KS W ISO 9219-2005 Aerospace-Bolts thin hexagonal head for pulleys close tolerance shank short thread in alloy steel and cadmium plated or in titanium alloy and MoS2 lubricated or Dime.pdf

1、 KSKSKSKS KS W ISO 9219SKSKSKS KSKSKS SKSKS KSKS SKS KS , (MoS2) , , 6 KS W ISO 9219： 2005 2005 12 22 W ISO 9219：2005 ( ) ( ) ( ) ( ) ： ：2005 12 22 20050915 ： ： ( ) ( 02 5097282 5) . 7 5 , . ICS 49.030.20 KS W ISO 9219：2005 , (MoS2) , , 6 Aerospace Bolts, thin hexagonal head, for pulleys, close tole

2、rance shank, short thread, in alloy steel and cadmium plated or in titanium alloy and MoS2lubricated or in corrosion- resistant steel and passivated Dimensions and masses 2002 ISO 9219 Aerospace Bolts, thin hexagonal head, for pulleys, close tolerance shank, short thread, in alloy steel and cadmium

3、plated or in titanium alloy and MoS2lubricated or in corrosion-resistant steel and passivatedDimensions and masses . 1. 1 2)/235 ( ) 1 100 MPa(11 100 MPa( )/315 ( )2 6 . KS W ISO 9217 KS W ISO 9218 , ISO 9216 , ISO 1234 . 1 ( ) 2( ) . 2. . , . . . ISO IEC , . KS A ISO 13715：2002 KS W ISO 3353 1：2003

4、 1： KS W ISO 5855 2：2005 MJ 2： KS W ISO 7689：2002 1 100 MPa MJ KS W ISO 7913：2002 KS W ISO 9152：2005 1 100 MPa MJ , KS W ISO 9217：2005 W ISO 9219：2005 KS W ISO 9218：2005 ISO 1234：1997 Split pins ISO 8075：1985 Aerospace Surface treatment of hardenable stainless steel parts ISO 9216： 2002 AerospaceNut

5、s, hexagonal, slotted(castellated), for pulleys, in alloy steel and cadmium plated or in corrosion-resistant steel and passivatedDimensions and masses EN 2133：1997(3) Aerospace seriesCadmium plating of steels with specified tensile strength 1 450 MPa, copper, copper alloys and nickel alloys 4prEN 21

6、37( ) Aerospace seriesSteel FE-PL75 1 100 MPa R 1 250 MPaBars Dm e 100 mm 5prEN 2442( ) Aerospace seriesSteel FE-PL711 1 100 MPa R 1 300 MPaBars and wires Dm e 25 mm 4prEN 2446( ) Aerospace seriesSteel FE-PL45 1 100 MPa R 1 300 MPaBars D 25 mm m e 6prEN 2475( ) Aerospace seriesSteel FE-PL2106(30CrNi

7、Mo8) Air melted Hardened and tempered1 100 MPa R 1 300 MPaBar for machining D 100 mm m e 3EN 2491：1997( ) Aerospace seriesMolybdenum disulphide dry lubricants Coating methods 7prEN 2532( ) Aerospace seriesTitanium alloy TI-P68 1100 MPa R 1 280 MPaBar D 25 mm m e 4prEN 2793( ) Aerospace seriesPhospha

8、te treatment of ferrous alloys 6prEN 2817( ) Aerospace seriesSteel FE-PM1802(X5CrNiCu15-5) Consumable electrodeSolution treated and precipitation treatedRm 1 070 MPaBar for machining a or D 200 mm 8TR 3775：1999( ) Aerospace seriesBolts and pins Materials AMS QQ P 416A：2002 Plating, cadmium(electrode

9、posited) 3) AECMA (4( ) (CEN) AECMA 5) AECMA . prEN 3514 Aerospace seriesSteel FE-PL711Hardened and tempered1 100 MPa R( 1 300 MPaBar and wire for bolts Dm e 25 mm . 6) AECMA (7) AECMA . prEN 3466 Aerospace series Titanium alloy TI-P63001Solution treated and aged Bar for machining D 150 mm . (8) AEC

10、MA (3. 3.1 , , , 1, 2, 1 . . , . . KS W ISO 7913：2002 . 2 W ISO 9219：2005 3 1 ：mm D1E (1) A BD20.5D3H13D4D5H13 F H 0 0.3050 MJ50.84h6h 5 3.4 7.4 8 h12 8.7060 MJ614h6h 6 0.0100.035080 MJ614h6h 8 4.2 9.4 1.510 10.9 2.5100 MJ814h6h 10 0.0130.0386.2 12.3 1.9 13 14.3 3 120 MJ101.254h6h 12 7.9 16.3 17 18.

