standard Diameter code (see table 1) Grip length code (se

20、e table 2) 5 Marking Marking as per EN2424 style B on rivet head (EN Standard Number, grip length code and manufacturers identification required). Instead of the EN Standard Number, the manufacturers part number shall be permissible. Single digit marking is permissible for grip length code less than

21、 10. Shifting anvil or serrated portion of stem are dyed green for the diameter code 05 and 06 only. 6 Technical specification See MIL-F-8975 except tensile strength and spindle retention requirements (see table 1). Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-