SAE AMS 4349D-2006 Core Honeycomb Aluminum Alloy Corrosion Inhibited For Sandwich Construction 5056 350 (177)《5056、350 (177)夹层结构用耐腐铝合金蚀蜂巢芯》.pdf

1、_ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising there

2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2011 SAE International All rights reserved. No part of this p

3、ublication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-497

4、0 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS4349D AEROSPACE MATERIAL SPECIFICATION AMS 4349 REV. D Issued 1977-07 Revised

5、2006-09 Reaffirmed 2011-11 Superseding AMS 4349C Core, Honeycomb, Aluminum Alloy, Corrosion Inhibited For Sandwich Construction 5056, 350 (177) RATIONALE This document has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE 1.1 Form This specification covers bonded honeycomb cor

6、e made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered. 1.2 Application This honeycomb core has been used typically in sandwich construction for short-term exposure up to 350 F (177 C) or for long-term exposure up to 200 F (95 C), but usage is not lim

7、ited to such applications. 1.3 Safety - Hazardous Materials While the materials, methods, applications, and processes described or referenced in this specification may involve the use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is the

8、 sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of

9、 the purchase order forms a part of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last

10、published issue of that document shall apply. 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS 4005 Aluminum Alloy Foil, 5.0Mg - 0.12Mn - 0.12Cr (5056-H1

11、91), Strain Hardened SAE AMS 4349D Page 2 of 12 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 117 Salt Spray (Fog) Testing ASTM C 273 Shear Properties in Flatwise Plane of Flat

12、Sandwich Constructions or Sandwich Cores ASTM C 365 Flatwise Compressive Strength of Sandwich Cores 2.3 U.S. Government Publications Available from the Document Automation and Production Service (DAPS), Building 4/D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: 215-697-6257, http:/assist.da

13、ps.dla.mil/quicksearch/. FED-STD-595 Color 3. TECHNICAL REQUIREMENTS 3.1 Material 3.1.1 Metal Shall be AMS 4005 aluminum alloy foil of the thickness specified on the part drawing or purchase order except that maximum foil thickness shall be as specified in Table 1. 3.1.2 Adhesive The adhesive system

14、 used for node-to-node attachment shall be such that the resultant core meets the requirements specified herein. 3.2 Configuration The core material shall consist of strips of aluminum alloy foil treated for corrosion protection, bonded together such that cells approximately hexagonal in shape are f

15、ormed when fully expanded (See Figure 1). 3.2.1 Designation Core shall be designated according to the following numbering system: Nominal density, pounds per cubic foot (kg/m3) Cell size, inch (mm) Foil thickness, ten-thousandths inch (m) “N” for nonperforated or “P” for perforated Alloy Adhesive, o

16、ption of supplier Example: Core with a nominal density of 4.3 pounds per cubic foot (69 kg/m3) with a 1/4 inch (6.4 mm) cell size, 0.0020 inch (51 m) foil thickness, nonperforated, made of 5056 aluminum alloy, and bonded with required adhesive shall be numbered as follows: 4.3 - 1/4 20N (5056) (XXXX

17、) in inch/pound units 69 - 6.4 51N (5056) (XXXX) in SI units SAE AMS 4349D Page 3 of 12 3.2.2 Perforations When perforated core is specified, the perforations shall be approximately 0.005 inch (0.13 mm) in diameter and spaced to vent each cell into at least three adjacent cells at least once for eac

18、h 1/4 inch (6.4 mm) of core thickness. When thicknesses under 1/4 inch (6.4 mm) are furnished, there shall be at least one perforation per cell into each of three adjacent cells. 3.2.3 Cell Pitch Shall be 1.733 times the nominal cell size, +20%, -10%, measured by taking the average distance between

19、ten nodes along a ribbon for six different ribbons. 3.3 Condition Core shall be supplied in the expanded form; it shall be clean, free of contamination, and treated for corrosion resistance. 3.4 Properties Core, having nominal dimensions as specified in Table 1, shall conform to the following requir

20、ements; tests shall be conducted on the core supplied in accordance with specified test methods. Properties of core having nominal dimensions other than specified in Table 1 shall be acceptable to purchaser. 3.4.1 Flatwise Compressive Strength The minimum individual values shall be as specified in T

21、able 1, determined in accordance with 4.5.1. 3.4.2 Plate Shear Strength and Plate Shear Modulus Shall be as specified in Table 1, determined in accordance with ASTM C 273 at 77 F 5 (25 C 3), using a 0.625-inch (15.88-mm) thick specimen. 3.4.3 Node Bond Strength Shall be not less than 30 pounds force

22、 (133 N) at 77 F 5 (25 C 3) and not less than 15 pounds force (67 N) at 350 F 5 (177 C 3), determined in accordance with 4.5.2. 3.4.4 Core Density Shall be within 10% of the specified density, determined in accordance with 4.5.3. SAE AMS 4349D Page 4 of 12 3.4.5 Corrosion Resistance Core specimens s