11、9 3.5150 MJ121.254h6h 15 9.8 8 18.3 2.419 21.1 170 MJ141.54h6h 17 0.0160.04111.5 9 21.3 22 24.5 4 200 MJ161.54h6h 20 13.5 10 23.3 3 24 26.8 220 MJ181.54h6h 22 15.5 11 26.3 27 30.2 250 MJ201.54h6h 25 0.0200.045f7 17.5 12 29.3 3.830 h13 33.6 5 L1(2)L2L3R1R2(3) kg/1 000 0.2 A B 0.3 0 0.20.20 L3 L3 1 mm

12、 L3 L3 1 mm050 005050 550 L16 L19 2.76 0.15 1.56 0.09 060 006060 660 4.47 0.22 2.53 0.12 080 L17 L110 0.25 5.85 0.39 3.31 0.22 100 L17.5 L111.5 10.97 0.62 6.21 0.35 120 L19 L114.5 0.40.4 19.52 0.89 11.06 0.5 150 L110 L116 27.39 0.99 15.52 0.56 170 L112 L119 0.6 0.6 39.36 1.28 22.31 0.73 200 L113 L12

13、0.5 57.8 1.85 32.76 1.05 220 L114.5 L122.5 76.17 2.24 43.17 1.27 250 007080 780 L115 L124.5 0.9 0.8 100.79 2.97 57.13 1.68 (1) KS W ISO 5855 2： 2005 . ： 050 060 , d D1 min 0.025 .(2) ： L1 30 1 L1 30 2 , L1 1 2 0 (3) . . A 7.85 kg/dm3 B 4.45 kg/dm33.2 2 . W ISO 9219：2005 2 ： 6 m 10 m(2) 1 . A 1 100 M

14、Pa(1) , D3： 1 . 1 . B 1 100 MPa(1) ： 25 m 10 m( ) ISO 8075 C (1) (2) 20 mm . . 4. . KS W ISO 9219 A 050 024KS / ( 2 ) ( 1 ) ( 1 ) 5. 2 . 4. . 6. 6.1 , A KS W ISO 7689 . 6.2 , B KS W ISO 9152 . (1) 2 1) KS W ISO 3353 1 . ( 1 050 060 4 W ISO 9219：2005 ：mm ： m KS A ISO 13715 (1) (2) KS W ISO 3353 1 . (

15、3) 2 080 250 (2) (1) (3) 0.5(2) 5 W ISO 9219：2005 1() . . 1 1 ： EN 2133 A 1 100 MPa(1prEN 2137 ) prEN 2442 prEN 2446 prEN 2793, C , D3： prEN 2475 TR 3775 B 1 100 MPa(1prEN 2532 EN 2491 ) (MoS2) TR 3775 C prEN 2817(2)ISO 8075 (1) (2) AMS 5659 F10.84, 15 5 PH, H 1025 1 2 ： AMS QQ P 416A A 1 100 MPa(1)

16、 , D3： B 1 100 MPa(1) ISO 8075 C (1) 6 , (MoS2) , , 6 2006 1 16 135513 7017 (02)60094567 (02)600948878 http:/ 607822 1 11( 10) (051)5571239 Fax. (051)557 0430 702012 2 1741( 3 ) (053)38415624 Fax. (053)384 1565 790 380 627( ) (054)2789611 Fax. (054)278 9662 406130 994( 16) (032)26002607 Fax. (032)26

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19、031)82981824 Fax. (031)8298185 KS W ISO 9219：2005 KSKSKSSKSKS KSKS SKS KSKS SKSKS KSKSKSAerospaceBolts, thin hexagonal head, for pulleys, close tolerance shank, short thread, in alloy steel and cadmium plated or in titanium alloy and MoSKOREAN STANDARDS ASSOCIATION 2lubricated or in corrosion resistant steel and passivatedDimensions and masses ICS 49.030.20