NASM 22529-2-1999 GROMMET, CUSHION CY)MPOSITE, EDGING.PDF
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1、NASM 22529-2-1999 GROMMET, CUSHION CY)MPOSITE, EDGING_ADOPTION NOTICE NASM22529/2 , GROMMET, CUSHION, COMPOSITION, EDGING, was adopted on 23 MARCH 1999 for use by the Department of Defense (DoD). Proposed changes by DoD Activities must be submitted to the DoD Adopting Activity: Defense Industrial Su
2、pply Center, ATTN: DISC-AESD, 700 Robbins Avenue, Philadelphia, PA 19111-5096. DoD Activities may obtain copies of this standard from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, FA 19111-5094. The private sector and other Government agencies may purchase c
3、opies from the AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC., 1250 EYE STREET, N. W., WASHINGTON, DC 20005-3924. Custodians : Amy - Navy - AS Air Force - 99 DIA- IS Adopting activity: DIA-IS . (Project 5325-0455-01) AMSC N/A FSC 5325 DISTRIBUTION STATEMENT A. Approved for public release; distrib
4、ution is unlimited. COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Information Handling Services. .I. STD.AIA/NAS NASfl22527/2-ENGL 1999 0338743 050b32b 7T2 NATIONAL AEROSPACE STANDARD Q COPYRIGHT 1999 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RES
5、ERVED NASM2252912 SPECIFICATION SHEET GROMMET, CUSHION CY)MPOSITE, EDGING The requirements for acquiring the product desmied herein shall consist of this specification sheet and the issue of NASM22529. REQUIREMENTS: 1. Materials: 1.1 Substrate: -1 thru -7, %hard 300 series stainless steel per AMs 55
6、17, AMs 5903, Ah4S 5907 or AMs 5310; -8, % hard 300 series stainless steel per AMs 5518, AMs 5904 or AMs 591 1. 1.2 Coating: Thennosetting epoxy, color: lime green per FED-STD 595, Color Number 14553. 1.2.1 Elastomer Cushion: Shore A, 46 Durometer. Flammability per MIL-STD-202, Method 11 1 A, color:
7、 Grey 1.2.2 Elongation: No cracks shall be viaMe at 15% elongation. 1.2.3 Thermal endurance: 85OC continuous (2,000 Ws) per IEEE 57. 2. The Composite Grommet meets all the requirements of NASM22529 with the following exception: 4.2.9 Dielectric withstanding voltage, 1200 Volts, 60 Hz. This grommet i
8、s primarily intended to provide chafing protection. THE INITIAL RELEASE OF THIS DOCUMENT SUPERSEDES MJLDTG22529/2, REVISION B. PART NUMBERS REMAIN M22529/2. LIST OF CURRENT SHEETS 1 of4 FSC 5325 APPROVAL DATE FEBRUARY 1999 REVISION USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STAN
9、DARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SUPPLIERS OR CERTIFY CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABILITY OF ITEMS FOR ANY PARTICULAR APPLICATION, OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PAT
10、ENT OR TRADEMARK RIGHTS COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Information Handling ServicesNATIONAL AEROSPACE STANDARD Q COPYRIGHT 1999 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA MC. ALL RIGHTS RESERVED NASM2252912 3. Examples of Part Number: 3.1 Reek M225
11、29/2 -4 R -25 (BT4-0025-ERO602) M2252912 -6 R -100 (BT6-0100-ERO602) Length in feet Length in fa Sheet thickness Sheet thickness .070”-.093” .105”-.134“ 3.2 Cut lengths: Cut Lengths are available in increments of. 15”. EXAMPLE: Calculated Length: 4.10” dia. Hole x R: = 12.88”/.15 = 85.87 castles, cu
12、t shorter to the nearest whole castle. M22529/2 -1 C -85 (BT1-0085-ECO602) Number of Castles Factory Precut Length Sheet Thikne .O25 - .O36 Notes: 1 Tolerances: .XX = f.02; .XXX = f.010 2 Within a given sheet thickness range and spring characteristicof the grommet, end user should determine the grom
13、met size by trial. 3 In applications where a sacrificial surface is desirable the cushion grommet may be used for edge dressing, odd-shaped holes, and circular holes to provide chafing protection. 4 Installation: 4.1 To assure the absence of deformation of adjacent gripping fingers (Castles) proxima
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