23、hall show a weight loss not greater than 125 milligrams per square foot (1345 mg/m2) of exposed foil area, determined in accordance with 4.5.4. TABLE 1A - CORE PROPERTIES, INCH-POUND UNITS Cell Size Inch Nominal Foil Thickness Designated Inch Nominal Foil Thickness Maximum Inch Nominal Density pound

24、s per cubic foot Plate Shear Strength psi, min individual Direction of Test W Plate Shear Strength psi, min individual Direction of Test L Plate Shear Modulus ksi, min average Direction of Test W Plate Shear Modulus ksi, min average Direction of Test L Flatwise Compressive Strength psi, min (Individ

25、ual) Bare Flatwise Compressive Strength psi, min (Individual) Stabilized 1/8 0.0007 0.0010 0.0015 0.0020 0.0011 0.0015 0.0022 0.0029 3.1 4.5 6.1 8.1 110 205 305 440 200 350 535 740 16.0 25.0 37.0 50.0 31.0 51.0 77.0 112.0 250 475 760 1200 260 500 825 1300 5/32 0.0007 0.0010 0.0015 0.0020 0.0025 0.00

26、11 0.0015 0.0022 0.0029 0.0034 2.6 3.8 5.3 6.9 8.4 80 155 250 360 455 152 272 435 610 775 12.0 20.0 31.0 42.0 52.0 24.0 41.0 64.0 91.0 115.0 180 360 615 920 1110 185 375 650 1000 1375 3/16 0.0007 0.0010 0.0015 0.0020 0.0025 0.0030 0.0011 0.0015 0.0022 0.0029 0.0034 0.0042 2.0 3.1 4.4 5.7 6.9 8.1 50

27、110 198 280 360 440 105 200 340 480 610 740 9.0 16.0 24.0 34.0 42.0 50.0 17.0 31.0 50.0 70.0 91.0 112.0 110 250 460 665 920 1200 120 260 490 735 1000 1300 1/4 0.0007 0.0010 0.0015 0.0020 0.0025 0.0030 0.0040 0.0011 0.0015 0.0022 0.0029 0.0034 0.0042 0.0053 1.6 2.3 3.4 4.3 5.2 6.0 7.9 38 62 130 190 2

28、45 300 430 78 130 230 325 425 512 720 6.0 11.0 18.0 24.0 30.0 36.0 49.0 13.0 21.0 35.0 48.0 62.0 75.0 108.0 75 145 300 440 600 740 1150 80 155 315 465 645 805 1265 3/8 0.0007 0.0010 0.0015 0.0020 0.0025 0.0030 0.0040 0.0050 0.0011 0.0015 0.0022 0.0029 0.0034 0.0042 0.0053 0.0065 1.0 1.6 2.3 3.0 3.7

29、4.2 5.4 6.5 25 38 62 100 150 180 260 335 45 78 130 190 260 315 450 568 4.0 6.0 11.0 15.0 20.0 23.0 32.0 39.0 7.0 13.0 21.0 30.0 40.0 47.0 66.0 84.0 25 75 145 240 335 410 630 825 35 80 155 250 362 443 680 908 SAE AMS 4349D Page 5 of 12 TABLE 1B - CORE PROPERTIES, SI UNITS Cell Size mm Nominal Foil Th

30、ickness Designated m Nominal Foil Thickness Maximum m Nominal Density kg/m3Plate Shear Strength MPa, min individual Direction of Test W Plate Shear Strength MPa, min individual Direction of Test L Plate Shear Modulus MPa, min average Direction of Test W Plate Shear Modulus MPa, min average Direction

31、 of Test L Flatwise Compressive Strength MPa, min (Individual) Bare Flatwise Compressive Strength MPa, min (Individual) Stabilized 3.2 17.8 25.4 38.1 50.8 27.8 38.1 55.9 73.7 50 72 98 130 0.758 1.413 2.103 3.034 1.379 2.413 3.620 5.102 110 172 255 345 214 352 531 772 1.724 3.275 5.240 8.274 1.793 3.

32、448 5.688 8.964 4.0 17.8 25.4 38.1 50.8 63.5 27.8 38.1 55.9 73.7 86.4 42 61 85 110 135 0.552 1.069 1.724 2.482 3.137 1.048 1.875 2.999 4.206 5.344 83 138 214 290 359 165 283 441 627 793 1.241 2.482 4.240 6.343 7.633 1.276 2.586 4.482 6.895 9.481 4.8 17.8 25.4 38.1 50.8 63.5 76.2 27.8 38.1 55.9 73.7

33、86.4 106.7 32 50 70 91 110 130 0.345 0.758 1.365 1.931 2.482 3.034 0.724 1.379 2.344 3.310 4.206 5.102 62 110 165 234 290 345 117 214 345 483 627 772 0.758 1.724 3.172 4.723 6.343 8.274 0.827 1.793 3.329 5.068 6.895 8.964 6.4 17.8 25.4 38.1 50.8 63.5 76.2 101.6 27.8 38.1 55.9 73.7 86.4 106.7 134.6 2

