1、- - - AECMA STANDARD prEN 6067 NORME AECMA Edition P 2 AECMA NORM October 2000 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 6-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 - Nota - Extra copies can be supplied by E.N.A.E. - Technopolis 54 -
2、 199. rue Jean-Jacques Rousseau - 92138 ISSY-LEC-MOULINEAUX CEDEX I I ICs: Descriptors: 2000-40-31 ENGLISH VERSION AECMA Mr Lck Gulledelle 94 8-1200 BRUXELLES Aerospace series Pin, quick release, self-retaining, Positive locking, double acting, Button handle Supersedes edition P 1 August 1998 Srie a
3、rospatiale Broche, dclenchement rapide, imperdable, verrouillage double action, Poigne bouton poussoir Luft- und Raumfahrt Kugelsperrbolren, selbstsichernd, doppeltwirkend, Druckknopfbettigung This %emspace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Associa
4、tion 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 concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shal
5、l not be changed to an extent that inferchangeability 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 OfEcial Services of the Member countries it will be submit
6、ted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. AIBfF3 Chairman I Edition approved for publication 1 Comments should be sent within six months after the date of Dublication to Copyright Association Europeene des Constructeurs de Materiel Aerospatial
7、Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN bOb7-ENGL 2000 = 303233L 0038773 732 Page 2 prEN 6067: 2000 Contents list Scope Normative references . . 3 Required characteristics 3 Designation . 8 Marking 9 Te
8、chnical specification 9 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-,-,-STD.AECMA PREN bOb7-ENGL 2000 S LOL23Ll 001877Li b57 = Page 3 prEN 6067: 2000 I
9、 Scope This standard specifies the dimensions, tolerances and the required characteristics of a quick release, self retaining, positive locking, double acting pin with button handle for aerospace application. 2 Normative references This European Standard incorporates by dated or undated reference pr
10、ovisions from other publications. These normative references are at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by a
11、mendment or revision. For undated references the latest edition of the publication referred to applies. EN 2424 AMS 5678 AMS-QQ-S-763 AMS-S-6758 AMS-T-6736 ASTM A 108 ASTM A 228 ASTM A 240 ASTM A 31 3 ASTM A 967 MIL- P-23460 QQ-P-416 Aerospace series - Marking of aerospace products Steel, corrosion
12、resistant, wire 17CR-7.1 NI-1 .lAL , cold drawn, precipitation-hardenable, (UNS S 177000) 1) Steel bars, wire, shapes, and forgings, corrosion resistant 1) Steel, chrome-molybdenum (41 30) bars and reforging stock (Aircraft Quality) 1) Tubing, chrome-molybdenum (4130 or 8630) steel, seamless and wel
13、ded 1) Standard specification for steel bars, carbon, cold finished, standard quality 2) Standard specification for steel wire, music spring quality 21 Standard specification for heat-resisting chromium and chromium-nickel stainless steel plate, sheet, and strip for pressure vessels 2) Standard spec
14、ification for stainless steel spring wire 2) Standard specification for chemical passivation treatments for stainless steel parts 2) Pin, quick-release, self-retaining, positive-locking 3) Plating, cadmium (electrodeposited) 3) 3 Required characteristics 3.1 Configuration, dimensions, tolerances See
15、 figure 1 and tables I, 2 and 3. Dimensions and tolerances are expressed in inches (millimetres) i) Published by: Society of Automotive Engineers (CAE), 400 Commonwealth drive, Warrendale, PA 15096 - 0001. 2) Published by: American Society for Testing and Materials. (ASTM), 100 Barr Harbor Dr., West
16、 Conshohocken, 3) Published by: Department Of Defense (DOD) the Pentagon, Washington DC 20301. PA I 9428-2959 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from I
17、HS-,-,-STDeAECMA PREN bOb7-ENGL 2GOo 3012311 0038975 595 Page 4 prEN 6067: 2000 ,soa 1 Code L + 0.020 O + yo8 3 Table 2 : Grip length Grip length Code I L Grip length Code I L + 0.020 O + yoal 70 2.600 2.700 (68,581 7.000 (1 77,80) 7.1 O0 (1 8OW 7.200 (1 82,88) 7.300 (1 85,42) 0.400 O4 I (10,16) 71