34、6 37 55 69 83 96 126 0.262 0.427 0.896 1.310 1.689 2.068 2.965 0.538 0.896 1.586 2.241 2.930 3.530 4.964 41 76 124 165 207 248 338 90 145 241 331 427 517 745 0.517 1.000 2.068 3.034 4.137 5.102 7.929 0.552 1.069 2.172 3.206 4.447 5.550 8.722 9.5 17.8 25.4 38.1 50.8 63.5 76.2 101.6 127.0 27.8 38.1 55

35、.9 73.7 86.4 106.7 134.6 165.1 16 26 37 48 59 67 86 104 0.172 0.262 0.427 0.690 1.034 1.241 1.793 2.310 0.310 0.538 0.896 1.310 1.793 2.172 3.103 3.916 28 41 76 103 138 159 221 269 48 90 145 207 276 324 455 579 0.172 0.517 1.000 1.655 2.310 2.827 4.344 5.688 0.241 0.552 1.069 1.724 2.496 3.054 4.689

36、 6.261 3.5 Quality The core, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimental to usage of the core. 3.5.1 The core shall be free from corrosion, oil, and other contamination detrimental to bonding. 3.5.2 A

37、change in color of core material shall be acceptable provided the color change occurs in a line parallel to “L” (Figure 1), indicative of a change in foil material where more than one foil coil is used in the manufacture of a core block. 3.5.3 Expanded core shall make total facing contact with a fla

38、t surface under uniform pressure without resulting in any damage that would cause rejection of the core. 3.5.4 Expanded core splices which have double foils (two ribbons bonded together which cause uneven expansion in the “L” direction (See Figure 1) shall be acceptable if the double foils are not m

39、ore frequent than one in any 8 inches (203 mm). SAE AMS 4349D Page 6 of 12 3.5.5 The c/d ratio (See Figure 2) of mismatched nodes shall be 0.00 to 0.25. 3.5.6 The maximum requirements for imperfections visually observed in any randomly selected 12-inch (305-mm) diameter circle are shown in Table 2.

40、TABLE 2 - VISUAL IMPERFECTIONS Type of Imperfection Maximum Number for 1/8 Inch (3.2 mm) Cell Size Maximum Number for 5/32 inch (4.0 mm) Cell Size Maximum Number for 3/16 inch (4.8 mm) Cell Size Maximum Number for 1/4 inch (6.4 mm) Cell Size Maximum Number for 3/8 inch (9.5 mm) Cell Size Mismatched

41、Nodes Loose Metal or Flakes (See 3.5.6.1) Split Cell Walls Buckled Cell Walls Unbonded Nodes 70 35 0 0 2 55 28 0 0 2 40 20 0 0 2 25 12 0 0 2 10 5 0 0 2 3.5.6.1 Flakes are excess metal attached to foil edges which do not interfere with measurements of core thickness. 3.6 Sizes and Tolerances 3.6.1 Si

42、ze Core shall be supplied in the size ordered with core dimensions as shown in Figure 1: where: T = Thickness, depth, or height dimension measured parallel to the core cell axis L = Longitudinal or ribbon (length) dimension measured along the direction of a ribbon W = Width dimension measured normal

43、 to the ribbon direction 3.6.2 Core Thickness Shall be 0.005 inch ( 0.13 mm) for machined slices up to 4.0 inches (102 mm) in nominal thickness, 0.062 inch ( 1.57 mm) for machined slices over 4 inches (102 mm) in nominal thickness, and + 0.25 inch (+ 6.4 mm), -0.00 for raw block. 3.6.3 Length (L) an

44、d width (W) of unexpanded core shall be as ordered, + 0.25 inch (+ 6.4 mm), -0; for expanded core, tolerances shall be + 2 inches (+ 51 mm), -0. 3.6.4 The cell size of any ten adjacent cells shall vary not more than 10% from nominal, determined by taking the average distance between node bonds along

45、 the “W” dimension (See Figure 1) for at least 60 cells selected at random in groups containing ten adjacent cells. 3.6.5 All ribbons shall be parallel to each other within 10 degrees. The ribbon direction shall be determined by measuring the angle between one line through two nodes on the same ribb

46、on (“L” direction), 12 inches (305 mm) apart, and another line in the principal ribbon direction (See Figure 1). 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection The manufacturer of core shall supply all samples and shall be responsible for all required tests. Purchaser reserves the

47、 right to sample and to perform any confirmatory testing deemed necessary to ensure that the core conforms to specified requirements. SAE AMS 4349D Page 7 of 12 4.2 Classification of Tests 4.2.1 Acceptance Tests Flatwise compressive strength (3.4.1), node bond strength (3.4.3), and core density (3.4

48、.4) are acceptance tests and shall be performed on each lot. 4.2.2 Preproduction Tests All technical requirements are preproduction tests and shall be performed prior to or on the first-article shipment of core by the manufacturer, when a change in ingredients and/or processing requires reapproval a

49、s in 4.4.2, and when purchaser deems confirmatory testing to be required. 4.3 Sampling and Testing Shall be in accordance with the following: 4.3.1 For Acceptance Tests Each block or 2% of the slices from each lot shall be sampled at random to provide sufficient core to perform all required tests. The number of determinations for each requirement shall be as specified in the applicable test procedure or, if