18、0.500 O5 1 (12,701 28 72 29 73 0.600 30 5.200 52 I (132,08) 7.400 74 I (187,96) 0.800 O8 I (20,32) 31 3.1 O0 (78,741 5.300 53 1 (134,62) 7.500 75 I (190,501 0.900 O9 I (22,86) 3.200 32 I (81,28) 5.400 5.500 7.600 7.700 7.800 (1 98,12) 7.900 (200,66) 55 1 (139,70) 1 .o00 1.100 1.200 l2 (30,48) 3.300
19、3.400 3.500 (88,901 3.600 36 (91,44) 5.600 5.700 1.300 l3 I (33,02) 5.800 58 I (147,32) 8.000 8o I (203,20) 1.400 l4 I (3536) 3.700 37 I (93,98) 1.500 1 (38,101 3.800 3.900 4.000 (1 01,60) 4.100 (1 04,14) 8.200 8.300 1.600 1.700 1.800 (45,721 1 .goo (48,261 6.100 6.200 8.400 84 1 (213,36) 6.300 63 1
20、 (160,021 8.500 85 (215,90) 4.200 42 I (106,68) 8.600 2.000 2o I (50,80) 4.300 4.400 6.500 6.600 6.700 (1 70,18) 2.100 21 I (53,341 8.800 88 I (22332) 8.900 89 I (226,06) 4.500 4.600 4.700 (1 19,38) 6.800 68 I (172,72) 9.000 I (228,60) 6.900 69 I (175,26) 7.100 1 (231,141 (continued) (continued) (co
21、ntinued) (continued) 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-,-,-STD*AECMA PREN bOb7-ENGL 2000 W 103231i 0038978 2TV 9 Page 7 prEN 6067: 2000 Code
22、92 93 94 Table 2 (concluded) L + 0.020 (t t508 ) 9.200 (233,68) 9.300 (236,22) 9.400 (238,76) O Diameter Code Nominal inch 03 311 6 04 1 14 05 511 6 06 318 07 711 6 08 112 o9 911 6 10 518 12 314 14 718 16 I 9.500 9.600 9.700 (246,38) Double Shear Tensile Strength Recommended min. min. Hole Diameter
23、max. min. LBS LBS (daw (daw 4 600 200 O. 1940 o. 1900 (2 046) (88) (4,931 (4,83) 8 200 230 0.2540 0.2500 (3 648) (102) (6.45) (635) 12 800 510 0.3165 0.3125 18 400 575 0.3790 0.3750 25 O00 710 0.4425 0.4375 32 800 1160 0.5050 0.5000 (14 590) (51 5) (12,83) (12,70) 41 200 I 420 0.5675 0.5625 (18 327)
24、 (631) (1441) (1429) 51 200 2 070 0.6300 0.6250 (22 775) (920) (16,OO) (15,87) 73 600 2 950 0.7570 0.7500 (32 739) (1 312) (1923) (1 9,05) 100 O00 3 900 0.8820 0.8750 (44 482) (I 734) (22,401 (22.22) 131 O00 5 480 1 .o1 O0 1 .o000 (58 272) (2 437) (25,651 (25,40) (5 694) (226) (8,041 (7,941 (8 185)
25、(255) (9,631 (9,521 (11 121) (31 5) (1 1,24) (11,ll) 3.2 Mechanical characteristics See table 3 Table 3 : Mechanical characteristics, hole diameter Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or netwo
26、rking permitted without license from IHS-,-,-Page 8 prEN 6067: 2000 Spindle Button Spring Handle 3.3 Materials, finishes See table 4. Alloy steel 4130 (HRC 36 to 40) as per AMs-S-6758 Carbon steel as per ASTM A 108 Music wire as per ASTM A 228 Carbon steel as per ASTM A 108 or CRES 302 as per QQ-S-7
27、63 Table 4 : Materials, finishes Head ELEMENTS I Alloy steel 4130 as per MIL-S-6758 (HRC 36 to 40) or Carbon steel as per ASTM A 108 (HRC 36 to 40) Figure 1 4ttaching Ring o Music wire as per ASTM A 228 o Balls Ring Handle o CRES 440C (HRC 58 to 62) as per AMS-QQ-S-763 CRES 17-7 PH as per AMS 5678 (
28、heat treatment to CH 900) or CRES 302 as per ASTM A 313 Description I Description block Pin, quick release, self-retaining, positive locking, double acting, button handle MATERIAL Identity block EN6067T04-1 O I Alloy steel 4130 (HRC 36 to 40) as per AMs-T-6736 or AMs-S-6758 I- Number of this standar
29、d Handle code (see figure i) Diameter code (see table I) TAB Carbon steel as per ASTM A 108 or CRES 302 as per ASTM A 240 FINISH Cadmium plated as per QQ-P-4 1 6 type I I, class 2 Cadmium plated as per QQ-P-416 type II, class 2 Passivated as per ASTM A 967 Cadmium plated as per QQ-P-416 type II, cla
30、ss 2 Cadmium plated as per QQ-P-416 type II, class 2 Passivated as per ASTM A 967 Cadmium plated as per QQ-P-416 type II, class 2 4 Designation EXAMPLE : NOTE: If necessary, the code 19005 shall be placed between the description block and the identity block Copyright Association Europeene des Constr
31、ucteurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN bOb7-ENGL 2000 10123LL 00187aO 752 Page 9 prEN 6067: 2000 5 Marking Paris shall be marked as per EN 2424, style P (see figure 1). 6 Technical specification See MIL-P-23460. 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-,-,-
